JAA Test Prep 033 - Flight Planning Edition 2008 033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS 1 © 2008 AVIATIONEXAM.com 1129 (A) 1171 (D) 12526 (C) 25049 (B) 25050 (C) 25051 (D) 25070 (B) 25173 (D) 28335 (D) 28336 (A) 28337 (A) 28338 (A) 033-01-01 Navigation plan 1129. (all) How many feet you have to climb to reach FL75? Given: Departure aerodrome elevation: 1.500 ft QNH: 1023 hPa Temperature: ISA 1 hPa: 30 ft #A) 6.300 ft B) 6.000 ft C) 6.600 ft D) 7.800 ft 1171. (all) VFR flights shall not be flown over the congested areas of cities at a height less than: A) the heighest obstacle. B) 2.000 ft above the heighest obstacle within a radius of 600 ft from the aircraft. C) 500 ft above the heighest obstacle. #D) 1.000 ft above the heighest obstacle within a radius of 600 m from the aircraft. 12526. (all) (Refer to figures 033-73) The measured course 042° T The variation in the area is 6° W and the wind is calm The deviation is 4° W In order to follow this course, the pilot must fly a compass heading of: A) 040° B) 044° #C) 052° D) 058° 25049. (all) (Refer to Jeppesen Manual chart ED-6) What is the lowest ICAO VFR level for a flight from TRA (N47°42 E008°26) to KPT (N47°45 E010°21) ensuring that you are at least at minimum grid area altitude with QNH 1013? A) FL070 #B) FL095 C) FL075 D) FL090 25050. (all) On a flight from (47°10 N 010°00 E) to (49°10 N 010°00 E) at a TAS of 140 kts with a 20 kts headwind component, how many nautical air miles do you fly? A) 100 B) 120 #C) 140 D) 70
25051. (all) Given CAS/RAS of 130 kts, OAT 0 °C at 10.000 ft, trip distance of 240 NGM, track 275° (T) and W/V 030/30 kts. What is your true heading and time enroute? A) 287° and 103 minutes. B) 287° and 95 minutes. C) 285° and 95 minutes. #D) 285° and 88 minutes. 25070. (all) (Refer to figure 033-06) What is the fuel, time and distance to climb from an aerodrome at sea level up to FL100 where the outside air temperature is 0 °C? A) 13 USG, 24 min, 45 NM. #B) 9 USG, 16 min, 28 NM. C) 9 USG, 14 min, 27 NM. D) 5 USG, 10 min, 16 NM. 25173. (all) Given: True course: 017° W/V: 340°/30 TAS: 420 kts Find: 1) the wind correction angle (WCA) 2) the ground speed (G/S) A) (1) +2°; (2) 416 kts. B) (1) +2°; (2) 396 kts. C) (1) -2°; (2) 426 kts. #D) (1) -2°; (2) 396 kts. 28335. (AIR: atpl, cpl; HELI: atpl, cpl) The average true course from C (62°N 020°W) to B (58°N 004°E) is: A) 120° B) 119° C) 099° #D) 109° 28336. (AIR: atpl, cpl; HELI: atpl, cpl) The initial magnetic course from C (62°N 020°W) to B (58°N 004°E) is: #A) 116° B) 080° C) 098° D) 113° 28337. (AIR: atpl, cpl; HELI: atpl, cpl) The initial true course from C (62°N 020°W) to B (58°N 004°E) is: #A) 098° B) 116° C) 080° D) 278° 28338. (AIR: atpl, cpl; HELI: atpl, cpl) The distance (NM) from A (64°N 006°E) to C (62°N 020°W) is: #A) 720 B) 690 C) 1590 D) 1440 033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS 2
© 2008 AVIATIONEXAM.com 28339 (A) 28340 (C) 28341 (D) 28342 (A) 28343 (D) 1112 (B) 1115 (D) 1121 (B) 1135 (A) 1138 (D) 28339. (AIR: atpl, cpl; HELI: atpl, cpl) The average magnetic course from A (64°N 006°E) to C (62°N 020°W) is: #A) 271° B) 259° C) 247° D) 279° 28340. (AIR: atpl, cpl; HELI: atpl, cpl) The average true course from A (64°N 006°E) to C (62°N 020°W) is: A) 271° B) 247° #C) 259° D) 079° 28341. (AIR: atpl, cpl; HELI: atpl, cpl) The initial magnetic course from A (64°N 006°E) to C (62°N 020°W) is: A) 262° B) 267° C) 271° #D) 275° 28342. (AIR: atpl, cpl; HELI: atpl, cpl) The initial true course from A (64°N 006°E) to C (62°N 020°W) is: #A) 271° B) 275° C) 267° D) 246° 28343. (AIR: atpl, cpl; HELI: atpl, cpl) The distance (NM) from C (62°N 020°W ) to B (58°N 004°E) is: A) 775 B) 725 C) 700 #D) 760 033-01-02 Fuel plan 1112. (all) (Refer to figure 033-05) For a flight departing from MSL at 3.663 lbs, cruising at FL80 at 2.300 RPM, 20 °C lean of peak EGT, in 40 kts headwind, calculate endurance: A) 4,75 hrs #B) 5,3 hrs C) 6,1 hrs D) 6,55 hrs 1115. (all) Given: Dry operating mass (DOM): 33.510 kg Load: 7.600 kg Final reserve fuel: 983 kg Alternate fuel: 1.100 kg Contingency fuel: 102 kg The estimated landing mass at alternate should be: A) 42.312 kg B) 42.093 kg C) 42.210 kg
#D) 42.195 kg 1121. (all) A multi engine piston aeroplane is on an IFR flight. The fuel plan gives a trip fuel of 65 US gallons. The alternate fuel, final reserve included, is 17 US gallons. Contingency fuel is 5% of the trip fuel. The usable fuel at departure is 93 US gallons. At a certain moment the fuel consumed according to the fuel gauges is 40 US gallons and the distance flown is half of the total distance. Assume that fuel consumption does not change. Which statement is right? A) At the destination there will still be 30 US gallons in the tanks. #B) The remaining fuel is not sufficient to reach the destination with reserves intact. C) At departure the reserve fuel was 28 US gallons. D) At destination the required reserves remain intact. 1135. (all) (Refer to figure 033-05) Given: Cruising: FL75 Mixture: lean Full throttle: 2.300 RPM Takeoff fuel: 444 lbs Takeoff from: MSL Find endurance in hours: #A) 5 hrs 12 mins. B) 5 hrs 20 mins. C) 4 hrs 42 mins. D) 5 hrs 23 mins. 1138. (all) For a planned flight the calculated fuel is as follows: Flight time: 2:42 Taxi fuel: 9 kg Block fuel: 136 kg The reserve fuel, at any time, should not be less than 30% of the remaining trip fuel. How much fuel should remain after 2 hours flight time? A) 33 kg trip fuel and no reserve fuel. B) 33 kg trip fuel and 10 kg reserve fuel. C) 23 kg trip fuel and 10 kg reserve fuel. #D) 25 kg trip fuel and 8 kg reserve fuel. 033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS 3 © 2008 AVIATIONEXAM.com 1146 (A) 1155 (A) 1159 (A) 1164 (C) 1173 (A) 1275 (B) 1277 (A) 1146. (all) (Refer to figure 033-02) A flight has to be made with the SEP1. For the fuel calculation allow: - 10 lbs fuel for start up and taxi - 3 mins and 1 gallon of additional fuel to allow for the climb - 10 mins and no fuel correction for the descent - Planned flight time (overhead to overhead) is 3 hrs 12 mins - Reserve fuel 30% of the trip fuel - Power setting is 25HG (or full throttle) 2100 RPM, 20 °C lean
- FL70 and OAT is 11 °C The minimum block fuel is: #A) 283 lbs B) 268 lbs C) 215 kg D) 252 kg 1155. (all) During an IFR flight in a Beech Bonanza the fuel indicators show that the remaining amount of fuel is 100 lbs after 38 minutes. The total amount of fuel at departure was 160 lbs. For the alternate fuel, 30 lbs is necessary. The planned fuel for taxi was 13 lbs. Final reserve fuel is estimated at 50 lbs. If the fuel flow remains the same, how many minutes can be flown to the destination with the remaining fuel? #A) 12 minutes. B) 63 minutes. C) 44 minutes. D) 4 minutes. 1159. (all) (Refer to figure 033-08) A flight has to be made with a multi engine piston aeroplane. For the fuel calculations take 5 US gallons for the taxi, and an additional 13 minutes at cruise condition to account for climb and descent. Calculated time overhead to overhead is 2 hrs 37 min. Power setting is 65%, 2.500 RPM Calculated reserve fuel is 30% of the trip fuel FL120, Temperature 1 °C Find the minimum block fuel: #A) 91 US gallons. B) 86 US gallons. C) 76 US gallons. D) 118 US gallons. 1164. (all) For a planned flight the calculated fuel is as follows: Flight time: 3:06 Taxi fuel: 8 kg Block fuel: 118 kg The reserve fuel, at any time, should not be less than 30% of the remaining trip fuel How much fuel should remain after 2 hours flight time? A) 27 kg trip fuel and 12 kg reserve fuel. B) 39 kg trip fuel and 12 kg reserve fuel. #C) 30 kg trip fuel and 9 kg reserve fuel. D) 39 kg trip fuel and no reserve fuel. 1173. (all) (Refer to figure 033-04) Using the following information, calculate the range. Given: Aeroplane mass at start up: 3.663 lbs Fuel load (density 6lbs/gal): 74 gal Takeoff altitude: sea level Headwind: 40 kts Cruise altitude: 8.000 ft Power setting: full throttle 2.300 RPM 20 °C lean of peak #A) 633 NM B) 844 NM C) 730 NM D) 547,5 NM 1275. (all)
(Refer to figure 033-10) Given the following data: FL75 Lean mixture Economy Power setting Find the endurance with no reserve: A) 06:12 #B) 05:01 C) 06:06 D) 05:11 1277. (all) (Refer to figure 033-02) A flight has to be made with the single engine sample aeroplane. For the fuel calculation allow: - 10 lbs fuel for start up and taxi - 3 minutes and 1 gallon of additional fuel to allow for the climb - 10 minutes and no fuel correction for the descent - Planned flight time (overhead to overhead) is 03 hours and 12 minutes - Reserve fuel 30% of the trip fuel Power setting is 25 inHg (or full throttle), 2.100 RPM, 20 °C lean Flight level is 70 and the OAT 11 °C The minimum block fuel is: #A) 283 lbs B) 268 lbs C) 252 lbs D) 215 lbs 033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS 4 © 2008 AVIATIONEXAM.com 1284 (D) 1298 (A) 2298 (C) 12241 (A) 24772 (B) 25034 (D) 25055 (A) 25060 (D) 25067 (A) 1284. (all) (Refer to figure 033-03) A flight has to be made with the single engine sample aeroplane. For the fuel calculation allow: - 10 lbs fuel for start up and taxi - 3 minutes and 1 gallon of additional fuel to allow for the climb - 10 minutes and no fuel correction for the descent - Planned flight time (overhead to overhead) is 02 hours and 37 minutes - Reserve fuel 30% of the trip fuel - Power setting is 23 inHg (or full throttle), 2.300 RPM, 20 °C lean - Flight level is 50 and the OAT -5 °C The minimum block fuel is: A) 250 lbs B) 208 lbs C) 270 lbs #D) 265 lbs 1298. (all) (Refer to figure 033-07) A flight is to be made in a multi engine piston aeroplane (MEP1). The cruising level will be 11.000 ft. The outside air temperature at FL is -15 °C. The usable fuel is 123 US gallons.
The power is set to economic cruise. Find the range in NM with 45 min reserve fuel at 45% power. #A) 752 NM B) 852 NM C) 610 NM D) 602 NM 2298. (all) Using the following data, determine the maximum fuel load: DOM: 2.800 kg Trip: 300 kg Payload: 400 kg MTOM: 4.200 kg MLM: 3.700 kg A) 700 kg B) 1.000 kg #C) 800 kg D) 500 kg 12241. (all) (Refer to figure 033-08) A flight has to be made with a multi engine piston aeroplane (MEP 1). For the fuel calculations take 5 US gallons for the taxi, and an additional 13 min at cruise condition to account for climb and descent. Calculated time from overhead to overhead is 1 hrs 47 min. Powersetting is 45%, 2.600 RPM Calculated reserve fuel is 30% of the trip fuel FL100, Temperature -5 °C Find the minimum block fuel: #A) 47 US gallons B) 37 US gallons C) 60 US gallons D) 470 US gallons 24772. (all) Given: DOM: 33.510 kg Traffic load: 7.600 kg Trip fuel: 2.040 kg Final reserve: 983 kg Alternate fuel: 1.100 kg Contingency: 5% of trip fuel Which of the following is correct? A) Landing mass at destination is 43.193 kg. #B) Landing mass at destination is 43.295 kg. C) Takeoff mass is 43.295 kg. D) Takeoff mass is 45.233 kg. 25034. (all) (Refer to figure 033-04) At 6.000 ft what is the range of the aircraft at full throttle with 2.500 RPM set? A) 840 NAM B) 872 NAM C) 914 NAM #D) 756 NAM 25055. (AIR: all) A jet aircraft is due to fly to an isolated aerodrome. The aircraft fuel burn in the cruise is 7.500 kg/hrs and 5.000 kg/ hrs in the hold. What is the absolute minimum additional fuel it should carry? #A) 15.000 kg
B) 10.000 kg C) 3.750 kg D) 5.625 kg 25060. (all) You are required to uplift 40 US Gallons of AVGAS with sp. gravity of 0,72. How many litres and kilograms is this? A) 109 litres, 151 kg. B) 182 litres, 131 kg. C) 182 litres, 289 kg. #D) 151 litres, 109 kg. 25067. (all) (Refer to figure 033-03) On a standard day what is the TAS and fuel flow in USG at 10.000 ft? #A) 157 kts, 11,0 GPH. B) 137 kts, 66,2 GPH. C) 157 kts, 20,7 GPH. D) 157 kts, 11,4 GPH. 033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS 5 © 2008 AVIATIONEXAM.com 25166 (A) 25168 (C) 25186 (B) 1116 (B) 1131 (B) 1132 (B) 1169 (C) 1202 (C) 1301 (B) 25166. (all) (Refer to figure 033-03) Given: Lean mixture 23,0 inHg (or full throttle) at 2.300 RPM FL75 OAT +10 °C Find TAS and fuel flow in gallons per hour: #A) 160 kts, 11,6 GPH. B) 143 kts, 71,1 GPH. C) 160 kts, 68,5 GPH. D) 143 kts, 11,6 GPH. 25168. (all) Given: Dry Operating Mass: 33.000 kg Load: 8.110 kg Final reserve fuel: 983 kg Alternate fuel: 1.100 kg Contingency: 102 kg The estimated landing mass at the alternate aerodrome is: A) 42.210 kg B) 42.312 kg #C) 42.195 kg D) 41.110k g 25186. (all) For a planned flight the calculated fuel is as follows: Flight time: 2 hrs 42 min Block fuel: 136 kg Taxi fuel: 9 kg The reserve fuel, at any time, should be not less than 30% of trip fuel remaining. How many kg of fuel should remain after 2 hrs of flight? A) 33 kg trip and 10 kg reserve. #B) 25 kg trip and 8 kg reserve. C) 23 kg trip and 10 kg reserve.
D) 33 kg trip and no reserve. 033-01-03 Flight monitoring and in-flight replanning 1116. (all) After flying for 16 min at 100 kts TAS with a 20 kts tail wind component, you have to return to the airfield of departure. You will arrive after: A) 20 min. #B) 24 min. C) 10 min 40 sec. D) 16 min. 1131. (all) ATC require a descent from FL270 to FL160 to be level 6 NM before a VOR. If rate of descent is 800 feet per minute, mean groundspeed is 256 kts, how far out from the VOR must descent be started? A) 59 NM #B) 65 NM C) 144 NM D) 150 NM 1132. (all) In the cruise at FL155 at 260 kts TAS, the pilot plans for a 500 ft/min descent in order to fly overhead MAN VOR at 2.000 feet (QNH 1.030). TAS will remain constant during descent, wind is negligible, temperature is standard. The pilot must start the descent at a distance from MAN of: A) 140 NM #B) 120 NM C) 110 NM D) 130 NM 1169. (all) A VFR flight in Piper SENECA III. At a fuel check you have 60 US gallons (USG) of usable fuel remaining. Alternate fuel required is 12 USG. The flight time remaining is 1 hrs 35 min. What is the highest consumption rate acceptable? A) 33,0 USG/hrs B) 37,9 USG/hrs #C) 30,3 USG/hrs D) 21,3 USG/hrs 1202. (all) An aircraft flying at 7.500 ft is cleared to descend to be level at 1.000 ft, 6 NM before reaching a beacon. If ground speed is 156 kts and Rate of Descent is 800 ft/min, how many miles before the beacon should descent begin? A) 15,0 B) 30,2 #C) 27,1 D) 11,1 1301. (all) A descent is planned from 7.500 ft MSL so as to arrive at 1.000 ft MSL 6 NM from a VORTAC. With a GS of 156 kts and a rate of descent of 800 ft/min. The distance from the VORTAC when descent is started is: A) 15,0 NM #B) 27,1 NM C) 11,7 NM D) 30,2 NM 033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS 6 © 2008
AVIATIONEXAM.com 1313 (C) 24740 (D) 24744 (D) 24746 (C) 25053 (A) 25054 (C) 25058 (D) 25104 (A) 25105 (D) 1120 (C) 1192 (A) 1313. (all) Minimum planned takeoff fuel is 160 kg (30% total reserve fuel is included). Assume the groundspeed on this trip is constant. When the aeroplane has done half the distance the remaining fuel is 70 kg. Is diversion to a nearby alternate necessary? A) Diversion to a nearby alternate is not necessary, because it is allowed to calculate without reserve fuel. B) Diversion to a nearby alternate is not necessary, because the reserve fuel has not been used completely. #C) Diversion to a nearby alternate is necessary, because the remaining fuel is not sufficient. D) Diversion to a nearby alternate is necessary, unless the captain decides to continue on his own responsability. 24740. (all) An aircraft is in cruising flight at FL095, IAS 155 kts. The pilot intends to descend at 500 ft/min to arrive overhead the MAN VOR at 2.000 ft (QNH 1.030 hPa). The TAS remains constant in the descent, wind is negligible, temperature standard. At which distance from MAN should the pilot commence the descent? A) 42 NM B) 40 NM C) 45 NM #D) 48 NM 24744. (all) The still air distance in the climb is 189 NAM and time 30 min. What ground distance would be covered in a 30 kts headwind? A) 193 NM B) 203 NM C) 188 NM #D) 174 NM 24746. (all) An aircraft climbs from an airfield, elevation 1.500 ft, QNH 1.023 mb, to FL75. What height does the aircraft have to climb? (Assume 1 mb = 30 ft) A) 6.600 ft B) 7.800 ft #C) 6.300 ft D) 6.000 ft 25053. (all) An aircraft is flying at an indicated pressure altitude of 5.000 ft where the OAT is -10 °C. What is the aircraft s true altitude? #A) 4.750 ft B) 5.260 ft C) 5.120 ft D) 4.600 ft 25054. (all) A mountain 6.011 ft AMSL lies along an aircraft s track of 356° (T), variation 10°W, HDG 355° (M). What is the lowest VFR ICAO level the aircraft may fly to miss the mountain by at least 2.000 ft, QNH 990 hPa (assume 1 hPa = 30 ft)? A) FL075 B) FL090 #C) FL095
D) FL085 25058. (all) An aircraft takes 14 minutes to climb to FL290 covering 71 NAM, what is the ground distanced covered in a 30 kts headwind? A) 71 NGM B) 57 NGM C) 78 NGM #D) 64 NGM 25104. (all) Given: Variation 15°E Deviation 6°W Heading 080° (T) Determine aircraft s compass and magnetic headings: #A) 071, 065 B) 065, 071 C) 086, 095 D) 095, 086 25105. (all) Given: Variation 12°W Deviation 3°E Heading 180° (T) Determine aircraft s compass and magnetic headings: A) 168, 171 B) 168, 165 C) 192, 189 #D) 189, 192 033-01-04 Radio communication and navigation aids 1120. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-01) What navigation or communications facilities are at 48°55 N 009°20 E? A) NDB B) TACAN #C) VOR/DME D) VOR 1192. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-02) Give the frequency of ZURICH Volmet. #A) 127,2 MHz B) 127,2 kHz C) 128,525 MHz D) 118,1 MHz 033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS 7 © 2008 AVIATIONEXAM.com 1205 (A) 12239 (C) 12242 (D) 12243 (D) 12244 (C) 12245 (B) 1205. (all) (Refer to Jeppesen Manual ED-6 or figures ED6-04 and ED6-06) Give the frequency of the GRENCHEN VOR at 47°11 N 007°25 E. #A) 108,65 MHz. B) 326 kHz. C) channel 23. D) 120,1 MHz.
12239. (all) During a flight at night a position has to be reported to ATC. The aeroplane is at a distance of 750 NM from the groundstation and at flight level 350. The frequency to be used is: A) 17.286 kHz B) 123,9 MHz #C) 5.649 kHz D) 1.136 kHz 12242. (all) (Refer to Route Manual chart E (HI)4 CAA-Edition or figure HI-26) The radio navigation aid serving STRASBOURG (48°30 N 007°34 E) is a: A) VOR only, frequency 115,6 MHz. B) DME only, channel 115,6. C) TACAN only, frequency 115,6 MHz. #D) VOR/TACAN, frequency 115,6 MHz. 12243. (all) (Refer to Route Manual chart E (HI)4 CAA-Edition or figure HI-27) The radio navigation aid at ST DIZIER (48°38 N 004°53 E) is a: A) VOR, frequency 114,0 MHz, and TACAN channel 87. B) TACAN, channel 114,0 MHz. C) TACAN, channel 87, and NDB frequency 114,0 kHz. #D) TACAN, channel 87, frequency 114,0 MHz. 12244. (all) (Refer to Route Manual chart E (HI)4 CAA-Edition or figure HI-28) The radio navigation aid on airway UG4 at LUXEUIL (47°41 N 006°18 E) is a: A) VOR/DME and NDB, identifier LXI. B) VOR/DME only, identifier LUL. #C) VOR only, identifier LUL. D) VOR, identifier LUL, frequency paired with TACAN identifier LXI. 12245. (all) (Refer to Route Manual chart E (LO)1 or figure LO-12) The radio navigation aid at BELFAST CITY (54°37N 005°53W) is: A) an NDB, frequency 420 kHz, continuous operation. #B) an NDB, frequency 420 kHz, NOT continuous operation. C) a TACAN, channel 420. D) a fan marker, frequency 420 kHz. 033-02 ICAO ATC FLIGHT PLAN 8 © 2008 AVIATIONEXAM.com 1234 (B) 1237 (D) 1245 (C) 1250 (B) 25030 (C) 1211 (D) 1212 (D) 1213 (D) 1216 (A) 1217 (B) 033-02-01 Types of flight plan 1234. (all) From the options given below select those flights which require flight plan notification: 1) Any Public Transport flight. 2) Any IFR flight. 3) Any flight which is to be carried out in regions which are designated to ease the provision of the Alerting Service or
the operations of Search and Rescue. 4) Any cross-border flights. 5) Any flight which involves overflying water. A) 1, 5 #B) 2, 4 C) 1, 2, 3 D) 3, 4, 5 1237. (all) A current flight plan is a: A) flight plan in the course of which radio communication should be practised between aeroplane and ATC. B) filed flight plan. C) flight plan with the correct time of departure. #D) filed flight plan with amendments and clearance included. 1245. (all) For which flights are Flight Plans required? 1) IFR flights. 2) IFR and VFR flights. 3) Flights crossing national boundaries. 4) Flights over water. 5) Public transport flights. A) 2, 3, 4 B) 1, 3, 5 #C) 1, 3 D) 2, 3, 4, 5 1250. (all) For a repetitive flight plan (RPL) to be used, flights must take place on a regular basis on at least: A) 20 occasions. #B) 10 occasions. C) 30 occasions. D) 50 occasions. 25030. (all) Repetitive flight plans may be used for ___ flights with a high degree of stability over the same days of consecutive weeks on at least ___ occasions. A) IFR; 7 B) VFR; 10 #C) IFR; 10 D) VFR; 7 033-02-02 Completing the flight plan 1211. (all) When completing an ATS flight plan for a European destination, clock times are to be expressed in: A) central European time. B) local mean time. C) local standard time. #D) UTC. 1212. (all) In an ATS flight plan an aircraft will be classified as (L) if its MTOM is: A) 27.000 kg B) 10.000 kg C) 57.000 kg #D) 7.000 kg 1213. (all) (Refer to figure 033-61) In the ATS flight plan Item 15, a cruising speed of 470 kts will be entered as: A) N470
B) KN470 C) 0470K #D) N0470 1216. (all) In the ATS flight plan item 15, when entering a route for which standard departure (SID) and standard arrival (STAR) procedures exist: #A) both should be entered in the ATS plan where appropriate. B) SIDs should be entered but not STARs. C) STARS should be entered but not SIDs. D) neither SID nor STAR should be entered. 1217. (all) When submitting a flight plan before flight, departure time is? A) Overhead the first reporting point. #B) At which the aircraft leaves the parking area. C) Of takeoff. D) At which flight plan is filed. 033-02 ICAO ATC FLIGHT PLAN 9 © 2008 AVIATIONEXAM.com 1221 (D) 1222 (C) 1224 (C) 1226 (B) 1228 (D) 1229 (B) 1230 (A) 1232 (B) 1233 (C) 1235 (B) 1236 (A) 1239 (A) 1240 (D) 1221. (all) An aircraft has a maximum certificated takeoff mass of 137.000 kg but is operating at takeoff mass 135.000 kg. In Item 9 of the ATS flight plan its wake turbulence category is: A) medium plus (M+). B) heavy/medium (H/M). C) medium (M). #D) heavy (H). 1222. (all) The navigation plan reads: Trip fuel: 136 kg Flight time: 2 hrs 45 min Calculated reserve fuel: 30% of trip fuel Fuel in tank is minimum (no extra fuel on board) Taxi fuel: 3 kg The endurance on the ICAO flight plan should read: A) 2 hrs 49 min B) 2 hrs 45 min #C) 3 hrs 34 min D) 3 hrs 38 min 1224. (all) In the appropriate box of a flight plan form, corresponding to the estimated time of departure, the time indicated is that at which the aircraft intends to: A) start-up. B) takeoff. #C) go off blocks. D) pass the departure beacon. 1226. (all) (Refer to figure 033-61) In an ATS flight plan, item 15 (route), a cruising pressure altitude of 32.000 feet would be entered as: A) FL320 #B) F320
C) S3200 D) 32000 1228. (all) An aeroplane is flying from an airport to another. In cruise, the calibrated airspeed is 150 kts, true airspeed 180 kts, average ground speed 210 kts, the speed box on the filed flight plan shall be filled as follows: A) K0150 B) K0210 C) K0180 #D) N0180 1229. (all) When completing an ATS flight plan, an elapsed time (item 16) of 1 hrs 55 min should be entered as: A) 0115 #B) 0155 C) 115M D) 1H55 1230. (all) In the ATS flight plan item 13, in a flight plan submitted before departure, the departure time entered is the: #A) estimated off-block time. B) estimated time over the first point enroute. C) estimated takeoff time. D) allocated slot time. 1232. (all) For the purposes of item 9 (wake turbulence category) of the ATS flight plan, an aircraft with a maximum certificated takeoff mass of 62.000 kg is: A) light (L). #B) medium (M). C) heavy (H). D) unclassified (U). 1233. (all) An aircraft plans to depart London at 1000 UTC and arrive at Munich (EDDM) at 1215 UTC. In the ATS flight plan item 16 (destination / EET) should be entered with: A) EDDM 1215. B) EDDM 1415. #C) EDDM 0215. D) EDDM 2H15. 1235. (all) In the ATS flight plan item 19, if the number of passengers to be carried is not known when the plan is ready for filing: A) the plan should be filed with the relevant box blank. #B) TBN (to be notified) may be entered in the relevant box. C) an estimate may be entered but that number may not subsequently be exceeded. D) the plan may not be filed until the information is available. 1236. (all) In the ATS flight plan, for a non-scheduled flight which of the following letters should be entered in item 8 (type of flight): #A) N B) N/S C) G D) X 1239. (all) In the appropriate box of a flight plan, for endurance, one must indicate the time corresponding to:
#A) the total usable fuel on board. B) the required fuel for the flight. C) the required fuel for the flight plus the alternate and 45 minutes. D) the total usable fuel on board minus reserve fuel. 1240. (all) When completing an ATS flight plan for a flight commencing under IFR but possibly changing to VFR, the letters entered in item 8 (flight rules) would be: A) X B) N/S C) G #D) Y 033-02 ICAO ATC FLIGHT PLAN 10 © 2008 AVIATIONEXAM.com 1243 (C) 1244 (D) 1246 (B) 1249 (B) 1251 (A) 1253 (B) 1257 (C) 1259 (B) 1261 (B) 1262 (D) 1264 (C) 1265 (C) 1347 (C) 1243. (all) The cruising speed to write in the appropriate box of a flight plan is: A) ground speed. B) indicated air speed. #C) true air speed. D) calibrated air speed. 1244. (all) On a flight plan you are required to indicate in the box marked SPEED the planned speed for the first part of the cruise or for the entire cruise. This speed is: A) the estimated ground speed. B) the equivalent airspeed. C) the indicated airspeed. #D) the true airspeed. 1246. (all) In the ATS flight plan Item 15 (cruising speed), when not expressed as a Mach number, cruising speed is expressed as: A) IAS #B) TAS C) CAS D) ground speed 1249. (all) The navigation plan reads: Trip fuel: 100 kg Flight time: 1 hrs 35 min Taxi fuel: 3 kg Block fuel: 181 kg The endurance on the ICAO flight plan should read: A) 1 hrs 35 min #B) 2 hrs 49 min C) 2 hrs 04 min D) 2 hrs 52 min 1251. (all) The maximum permissible takeoff mass of an aircraft for the L wake turbulence category on a flight plan is: #A) 7.000 kg B) 2.700 kg C) 5.700 kg
D) 10.000 kg 1253. (all) In the ATS flight plan item 10 (equipment), the letter to indicate the carriage of a serviceable transponder - mode A (4 digits-4096 codes) and mode C, is: A) B #B) C C) A D) P 1257. (all) In an ATS flight plan item 15, in order to define a position as a bearing and distance from a VOR, the group of figures should consist of: A) VOR ident, magnetic bearing and distance in kilometres. B) VOR ident, true bearing and distance in kilometres. #C) VOR ident, magnetic bearing and distance in nautical miles. D) full name of VOR, true bearing and distance in kilometres. 1259. (all) When filling in a flight plan, wake turbulence category is a function of? A) Maximum certified landing mass. #B) Maximum certified takeoff mass. C) Estimated landing mass. D) Estimated takeoff mass. 1261. (all) When an ATS flight plan is submitted for a flight outside designated ATS routes, points included in item 15 (route) should not normally be at intervals of more than: A) 20 minutes flying time or 150 km. #B) 30 minutes flying time or 370 km. C) 15 minutes flying time or 100 km. D) 1 hour flying time or 500 km. 1262. (all) When a pilot fills in a flight plan, he must indicate the wake turbulence category. This category is a function of which mass? A) Actual takeoff mass. B) Estimated takeoff mass. C) Maximum certified landing mass. #D) Maximum certified takeoff mass. 1264. (all) In the appropriate box of a flight plan form, concerning equipment, the letter to be used to indicate that the aircraft is equipped with a mode A 4096 codes transponder with altitude reporting capability is: A) S B) P #C) C D) A 1265. (all) (Refer to figure 033-61) In an ATS flight plan item 15 (route), in terms of latitude and longitude, a significant point at 41°35 N 4°15 E should be entered as: A) N04135E0415 B) 41°35 N 04° 15 E #C) 4135N00415E D) N4135 E00415 1347. (all)
An aircraft in the cruise has a calibrated airspeed of 150 kts, a true airspeed of 180 kts and an average ground speed of 210 kts. The speed box of the flight plan must be filled as follows: A) K0210 B) N0150 #C) N0180 D) K0180 033-02 ICAO ATC FLIGHT PLAN 11 © 2008 AVIATIONEXAM.com 4306 (A) 4314 (A) 4315 (B) 4316 (B) 4326 (C) 4328 (A) 4332 (B) 4337 (C) 4339 (D) 4343 (A) 4346 (A) 4360 (A) 4306. (all) On an ATC flight plan, an aircraft indicated as H for HEAVY: #A) is of the highest wake turbulence category. B) has a certified landing mass greater than or equal to 136.000 kg. C) has a certified takeoff mass greater than or equal to 140.000 kg. D) requires a runway length of at least 2.000 m at maximum certified takeoff mass. 4314. (all) On a VFR flight plan, the total estimated time is: #A) the estimated time from takeoff to overhead the destination airport. B) the estimated time from takeoff to overhead the destination airport, plus 15 minutes. C) the estimated time from takeoff to landing at the alternate airport. D) the estimated time from engine start to landing at the destination airport. 4315. (all) Total elapsed time for an IFR flight, when filling in the ICAO flight plan at box 16, is the time elapsed from: A) takeoff until landing. #B) takeoff until reaching the IAF (Initial Approach Fix) of the destination aerodrome. C) taxi-out prior to takeoff until taxiing after landing. D) taxiing until the IAF (Initial Approach Fix) of the destination aerodrome. 4316. (all) Given the following flight plan information: Trip fuel: 136 kg Flight time: 2,75 hrs Reserve fuel: 30% of trip Fuel in tanks: minimum Taxi fuel: 3 kg State how endurance should be completed on the ICAO flight plan: A) 0338 #B) 0334 C) 0245 D) 0249 4326. (all) The navigation plan reads: Trip fuel: 100 kg
Flight time: 1 hrs 35 min Taxi fuel: 3 kg Block fuel: 181 kg How should endurance be shown on the flight plan? A) 0204 B) 0240 #C) 0249 D) 0252 4328. (all) On an ATC flight plan, the letter Y is used to indicate that the flight is carried out under the following flight rules: #A) IFR followed by VFR. B) VFR followed by IFR. C) IFR. D) VFR. 4332. (all) On a ATC flight plan, to indicate that you will overfly the way-point ROMEO at 120 kts at flight level 085, you will write: A) ROMEO / K0120 FL085. #B) ROMEO / N0120 F085. C) ROMEO / FL085 N0120. D) ROMEO / F085 N0120. 4337. (all) Reference item 19 of the ICAO flight plan, endurance is? A) Maximum flight time plus 45 minutes holding fuel. B) Maximum flight time plus 30 minutes holding fuel. #C) Fuel endurance of the aircraft. D) Total usable fuel required for the flight. 4339. (all) In the event that SELCAL is prescribed by an appropriate authority, in which section of the ATS flight plan will the SELCAL code be entered? A) Equipment. B) Route. C) Aircraft identification. #D) Other information. 4343. (all) For a radio equipped aircraft, the identifier in the ATS flight plan item 7 must always: #A) be the RTF callsign to be used. B) include the aircraft registration. C) include the operating agency designator. D) include an indication of the aircraft type. 4346. (all) You have a mode A transponder (4 digits, 4.096 codes) and mode C. Item 10 of the flight plan should show: #A) C B) A C) P D) S 4360. (all) Prior to an IFR flight, when filling in the ICAO flight plan, the time information which should be entered in box 16 (total elapsed time) is the time elapsed from: #A) takeoff until reaching the IAF (initial approach fix) of the destination aerodrome. B) taxi out prior to takeoff until the IAF. C) takeoff until landing. D) taxi-out prior to takeoff until completion off taxi-ing after
landing. 033-02 ICAO ATC FLIGHT PLAN 12 © 2008 AVIATIONEXAM.com 4361 (B) 4364 (D) 4366 (C) 4368 (C) 4369 (B) 12524 (B) 12529 (A) 12530 (A) 12531 (C) 12532 (B) 14186 (A) 22882 (A) 24765 (A) 4361. (all) On an ATC flight plan, to indicate that you will overfly the waypoint TANGO at 350 kts at flight level 280, you write: A) TANGO / K0350 FL280 #B) TANGO / N0350 F280 C) TANGO / FL280 N0350 D) TANGO / KT350 F280 4364. (all) If the destination airport has no ICAO indicator, in box 16 of your ATS flight plan, you write: A) //// B) AAAA C) XXXX #D) ZZZZ 4366. (all) (Refer to figure 033-61) Item 7 of the flight plan in accordance with PANS-RAC (DOC 4444) should always include, for an aircraft equipped with a radio: A) aircraft initialisation. B) aircraft type. #C) aircraft callsign. D) aircraft operator. 4368. (all) Reference the ICAO flight plan, in item 15 (speed) this speed refers to: A) indicated airspeed. B) equivalent airspeed. #C) initial cruising true airspeed. D) calculated ground speed. 4369. (all) (Refer to figure 033-61) When filling in item 9 of the flight plan and there is no aircraft designator listed, what should the entry be? A) None. #B) ZZZZ followed by an entry at item 18. C) XXXX followed by an entry at item 18. D) A descriptive abbreviation of the aircraft type. 12524. (all) (Refer to figure 033-61) Prior to an IFR fligt, when filling in the ICAO flight plan, the time information which should be entered in box 13 (time) is: A) the time of flight plan filing. #B) estimated off-block time. C) planned takeoff time. D) planned engine start time. 12529. (all) (Refer to figure 033-61) In the ATS flight plan item 10 (standard equipment) is considered to be: #A) VHF RTF, ADF, VOR and ILS.
B) VHF RTF, ADF, VOR and transponder. C) VHF RTF, VOR and transponder. D) VHF RTF, VOR, ILS and transponder. 12530. (all) (Refer to figure 033-61) In the ATS flight plan Item 15, for a flight along a designated route, where the departure aerodrome is not on or connected, to that route: #A) the letters DCT should be entered, followed by the point of joining the ATS route. B) it is necessary only to give the first reporting point on that route. C) the words AS CLEARED should be entered. D) it is not necessary to indicate the point of joining that route as it will be obvious to the ATS unit. 12531. (all) (Refer to figure 033-61) In the ATS flight plan item 19, emergency and survival equipment carried on the flight should be indicated by: A) placing a tick in the relevant box. B) listing the items carried on the REMARKS line. #C) crossing out the box relevant to any equipment not carried. D) circling the relevant box. 12532. (all) (Refer to figure 033-61) Item 9 of the ATS flight plan includes NUMBER AND TYPE OF AIRCRAFT. In this case, the NUMBER means: A) the ICAO type designator number as set out in ICAO Doc 8643. #B) the number of aircraft flying in a group. C) the registration number of the aircraft. D) the number of aircraft which will separately be using a repetitive flight plan (RPL). 14186. (all) An aircraft has: Maximum Certificated Takeoff Mass: 137.000 kg Actual Takeoff Mass: 135.000 kg Which wake turbulence category should be entered in item 9? #A) Heavy (H). B) Medium (M). C) Medium/Heavy (M/H). D) Heavy/Medium (H/M). 22882. (all) For a flight plan filed before the flight, the indicated time of departure is: #A) the estimated off-block time. B) the time at which the flight plan is filed. C) the time of takeoff. D) the time overhead the first reporting point after takeoff. 24765. (all) What is the maximum estimated elapsed time or distance between points on track mentioned in Item15 of the flight plan, for flights outside designated ATS routes? #A) 30 min / 200 NM. B) 60 min / 370 NM. C) 90 min / 370 km. D) 120 min / 370 NM. 033-02 ICAO ATC FLIGHT PLAN
13 © 2008 AVIATIONEXAM.com 24766 (B) 25044 (C) 25045 (B) 25175 (B) 28346 (D) 1209 (C) 1231 (D) 1256 (B) 1263 (D) 1267 (D) 24902 (D) 24766. (all) Given: Trip fuel: 100 kg Planned flight time: 1 hrs 30 min Taxi fuel: 3 kg Block fuel: 181 kg How should endurance be shown on the flight plan? A) 0204 #B) 0240 C) 0249 D) 0252 25044. (all) Your aircraft has a maximum certified takeoff mass of 140.000 kg. Today your calculated takeoff mass is 130.000 kg. What letter should appear in the wake turbulence category on the flight plan form? A) Leave blank B) L #C) H D) M 25045. (all) Your initial cruising speed and level are 300 kts and flight level 250 at position STP on airway B3 you plan to climb to flight level 330 and increase speed to 350 kts. How should this change be shown in box 15 on the flight plan form? A) N0300 F250 from STP N0350 F330 B3. #B) STP/N0350F330 B3. C) STP/N0330F350 B3. D) STP/N0350F330 25175. (all) The cruising speed in item 15 of an ATS flight plan is: A) Indicated Air Speed. #B) True Air Speed. C) Ground Speed. D) Calibrated Air Speed. 28346. (AIR: atpl) Your aircraft is approved for MNPS and RVSM. What do you have to insert in item 10 of the ATC flight plan? A) W B) Y C) X #D) W, X 033-02-03 Filing the flight plan 1209. (all) It is possible, in flight, to: 1) File an IFR flight plan 2) Modify an active IFR or VFR flight plan 3) Cancel an active VFR flight plan 4) Close an active VFR flight plan Which of the following combinations contains all of the correct statements? A) 1, 2, 4 B) 1, 2, 3 #C) 1, 2, 3, 4 D) 2, 3, 4
1231. (all) Which of the following statements regarding filing a flight plan is correct? A) A flying college can file repetitive flight plan for VFR flights. B) Any flight plan should be filed at least 10 minutes before departure. C) A flight plan should be filed when a national FIR boundary will be crossed. #D) In case of ATFM (Air Traffic Flow Management) the flight plan should be filed at least three hours in advance of the EOBT. 1256. (all) How many hours in advance of departure time should a flight plan be filed in the case of flights into areas subject to air traffic flow management (ATFM)? A) 1:00 hour. #B) 3:00 hours. C) 0:30 hours. D) 0:10 hours. 1263. (all) The planned departure time from the parking area is 1815 UTC. The estimated takeoff time is 1825 UTC. The IFR flight plan must be filed with ATC at the latest at: A) 1755 UTC B) 1725 UTC C) 1745 UTC #D) 1715 UTC 1267. (all) A repetitive flight plan (RPL) is filed for a scheduled flight: Paris Orly to Angouleme, Paris Orly as alternate. Following heavy snow falls, Angouleme airport will be closed at the expected time of arrival. The airline decides before departure to plan a re-routing of that flight to Limoges. A) The pilot-in-command must advise ATC of his intention to divert to Limoges at least 15 minutes before the planned time of arrival. B) The airline s Operations Department has to tansmit a change in the RPL at the ATC office, at least half an hour before the planned time of departure. C) It is not possible to plan another destination and the fIight has to be simply cancelled that day (scheduled flight and not chartered). #D) The RPL must be cancelled for that day and a specific flight plan has to be filed. 24902. (AIR: all) For an intercontinental flight routed via the North Atlantic system, how long before start up is requested should your flight plan have been filed? A) 30 min B) 6 hrs C) 60 min #D) 3 hrs 033-02 ICAO ATC FLIGHT PLAN 14 © 2008 AVIATIONEXAM.com 25056 (B) 1219 (C) 1238 (B) 1254 (A) 1210 (C) 1214 (D) 1248 (B) 1255 (C) 1258 (C) 1260 (B)
25056. (all) An aircraft has a flight time of 2 hrs 30 min, a contingency fuel of 30% is carried. What is the total endurance? A) 1 hr 55 min #B) 3 hrs 15 min C) 3 hrs D) 2 hrs 30 min 1254. (all) An aeroplane is on an IFR flight. The flight is to be changed from IFR to VFR. Is it possible? A) Yes, the pilot in command must inform ATC using the phrase cancelling my IFR flight . B) No, you have to remain IFR in accordance to the filed flight plan. #C) No, only ATC can order you to do this. D) Yes, but only with permission from ATC. 033-02-04 Closing the flight plan 1219. (all) You make a diversion from the route given in the flight plan and land at an uncontrolled airfield. Within what time after landing should you inform ATC? A) 10 min #B) 20 min C) 30 min D) 45 min 1238. (all) If a pilot lands at an aerodrome other than the destination aerodrome specified in the flight plan, he must ensure that the ATS unit at the destination aerodrome is informed within a certain number of minutes of his planned ETA at destination. This number of minutes is: #A) 10 B) 30 C) 15 D) 45 033-02-05 Adherence to flight plan 1210. (all) During an IFR flight TAS and time appear to deviate from the data in the flight plan. The minimum deviations, that should be reported to ATC in order to conform to PANSRAC, are: A) TAS 5 kts and time 5 minutes. B) TAS 3% and time 3 minutes. #C) TAS 5% and time 3 minutes. D) TAS 10 kts and time 2 minutes. 1214. (all) When an ATS flight plan has been submitted for a controlled flight, the flight plan should be amended or cancelled in the event of the off-block time being delayed by: A) 90 minutes or more. B) 45 minutes or more. C) 60 minutes or more. #D) 30 minutes or more. 1248. (all) If a pilot lands at an aerodrome other than the destination aerodrome specified in the ICAO flight plan, he must ensure that the ATS unit at the destination is informed within a specified time of his planned ETA at destination. The time is: A) 45 min
#B) 30 min C) 15 min D) 10 min 1255. (all) In the ATS flight plan item 15, it is necessary to enter any point at which a change of cruising speed takes place. For this purpose a CHANGE OF SPEED is defined as: A) 20 km/h or Mach 0,1 or more. B) 10% TAS or Mach 0,05 or more. #C) 5% TAS or Mach 0,01 or more. D) 20 kts or Mach 0,05 or more. 1258. (all) You have filed a flight plan for an uncontrolled flight and suffer a delay prior to departure. After how long a delay must you restate your OBT? A) 30 min B) 40 min #C) 60 min D) 90 min 1260. (all) In flight, it is possible to: 1) File an IFR flight plan. 2) Modify an active flight plan. 3) Cancel aVFR flight plan. 4) Close a VFR flight plan. A) 1, 3 #B) 1, 2, 3, 4 C) 2, 3, 4 D) 1, 4 033-02 ICAO ATC FLIGHT PLAN 15 © 2008 AVIATIONEXAM.com 1266 (A) 24764 (C) 1266. (all) You have a flight plan IFR from Amsterdam to London. In the flight plan it is noted that you will deviate from the ATS route passing the FIR boundary Amsterdam/London. The airway clearance reads Cleared to London via flight planned route . Which of the following statements is correct? #A) The route according to the flight plan is accepted. B) The filed deviation is not accepted. C) You will get a separate clearance for the deviation. D) It is not allowed to file such a flight plan. 24764. (all) If your speed, in flight, changes from that given in the flight plan, you should notify ATC for changes of more than: A) 5% TAS / ETA 5 min. B) 3% TAS / ETA 3 min. #C) 5% TAS / ETA 3 min. D) 3% TAS / ETA 5 min. 033-03 PRACTICAL FLIGHT PLANNING 16 © 2008 AVIATIONEXAM.com 1167 (C) 1181 (D) 1185 (B) 1191 (D) 1252 (B) 1276 (C) 1286 (B) 4340 (D) 12270 (C) 12271 (A) 12272 (D) 23750 (A) 033-03-01 Chart preparation
1167. (all) (Refer to Jeppesen Manual ED-6 or fugure ED6-03) Flying VFR from VILLINGEN (48°03,5 N, 008°27,0 E) to FREUDENSTADT (48°28,0 N, 008°24,0 E), determine the distance: A) 54 NM B) 29 km #C) 24 NM D) 33 NM 1181. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-04) The GRENCHEN LSZG aerodrome (47°11 N 007°25 E) has a tower frequency of 120,10 MHz. The (V) after the frequency indicates: A) available on request. B) only to be used during daylight. C) available for VFR flight only. #D) VDF available. 1185. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-05) What navigation or communications facilities are at 48°23 N 008°39 E? A) NDB #B) VOR C) VOR/DME D) VORTAC 1191. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-07) An aeroplane is flying VFR and approaching position TANGO (48°37 N 009°16 E) at FL55 and on a magnetic track of 090. The distance from TANGO is 20 NM. The navigation aid and frequency at TANGO is: A) VORTAC 112,50 kHz. B) DME 112,50 MHz. C) VOR 112,50 with no DME. #D) VORTAC 112,50 MHz. 1252. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-08) Flying VFR from PEITING (47°48 N 010°55,5 E) to IMMENSTADT (47°33,5 N 010°13,0 E) determine the magnetic course. A) 077 #B) 243 C) 257 D) 063 1276. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-09) Flying from position ERBACH (48°21 N 009°55 E) to POLTRINGEN airport (48°33 N 008°57 E). Find the magnetic course and distance. A) 108° / 60 NM. B) 252° / 41 NM. #C) 287° / 41 NM. D) 287° / 60 NM. 1286. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-10) Flying from position SIGMARINGEN (48°05 N 009°13 E) to BIBERACH airport (48°07 N 009°46 E). Find the magnetic course and distance. A) 093° / 41 NM.
#B) 086° / 22 NM. C) 267° / 22 NM. D) 086° / 32 NM. 4340. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-03) Flying VFR from VILLINGEN (48°03,5 N 008°27,0 E) to FREUDENSTADT (48°28,0 N 008°24,0 E), determine the magnetic course: A) 176° B) 004° C) 185° #D) 356° 12270. (all) (Refer to Route Manual VFR+GPS chart ED-6 or figure ED6-03) Flying VFR from VILLINGEN (48°03,5 N 008°27,0 E) to FREUDENSTADT (48°28,0 N 008°24,0 E). Determine the minimum altitude within a corridor 5 NM left and 5 NM right of the courseline in order to stay 1.000 ft clear of obstacles. A) 4.200 ft B) 1.500 ft #C) 3.900 ft D) 2.900 ft 12271. (all) (Refer to Route Manual VFR+GPS chart ED-6 or figure ED6-08) Flying VFR from PEITING (47°48,0 N 010°55,5 E) to IMMENSTADT (47°33,5 N 010°13,0 E). Determine the distance. #A) 32 NM B) 46 NM C) 58 NM D) 36 NM 12272. (all) (Refer to Route Manual VFR+GPS chart ED-6 or figure ED6-08) Flying VFR from PEITING (47°48,0 N 010°55,5 E) to IMMENSTADT (47°33,5 N 010°13,0 E). Determine the minimum altitude within a corridor 5 NM left and 5 NM right of the courseline in order to stay 1.000 ft clear of obstacles. A) 5.500 ft B) 6.600 ft C) 5.300 ft #D) 6.900 ft 23750. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon) Approach chart (29-1) or figure VFR-10) What is the variation shown on the chart? #A) 3°E B) 3°W C) 5°E D) 5°W 033-03 PRACTICAL FLIGHT PLANNING 17 © 2008 AVIATIONEXAM.com 23751 (B) 23753 (B) 23754 (A) 23755 (C) 23756 (D) 23757 (C) 23758 (C) 23759 (C) 23760 (A) 23761 (A) 23762 (D) 23751. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM (VFR), Aberdeen
(Dyce) Area chart (10-1V) or figure VFR-1) What is the elevation of the highest ground within the boundary of Aberdeen Control Zone? A) 1.245 ft #B) 1.733 ft C) 2.105 ft D) 2.025 ft 23753. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) What is elevation of LSZH ZURICH KLOTHEN airport (47°28 N, 008°33 E)? A) 1.000 m #B) 1.416 ft C) 1.421 ft D) 1.572 ft 23754. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Flying from EDPJ LAICHINGEN airport (48°30 N 009°38 E) to EDSZ ROTTWEIL ZEPFENHAN (48°12 N 008°44 E). Find magnetic course and the distance. #A) Magnetic course 243°, distance 41 NM. B) Magnetic course 063°, distance 41 NM. C) Magnetic course 063°, distance 62 NM. D) Magnetic course 243°, distance 62 NM. 23755. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Flying from EDPJ LAICHINGEN airport (48°30 N 009°38 E) to EDTM MELGEN airport (48°03 N 009°22 E). Find magnetic course and the distance. A) Magnetic course 022°, distance 44 NM. B) Magnetic course 022°, distance 28 NM. #C) Magnetic course 202°, distance 28 NM. D) Magnetic course 202°, distance 44 NM. 23756. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Flying from EDSZ ROTTWEIL ZEPFENHAN (48°12 N 008°44 E) to EDPJ LAICHINGEN airport (48°30 N 009°38 E). Determine the highest obstacle within a corridor 5NM left and right from track. A) 2.852 ft B) 3.612 ft C) 3.278 ft #D) 3.760 ft 23757. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Flying from EDSZ ROTTWEIL ZEPFENHAN (48°12 N 008°44 E) to EDPJ LAICHINGEN airport (48°30 N 009°38 E). Find magnetic course and the distance. A) Magnetic course 063°, distance 62 NM. B) Magnetic course 243°, distance 41 NM. #C) Magnetic course 063°, distance 41 NM. D) Magnetic course 243°, distance 62 NM. 23758. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6)
Flying from EDSZ ROTTWEIL ZEPFENHAN (48°12 N 008°44 E) to EDTM MENGEN airport (48°03 N 009°22 E). Determine the highest obstacle within a corridor 5NM left and 5 NM right of track. A) 2.920 ft B) 3.331 ft #C) 3.760 ft D) 2.605 ft 23759. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Flying from EDSZ ROTTWEIL ZEPFENHAN (48°12 N 008°44 E) to EDTM MENGEN airport (48°03 N 009°22 E). Find magnetic course and the distance. A) Magnetic course 108°, distance 40 NM. B) Magnetic course 288°, distance 27 NM. #C) Magnetic course 108°, distance 27 NM. D) Magnetic course 288°, distance 40 NM. 23760. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Flying from EDTM MELGEN airport (48°03 N 009°22 E) to EDSZ ROTTWEIL ZEPFENHAN (48°12 N 008°44 E). Find magnetic course and the distance. #A) Magnetic course 288°, distance 27 NM. B) Magnetic course 108°, distance 27 NM. C) Magnetic course 108°, distance 40 NM. D) Magnetic course 288°, distance 40 NM. 23761. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Flying from EDTM MENGEN airport (48°03 N 009°22 E) to EDPJ LAICHINGEN airport (48°30 N 009°38 E). Determine the highest obstacle within a corridor 5NM left and 5 NM right from track. #A) 2.870 ft B) 2.838 ft C) 2.507 ft D) 2.120 ft 23762. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Flying from EDTM MENGEN airport (48°03 N 009°22 E) to EDPJ LAICHINGEN airport (48°30 N 009°38 E). Find magnetic course and the distance. A) Magnetic course 202°, distance 44 NM. B) Magnetic course 202°, distance 28 NM. C) Magnetic course 022°, distance 44 NM. #D) Magnetic course 022°, distance 28 NM. 033-03 PRACTICAL FLIGHT PLANNING 18 © 2008 AVIATIONEXAM.com 23763 (C) 23764 (B) 23765 (B) 23767 (B) 23802 (A) 23803 (A) 23804 (B) 23805 (C) 23806 (D) 23807 (B) 23808 (B) 23809 (A) 23763. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Name the frequency of TANGO VORTAC (48°37 N
009°16 E): A) 118,60 MHz B) 422 kHz #C) 112,50 MHz D) 118,80 MHz 23764. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) What minimum grid area altitude is applicable for EDPJ LAICHINGEN airport (48°30 N 009°38 E)? A) 46 #B) 43 C) 2.434 ft D) 402 m 23765. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) What minimum grid area altitude is applicable for EDTM MENGEN airport (48°03 N, 009°22 E)? A) 43 #B) 46 C) 1819 ft. D) 1120 m. 23767. (all) (Refer to Jeppesen Student Route Manual VFR+GPS chart ED-6) Which navigation aid is located in position 48°55 N 009°20 E? A) NDB #B) VOR/DME C) TACAN D) VOR 23802. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Sabadell Area chart (19-1) or figure VFR-12) What is the published frequency for Barcelona ATIS? #A) 118,65 MHz B) 119,10 MHz C) 124,70 MHz D) 120,80 MHz 23803. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Sabadell Aerodrome chart (19-2) or figure VFR-13) What is the published initial VFR arrival procedure for helicopters? #A) From the southwest. B) From reporting point N or E. C) From Sant Cugat del Vallis. D) From reporting point MARTORELL or MOLLET. 23804. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Barcelona Area chart (10-1V) or figure VFR-16) If routeing along the Barcelona VFR corridors from Reus REP to SAN CELONI, what is the maximum altitude available without changing? A) 3.000 ft #B) 2.000 ft C) 4.500 ft D) 3.500 ft 23805. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon)
Approach chart (29-1) or figure VFR-10) What is the published frequency to use for start up? A) Approach 119,10. B) Tower 118,10. #C) Ground 121,70. D) ATIS 123,40. 23806. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon) Approach chart (29-1) or figure VFR-10) What is the frequency and ident of the DVOR/DME shown at the northern end of Hellinikon airfield? A) 294 HN B) 357 KVR C) 275 HK #D) 114,40 ATH 23807. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon) Approach chart (29-1) or figure VFR-10) What is the total distance when following the VFR routeing from Abeam Patroklos to Hellinikon? A) 19 km #B) 19 NM C) 14 NM D) 16 NM 23808. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon) Area chart (29-1) or figure VFR-10) What is the maximum permitted altitude if routeing inbound from Abeam Patroklos to Hellinikon? A) 1.500 ft #B) 300 ft C) 4.000 ft D) 322 ft 23809. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon) Landing Chart (29-2) or figure VFR-11) What is the position of the Aerodrome Reference Point? #A) 37°53,8 N 23°43,7 E B) 37°54,2 N 23°44,3 E C) 37°53,2 N 23°43,3 E D) 37°54,8 N 23°44,7 E 033-03 PRACTICAL FLIGHT PLANNING 19 © 2008 AVIATIONEXAM.com 23810 (D) 23813 (D) 23814 (D) 23815 (B) 23816 (A) 23817 (A) 23818 (A) 23819 (D) 23820 (A) 23821 (B) 23822 (C) 23823 (A) 23810. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon) Aerodrome chart (29-2) or figure VFR-11) What are the available outbound tracks for helicopters from the helicopter landing point at approximately 37°54 N 23°44 E? A) 215° or 035°. B) 245° or 035°. C) 065° or 245°. #D) 065° or 215°. 23813. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce)
Information Page (19-6) or figure VFR-2) Which of the Helicopter Routes in the Aberdeen CTR is the designated low visibility/bad weather route? A) H4 B) H1 C) H2 #D) H6 23814. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, De Kooy Aerodrome chart (19-2) or figure VFR-8) How many Helicopter landing points are shown on the chart for De Kooy Aerodrome? A) Fifteen (15) B) Four (4) C) Two (2) #D) Six (6) 23815. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, De Kooy Area chart (19-1) or figure VFR-7) What is (i) the frequency and (ii) QDM of the ILS at De Kooy Aerodrome? A) (i) 123,30; (ii) 220° (M) #B) (i) 109,70; (ii) 216° (M) C) (i) 109,70; (ii) 214° (T) D) (i) 123,30; (ii) 220° (T) 23816. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, De Kooy Area chart (19-1) or figure VFR-7) What is the minimum altitude over the Quiet Zone in the vicinity of De Kooy? #A) 1.500 ft B) 3.500 ft C) 3.000 ft D) 32.800 ft 23817. (HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce) Information Page (19-6) or figure VFR-2) According to the Helicopter Local Flying Regulations , approaches to the Helistrip 23 aiming point should be on a heading of: #A) 218° (M) B) 230° (M) C) 228° (M) D) 218° (T) 23818. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce) Information Page (19-6) or figure VFR-2) What are the designated departure routes when using (i) Rwy 34 and (ii) Rwy 05? #A) (i) H2; (ii) H4 B) (i) H6; (ii) H2 C) (i) H1; (ii) H3 D) (i) H5; (ii) H1 23819. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce) Information Page (19-6) or figure VFR-2) What is the designated departure route when using Runway 23 in bad weather and/or low visibility? A) H5 B) H3
#C) H1 D) H6 23820. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce) Information Page (19-6) or figure VFR-2) What is the minimum flight visibility required when landing at Aberdeen (Dyce) Airport other than when using Route H6? #A) 2 km B) 3 km C) 4 km D) 5 km 23821. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce) Area chart (19-5) or figure VFR-3) What ATIS frequency(ies) is/are available when on the ground? A) 121,85 only. #B) 114,30 or 121,85. C) 121,70 only. D) 121,70 or 121,85. 23822. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce) Area chart (19-5) or figure VFR-3) What is the ATIS frequency that may not be used when in flight? A) 121,70 B) 114,30 #C) 121,85 D) 118,10 23823. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Aberdeen Information Page (19-3) or figure VFR-4) The East Apron and Eastern Twy have restricted access. The maximum permitted wingspan: #A) is 20 m. B) is the same as a Beech 200. C) is 20 ft. D) does not apply to helicopters. 033-03 PRACTICAL FLIGHT PLANNING 20 © 2008 AVIATIONEXAM.com 23824 (A) 23825 (C) 23826 (A) 23827 (B) 23828 (B) 24742 (D) 24748 (C) 24896 (B) 25046 (A) 25562 (C) 25563 (B) 25564 (D) 25565 (C) 23824. (HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Aberdeen Aerodrome chart (19-2) or figure VFR-5) How many runways are available for use by helicopters? #A) Seven (7) B) Five (5) C) Six (6) D) Two (2) 23825. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM (VFR) , Aberdeen (Dyce) Area chart (10-1V) or figure VFR-1) What is the elevation of the highest obstacle within the boundary of Aberdeen Control Area? A) 2.025 ft
B) 1.245 ft #C) 2.105 ft D) 1.733 ft 23826. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM (VFR), Aberdeen (Dyce) Area chart (10-1V) or figure VFR-1) Which of the following frequencies is listed as available for contact with Aberdeen ATSU? #A) 135,17 B) 126,25 C) 119,87 D) 114,30 23827. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM (VFR), Aberdeen (Dyce) Area chart (10-1V) or figure VFR-1) What is the correct frequency to contact Scottish Information when overhead reporting point BANCHORY to the southwest of Aberdeen Airport? A) 126,25 #B) 119,87 C) 134,10 D) 135,17 23828. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM (VFR), Aberdeen (Dyce) Area chart (10-1V) or figure VFR-1) What is the elevation of the highest ground within the boundary of Aberdeen Control Area? A) 2.105 ft. #B) 2.025 ft. C) 1.733 ft. D) 1.245 ft. 24742. (all) (Refer to Jeppesen Manual ED-6) What is the navaid at 48°30 N 007°34 E? A) VORTAC/NDB B) NDB C) TACAN #D) VOR/DME 24748. (all) (Refer to Jeppesen Manual - chart ED-6) You are at position 47°59 N 010°15 E. Which Flight Information Service should you contact? A) Memmingen 117,20 Mhz. B) Memmingem 135,60 Mhz. #C) Munchen 126,95 Mhz. D) Munchen 131,22 MHz. 24896. (all) (Refer to Jeppesen Manual chart ED-6) STUTTGART airport (48°41 N 009°11 E) is within what sort of airspace: A) class E. #B) class D. C) class A. D) class G. 25046. (all) (Refer to Jeppesen Student Manual - chart ED-6) What is the main true track and distance from TRA (47°42 N 008°26 E) to KPT (47°45 N 010°21 E)? #A) 087° / 143 km B) 267° / 78 NM
C) 087° / 88 NM D) 091° / 76 NM 25562. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Esbjerg Aerodrome chart (19-2) or figure VFR-15) What are the dimensions of runway 08/26 at Esbjerg? A) 8.530 ft x 45 ft B) 8.530 m x 45 m #C) 2.600 m x 45 m D) 2.600 ft x 148 ft 25563. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Esbjerg Aerodrome chart (19-2) or figure VFR-15) What is the position of the Aerodrome Reference Point at Esbjerg? A) 55°31,6 N 008°33,1 W #B) 55°31,6 N 008°33,1 E C) 55°32,2 N 008°34,9 E D) 55°32,2 N 008°34,9 W 25564. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Esbjerg Area chart (19-1) or figure VFR-14) What is the course and distance from Locator HP to the threshold of Runway 08? A) 080° (T) / 4,2 km. B) 080° (T) / 4,2 NM. C) 080° (M) / 4,2 km. #D) 080° (M) / 4,2 NM. 25565. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, Esbjerg Area chart (19-1) or figure VFR-14). What is the track and distance shown on the chart from VOR/DME SKR (55°13,8 N 009°12,9 E to overhead Esbjerg (55°31,6 N 008°33,2 E)? A) 308° (T) / 29 NM. B) 308° (M) / 29 km. #C) 308° (M) / 29 NM. D) 308° (T) / 29 km. 033-03 PRACTICAL FLIGHT PLANNING 21 © 2008 AVIATIONEXAM.com 25566 (B) 25567 (A) 4348 (A) 12268 (D) 14444 (A) 25012 (B) 1126 (C) 1127 (D) 12525 (D) 12528 (B) 25566. (AIR: atpl, cpl; HELI: atpl, cpl) (Refer to Jeppesen Student Manual - TRM, The Netherlands Aerodrome Directory (7-3) or figure VFR-6) What is the local time (LT) in the Netherlands in (i) Winter and (ii) Summer? A) (i) LT - 2 Hours = UTC; (ii) LT - 1 Hour = UTC #B) (i) LT - 1 Hour = UTC; (ii) LT - 2 Hours = UTC C) (i) LT = UTC + 2 Hours; (ii) LT = UTC + 1 Hour D) (i) LT = UTC - 1 Hour; (ii) LT = UTC - 2 Hours 25567. (AIR: atpl, cpl; HELI: atpl, cpl) Refer to Jeppesen Student Manual - TRM, Greece Aerodrome Directory (7-3) or figure VFR-9) What is the local time (LT) in Greece in (i) Winter and (ii) Summer? #A) (i) LT = UTC + 2 Hours; (ii) LT = UTC + 3 Hours
B) (i) LT = UTC - 2 Hours; (ii) LT = UTC - 3 Hours C) (i) LT + 2 Hours = UTC; (ii) LT + 3 Hours = UTC D) (i) LT - 3 Hours = UTC; (ii) LT - 2 Hours = UTC 033-03-02 Navigation plans 4348. (all) What is Total Elapsed Time on a VFR flight plan? #A) From takeoff to overhead destination. B) From takeoff to overhead destination + 15 mins. C) From takeoff to landing. D) From taxi to arrival on the gate. 12268. (all) (Refer to Route Manual VFR+GPS chart ED-6 or figure ED6-12) Flying from SAULGAU airport (48°02 N 009°31 E) to ALTENSTADT airport (47°50 N 010°53 E). Find magnetic course and the distance. A) Magnetic course 282°, distance 56 NM. B) Magnetic course 102°, distance 82 NM. C) Magnetic course 078°, distance 82 NM. #D) Magnetic course 102°, distance 56 NM. 14444. (all) An aircraft flight planning chart states that the time to reach FL190 at a given gross mass is 22 minutes with a still air distance of 66 NM. The ground distance travelled when the average headwind component is 35 kts will be: #A) 53 NM B) 61 NM C) 79 NM D) 85 NM 25012. (AIR: all) At 1000 UTC Shanwick Oceanic clear you to enter the Oceanic control Area at 47°00 N 008°W, 220 track miles from your current position, at time 1033 UTC. At FL200, ISA conditions and with TAS 430 kts, headwind 30 kts, FMS being unavailable, what is the required Mach number to comply with this instruction? A) M 0,75 #B) M 0,70 C) M 0,60 D) M 0,80 033-03-03 Simple fuel plans 1126. (AIR: all) In a flight plan when the destination aerodrome is A and the alternate aerodrome is B, the final reserve fuel for a turbojet engine aeroplane corresponds to: A) 15 minutes holding 2.000 feet above aerodrome A. B) 30 minutes holding 2.000 feet above aerodrome B. #C) 30 minutes holding 1.500 feet above aerodrome B. D) 30 minutes holding 1.500 feeI above aerodrome A. 1127. (AIR: atpl, cpl; HELI: atpl, cpl) Given: Dry operating mass (DOM): 33.000 kg Load: 8.110 kg Final reserve fuel: 983 kg Alternate fuel: 1.100 kg Contingency fuel: 102 kg The estimated landing mass at alternate should be: A) 42.312 kg B) 41.110 kg C) 42.210 kg
#D) 42.195 kg 12525. (all) A helicopter is on a 150 NM leg to an off-shore oil rig. Its TAS is 130 kts with a 20 kts tailwind, its endurance is 3 hrs 30 min without reserve. Upon reaching destination, it is asked to proceed outbound to locate a ship in distress, on a track which gives a 15 kts tailwind. Maintaining zero reserve on return to the oil rig, the helicopter can fly outbound for distance of: A) 224,5 NM B) 158,6 NM C) 222,1 NM ##D) 160,3 NM 12528. (all) You are to determine the maximum fuel load which can be carried in the following conditions: - dry operating mass: 2.800 kg - trip fuel: 300 kg - payload: 400 kg - maximum takeoff mass: 4.200 kg - maximum landing mass: 3.700 kg A) 500 kg #B) 800 kg C) 1.000 kg D) 700 kg 033-03 PRACTICAL FLIGHT PLANNING 22 © 2008 AVIATIONEXAM.com 24752 (B) 1165 (A) 12267 (B) 12269 (D) 24752. (all) (Refer to figure 033-08) Given: Trip time 2 hrs 37 min from departure to destination at 2.500 RPM, 65% power. For the climb and descent add 13 min of cruise fuel. Reserve = 30% of trip fuel. Taxy fuel is 5 US gal. What is the min Ramp Fuel? A) 88 gal #B) 93 gal C) 120 gal D) 115 gal 033-03-04 Radio planning practice 1165. (all) (Refer to Jeppesen Manual ED-6 or figure ED6-02) What is the frequency for Stuttgart ATIS? #A) 126,125 MHz B) 135,775 MHz C) 112,250 MHZ D) 126,12 kHz 12267. (all) (Refer to Route Manual VFR+GPS chart ED-6 or figure ED6-02) Give the name and frequency of the Flight Information Service for an aeroplane in position (47°59 N, 010°14 E). A) MEMMINGEN INFORMATION 122,1 MHz. #B) MUNCHEN INFORMATION 126,95 MHz. C) MUNCHEN INFORMATION 120,65 MHz. D) FRANKFURT INFORMATION 128,95 MHz.
12269. (all) (Refer to Route Manual VFR+GPS chart ED-6 or figure ED6-11) Which navigation aid is located in position 48°30 N 007°34 E? A) NDB B) VOR C) TACAN #D) VOR/DME 033-04 IFR (AIRWAYS) FLIGHT PLANNING 23 © 2008 AVIATIONEXAM.com 2194 (C) 2199 (D) 2208 (D) 2222 (C) 2226 (A) 2234 (C) 033-04-01 Meteorological considerations 2194. (AIR: atpl, ir; HELI: atpl, ir) Given the following TAF / METAR: What are the lowest cloud conditions (oktas/feet) forecast for JOHANNESBURG/JAN SMUTS at 0300 UTC? JOHANNESBURG/JAN SMUTS FAJS/JNB FT0900 120900Z 121212 36010KT 9999 FEW030CB FEW035 PROB40 TEMPO 1318 VRB15KT 3000 TSRA SCT030CB BKN080 FM2000 03005KT CAVOK BECMG 0204 SCT008 SCT100 PROB30 0305 3000 BCFG BKN004 FM0800 34012KT 9999 SCT025 T25/12Z T15/03Z T27/12Z= A) 5 to 7 at 800. B) 3 to 4 at 800. #C) 5 to 7 at 400. D) 3 to 4 at 400. 2199. (AIR: atpl, ir; HELI: atpl, ir) Given the following TAF / METAR: Which best describes the weather, if any, at Lyon / Satolas at 1330 UTC? LYONS/SATOLAS LFLL/LYS SA1330 121330Z 14007KT 9000 -TSRA FEW020CB SCT033TCU BKN046 09/07 Q1003 NOSIG= FC1100r 121100Z 121221 VRB03KT 9999 FEW010 SCT020 BKN040 BECMG 1821 33006KT TEMPO 1221 VRB15G20KT 4000 SHRA SCT008 BKN015= FT1000 121000Z 121812 33004KT 9999 SCT025 BKN060 BECMG 2224 VRB02KT 8000 SCT010 SCT020 BECMG 0204 1500 BR BKN003 TEMPO 0407 0800 FG OVC002 BECMG 0810 33006KT 9999 SCT015 BKN030= A) Nil. B) Frequent rain showers. C) Fog. #D) Light rain associated with thunderstorms. 2208. (AIR: atpl, ir; HELI: atpl, ir) Refer to weather information for Birmingham. What is the total time for which the weather is forecast? BIRMINGHAM EGBB/BHX SA0850 280850 18014kt 9999 SCT024 BKN030 BKN045 12/08 Q1011= FC0600 280600Z 280816 190015G27kt 9999 BKN025 TEMPO 0812 5000 - DZ BKN012 BECMG 1214 19022G37= FT0400 280434Z 281212 19022G37 9999 BKN025 TEMPO 1902 5000 RA BKN010 BECMG 2201 25007kt A) 9 hours.
B) 18 hours. C) 24 hours. #D) 28 hours. 2222. (AIR: atpl, ir; HELI: atpl, ir) Given the following TAF / METAR: What maximum windspeed (kts) is forecast for BORDEAUX / MERIGNAC AT 1600 UTC? Bordeaux / Merignac LFBD / BOD SA1330 121330Z 21005KT 9000 FEW030TCU FEW 033CB SCT040 BKN100 09/08 Q1005 TEMPO 25015G25KT 3000 TSRA SCT005 BKN015CB= FC1100r 121100Z 121221 28010KT 9999 -RA SCT020 FEW025CB SCT040 TEMPO 1218 25015G25KT 6000 SHRA SCT008 SCT020CB BKN033 PROB30 TEMPO 1218 28020G30KT 3000 TSRA SCT005 BKN015CB BECMG 1821 22004KT 8000 NSW FEW006 BKN030= FT1000 121000Z 121812 30010KT 9999 SCT020 FEW025CB BKN040 BECMG 1822 22004KT 8000 FEW006 BKN030 BECMG 0306 24005KT 6000 SCT007 SCT015 BKN090 BECMG 1012 -RA= A) 10 B) 5 #C) 30 D) 25 2226. (AIR: atpl, ir; HELI: atpl, ir) A METAR reads: SA1430 35002KY 7000 SKC 21/03 QI024 = Which of the following information is contained in this METAR? #A) Temperature/dewpoint. B) Runway in use. C) Day/month. D) Period of validity. 2234. (AIR: atpl, ir; HELI: atpl, ir) Refer to the TAF below: What are the lowest cloud conditions forecast for 1900 UTC at HAMBURG (EDDH)? TAF EDDH ISSUED AT EDDH 0624 21010KT CAVOK BECMG 0810 9999 SCT025 SCT040 PROB30 TEMPO 1218 7000 -RADZ BKN012 BECMG 1620 7000 BKN020 TEMPO 1824 4000 RADZ BKN005 A) 5 to 7 at 1.200 ft. B) 3 to 4 at 500 ft. #C) 5 to 7 at 500 ft. D) 5 to 7 at 2.000 ft. 033-04 IFR (AIRWAYS) FLIGHT PLANNING 24 © 2008 AVIATIONEXAM.com 2243 (B) 2250 (C) 2258 (C) 2903 (C) 4304 (A) 4307 (A) 4318 (C) 4320 (C) 4330 (A) 4331 (A) 4335 (D) 2243. (AIR: atpl, ir; HELI: atpl, ir) Refer to weather information for Birmingham. What is the lowest visibility forecast at 280800Z? BIRMINGHAM EGBB/BHX SA0850 280850 18014kt 9999 SCT024 BKN030 BKN045
12/08 Q1011= FC0600 280600Z 280816 190015G27kt 9999 BKN025 TEMPO 0812 5000 - DZ BKN012 BECMG 1214 19022G37= FT0400 280434Z 281212 19022G37 9999 BKN025 TEMPO 1902 5000 RA BKN010 BECMG 2201 25007kt A) 50 km #B) 5.000 m C) 10 km or more D) 2.500 m 2250. (AIR: atpl, ir; HELI: atpl, ir) Given the following TAF/ METAR: What is the earliest time (UTC), if any, that thunderstorms are forecast for Tunis/Carthage? TUNIS/CARTHAGE DTTA/TUN SA1330 121330Z 24008KT 9999 FEW023 BKN200 24/08 Q1007= FC1200 121200Z 121322 28012KT 9999 FEW030 SCT200 BECMG 1518 30014KT SCT026 BKN200 TEMPO 1722 32014G25KT 6000 -SHRA FEW023CB= FT1020 121020Z 121212 26012KT 9999 FEW030 SCT200 BECMG 1619 30014KT 8000 SCT020 BKN100 TEMPO 1802 32014G25KT 6000 SHRA OR -TSSHRA FEW023CB BECMG 0406 28019KT 6000 BECMG 0810 8000 SCT020 SCT026 TEMPO 5000 -SHRA FEW026CB= A) 0800 B) 1300 #C) 1800 D) nil 2258. (AIR: atpl, ir; HELI: atpl, ir) A METAR reads: SA 1430 35002KT 7000 SKC 21/03 Q1024 Which of the following information is contained in this report? A) Day, month. B) Runway in use. #C) Temperature, dewpoint. D) Period of validity. 2903. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) Which best describes be maximum intensity of icing, if any, at FL150 in the vicinity of BUCHAREST (45°N 026°E)? A) Severe B) Nil #C) Moderate D) Light 4304. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) Which describes the maximum intensity of icing, if any, at FL180 in the vicinity of Casablanca (33°N 008°W)? #A) Severe B) Moderate C) Light D) Nil 4307. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) What is the temperature deviation (°C) from ISA over 60°N 000°E? #A) -9
B) -55 C) +2 D) +9 4318. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) What is the maximum wind speed over Italy? A) 100 kts at FL380. B) 110 kts at FL380 but the maximum not shown on the chart. #C) 110 kts at FL380. D) 130 kts at FL340. 4320. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) What mean temperature (°C) is likely on a course 360° (T) from 40°N to 50°N at 020°E? A) -47 B) -46 #C) -49 D) -50 4330. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) The approximate mean wind component (kt) along the true course 180 from 50°N to 40°N at 020°E is: #A) 55 kts tailwind. B) 40 kts tailwind. C) 70 kts tailwind. D) 55 kts headwind. 4331. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) At position 38°N 15°E what is the worst hazard which could be expected? #A) Engine flame-out and windscreen damage. B) Turbulence. C) Reduced visibilty. D) Nil. 4335. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) What is the wind associated with Munich (50°N 010°E)? A) Maximum wind of 160 kts from 360°(T). B) Maximum wind of 120 kts from 260° (M). C) Maximum wind of 100 kts from 360° (T). #D) Maximum wind of 140 kts from 290° (T). 033-04 IFR (AIRWAYS) FLIGHT PLANNING 25 © 2008 AVIATIONEXAM.com 4336 (D) 4350 (D) 4351 (D) 4353 (D) 4355 (B) 4359 (C) 12289 (C) 12290 (A) 12291 (D) 12293 (A) 12294 (C) 12295 (A) 12296 (D) 12297 (C) 4336. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) Which of the following flight levels, if any, is forecast to be clear of significant cloud, icing and CAT along the marked route from SHANNON (53°N 10°W) to BERLIN (53°N 13°E)? A) None B) FL290 C) FL210 #D) FL250 4350. (AIR: atpl, ir) (Refer to figure 033-79)
The approximate mean wind component at Mach 0,78 along the true course 270° at 50°N from 000° to 010°W is? A) 25 kts tailwind component. B) 55 kts headwind component. C) 35 kts tailwind component. #D) 40 kts headwind component. 4351. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) In the vicinity of WARSAW (52°N 020°E) the tropopause is at approximate: A) FL400 B) FL370 C) FL350 #D) FL330 4353. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) The surface system over London (51°N 000°E) is a / an: A) cold front moving west. B) warm front moving north. C) stationary occluded front. #D) occluded front moving east. 4355. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) In the vicinity of Paris (49°N 003°E), the tropopause is at approximately: A) FL340 #B) FL400 C) FL350 D) FL380 4359. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) Over PRAGUE (50N 014E) the lowest FL listed which is unaffected by CAT is: A) 350 B) 300 #C) 270 D) 400 12289. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) The surface weather system over England (53°N 002°W) is: A) a warm front moving southeast. B) a cold front moving east. #C) an occluded front moving east. D) a depression moving north. 12290. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) Which best describes the significant cloud, if any, forecast for the area southwest of BODO (67°N 014°E)? #A) 5 to 7 oktas CU and CB base below FL100, tops FL180. B) 5 to 7 oktas CU and CB base FL100, tops FL180. C) 3 to 7 oktas CU and CB base below FL100, tops FL180. D) Nil. 12291. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) Which best describes the maximum intensity of CAT, if any, forecast for FL330 over BENGHAZI (32°N 020°E)? A) Light B) Moderate C) Severe
#D) Nil 12293. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) The wind velocity over ITALY is: #A) a maximum of 110 kts at FL380. B) 130 kts at FL380 maximum velocity not shown on chart. C) a maximum of 160 kts at FL380. D) 110 kts at FL380 maximum velocity not shown on chart. 12294. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) The wind direction and velocity (° / kts) at 50°N 040°E is: A) 200/70 B) 020/80 #C) 020/70 D) 350/70 12295. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) The wind direction and velocity (° / kts) at 60°N 015°W is: #A) 290/155 B) 320/155 C) 110/155 D) 290/185 12296. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) What is the mean temperature deviation (°C) from the ISA over 50°N 10°W? A) +2 B) +9 C) +13 #D) -2 12297. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) The wind direction and velocity (° / kts) at 40°N 040°E is: A) 150/75 B) 300/75 #C) 330/75 D) 330/85 033-04 IFR (AIRWAYS) FLIGHT PLANNING 26 © 2008 AVIATIONEXAM.com 12298 (D) 12299 (C) 12300 (C) 12301 (C) 12533 (D) 12534 (D) 12535 (B) 12536 (B) 12537 (A) 12538 (A) 12539 (B) 12540 (A) 12541 (A) 12542 (B) 12298. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-70) What minimum visibility (m) is forecast for 0600 UTC at LONDON LHR (EGLL)? A) 2.200 B) 5.000 C) 10.000 #D) 1.500 12299. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-70) Which affects the visibility for 1330 UTC at TUNIS (DTTA)? A) Haze B) Mist #C) Smoke D) Dust 12300. (AIR: atpl, ir; HELI: atpl, ir)
(Refer to figures 033-70) What is the earliest time (UTC), if any, that thunderstorms are forecast for DUBAI (OMDB)? A) 1000 B) 1200 #C) 1400 D) Nil forecast 12301. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) What mean temperature (°C) is likely on a course of 360° (T) from 40°N to 50°N at 040°E? A) -49 B) -50 #C) -47 D) -46 12533. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) The W/V (°/kts) at 50°N 015°W is: A) 100/75 B) 175/90 C) 310/85 #D) 355/90 12534. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) What mean temperature (°C) is likely on a true course of 270° from 025°E to 010°E at 45°N? A) -48 B) -52 C) -54 #D) -50 12535. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-79) The W/V (°/kts) at 40°N 020°W is: A) 185/65 #B) 005/65 C) 185/60 D) 005/60 12536. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-82) What is the temperature deviation (°C) from ISA over 50°N 010°E? A) +10 #B) -10 C) -55 D) +2 12537. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-80) The W/V (°/kts) at 60°N 15°W is: #A) 290/40 B) 110/40 C) 280/20 D) 100/20 12538. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-77) Which best describes the significant cloud forecast for the area over WARSAW (52°N 021°E)? #A) 5 to 7 oktas CU and AC base below FL100 tops FL120. B) 3 to 4 oktas CU and AC base below FL100 tops FL120. C) 5 to 7 oktas CU and AC base FL100 tops FL120. D) 3 to 4 oktas CU and AC base FL100 tops FL120.
12539. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-77) Which best describes the maximum intensity of icing, if any, at FL100 overhead WARSAW (52°N 021°E)? A) Severe #B) Moderate C) Light D) Nil 12540. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) Which describes the intensity of icing, if any, at FL180 in the vicinity of the CANARY ISLANDS (29°N 015°W)? #A) Moderate or severe. B) Moderate. C) Light. D) Nil. 12541. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-77) The surface system over ZURICH (48°N 008°E) is: #A) occluded front moving east. B) quasi-stationary front moving east. C) quasi-stationary front moving south. D) occluded front moving north-east. 12542. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-77) In the vicinity of PARIS (49°N 002°E) the tropopause is at about: A) FL340 #B) FL350 C) FL400 D) FL450 033-04 IFR (AIRWAYS) FLIGHT PLANNING 27 © 2008 AVIATIONEXAM.com 12543 (A) 12544 (D) 12545 (C) 12546 (B) 12547 (A) 12548 (C) 12549 (A) 12550 (B) 12551 (B) 12552 (C) 22898 (C) 23747 (C) 23748 (C) 23749 (A) 12543. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-77) Which best describes the significant cloud forecast over ZURICH (48°N 008°E)? #A) Broken AC/CU base below FL100 tops FL190, embedded isolated CB base below FL100 tops FL300. B) Well separated CB base FL100 tops to FL300. C) Isolated CB embedded in layer cloud, surface to FL300. D) 5 to 7 oktas CU and AC base below FL100 tops to FL300. 12544. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) Which describes the maximum intensity of turbulence, if any, at FL210 in the vicinity of the CANARY ISLANDS (29°N 015°W)? A) Nil B) Light C) Moderate #D) Severe 12545. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-77) The maximum wind velocity (°/kts) over ATHENS (37°N 024°E) is:
A) 300/90 B) 270/320 #C) 250/110 D) 270/90 12546. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-77) Over LONDON (51°N 000°E/W), the lowest FL listed which is unaffected by CAT is: A) 360 #B) 230 C) 280 D) 310 12547. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-69) The forecast period covered by the PARIS/CHARLES-DEGAULLE TAFs totals (hours): #A) 27 B) 9 C) 18 D) 20 12548. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-69) The lowest cloud conditions (oktas/ft) at BORDEAUX/MERIGNAC at 1230 UTC were: A) 3 to 4 at 2.000. B) 3 to 4 at 800. #C) 1 to 2 at 3.000. D) 1 to 4 at 3.000. 12549. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-69) The surface wind velocity (°/kts) at PARIS/CHARLES-DEGAULLE at 1330 UTC was: #A) 270/04 B) 300/05 C) 270/08 D) 180/12 12550. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-69) Which is the heaviest type of precipitation, if any, forecast for BORDEAUX/MERIGNAC at 1000 UTC? A) Nil. #B) Light rain. C) Rain showers. D) Heavy rain associated with thunderstorms. 12551. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-69) What minimum visibility is forecast for PARIS/CHARLESDEGAULLE at 2100 UTC? A) 2.000 m #B) 6.000 m C) 10 km D) 8.000 m 12552. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-70) Which best describes the weather, if any, forecast for JOHANNESBURG/ JAN SMUTS at 0400 UTC? A) CAVOK. B) Mist and/or fog. #C) Patches of fog. D) Rain associated with thunderstorms.
22898. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-70) What affects the visibility forecast for TUNIS (DTTN)? A) Haze B) Mist #C) Smoke D) Dust 23747. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-78) The maximum wind velocity (°/kts) immediately north of TUNIS (36°N 010°E) is: A) 250/85 B) 180/105 #C) 190/95 D) 280/110 23748. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-78) Which describes the maximum intensity of turbulence, if any, forecast for FL260 over TOULOUSE (44°N 001°E)? A) Light. B) Nil. #C) Severe. D) Moderate. 23749. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-78) Which best describes the significant cloud forecast over TOULOUSE (44°N 001°E)? #A) Broken AC/CU base below FL100 tops FL150, embedded isolated CB base below FL100 tops FL270. B) Well separated CB base FL100 tops to FL270. C) Isolated CB embedded in layer cloud, surface to FL270. D) 5 to 7 oktas CU and AC base below FL100 tops to FL270. 033-04 IFR (AIRWAYS) FLIGHT PLANNING 28 © 2008 AVIATIONEXAM.com 23790 (B) 23791 (B) 23792 (D) 23793 (D) 23794 (D) 23795 (A) 23796 (A) 23797 (A) 25062 (C) 25063 (D) 25064 (A) 25069 (A) 25158 (B) 25159 (D) 23790. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-82) The W/V (°/kts) at 40°N 020°W is: A) 334/40 ##B) 310/40 C) 135/40 D) 155/40 23791. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-82) The W/V (°/kts) at 50°N 015°W is: A) 310/85 B) 290/75 C) 310/75 D) 100/75 23792. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-82) The W/V (°/kts) at 60°N 015°W is: A) 115/60 B) 300/70 C) 320/60 #D) 300/60
23793. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-78) In the vicinity of SHANNON (52°N 009°W) the tropopause is at about: A) FL270 B) FL350 C) FL300 #D) FL360 23794. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-78) The surface system over VIENNA (48°N 016°E) is a: A) cold front moving west. B) warm front moving north. C) stationary occluded front. #D) cold front moving east. 23795. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-78) Which best describes the maximum intensity of icing, if any, at FL160 in the vicinity of BERLIN (53°N 013°E)? #A) Moderate B) Severe C) Light D) Nil 23796. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-78) Which best describes the significant cloud forecast for the area east of Tunis (36°N 010°E)? #A) 5 to 7 oktas CU and AC base below FL100 tops FL180. B) 3 to 4 oktas CU and AC base below FL100 tops FL180. C) 5 to 7 oktas CU and AC base FL100 tops FL180. D) 3 to 4 oktas CU and AC base FL100 tops FL160. 23797. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-78) Which describes the intensity of icing, if any, at FL150 in the vicinity of TOULOUSE (44°N 01°E)? #A) Moderate or severe. B) moderate. C) Light. D) Nil. 25062. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-76) The lowest height of the tropopause on the whole chart is: A) FL240 B) FL250 #C) FL220 D) FL200 25063. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-76) On a flight from Cairo to Madrid at FL350 when Mt. Etna is not active, what sort of in-flight weather hazard might you encounter? A) None. B) Severe icing and turbulence within any CB. C) Light CAT. #D) Moderate CAT. 25064. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-76) The strongest wind and its level associated with any jetstream on the chart is: #A) 160 kts at FL320.
B) 100 kts at FL340. C) 150 kts at FL310. D) 130 kts at FL300. 25069. (AIR: atpl, ir; HELI: atpl, ir) In a METAR report the abbreviation NOSIG means: #A) no significant change. B) no significant cloud. C) no significant weather. D) no significant problems. 25158. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-81) The approximate mean wind velocity expected enroute at FL300 from Oslo (position O) to London (position L) is: A) 056/45 #B) 236/45 C) 236/51 D) 056/51 25159. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-81) The approximate mean temperature expected on route at FL260 from Oslo (position O) to London (position L) is: A) -59 °C B) -51 °C C) -56,5 °C #D) -43 °C 033-04 IFR (AIRWAYS) FLIGHT PLANNING 29 © 2008 AVIATIONEXAM.com 25160 (C) 25181 (C) 25182 (B) 25183 (C) 26301 (A) 28324 (C) 28332 (A) 28333 (C) 28334 (A) 1119 (B) 1124 (B) 1134 (A) 25160. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-81) The W/V over position S in Ireland is: A) 330/20 B) 330/50 #C) 330/60 D) 150/20 25181. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-76) Over PALMA (39°N 003°E) the lowest FL listed which is unaffected by CAT is: A) FL265 B) FL380 #C) FL260 D) FL270 25182. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-80) The approximate mean wind component along the true course 180° from 50°N to 40°N at 005°W is: A) 345/75 #B) 325/65 C) 145/75 D) 165/60 25183. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-80) What is the temperature deviation (°C) from ISA over 50°N 010°E? A) -58
B) -6 #C) +2 D) +10 26301. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-82) The approximate mean wind component (kts) along true course 180° from 50°N to 40°N at 005° W is: #A) tail wind 55 kts. B) tail wind 40 kts. C) tail wind 70 kts. D) headwind 45 kts. 28324. (AIR: atpl) (Refer to figures 033-75) The surface weather system over England (53°N 002°W) is: A) a warm front moving southeast. B) a depression moving north. #C) an occluded front moving east. D) a cold front moving east. 28332. (AIR: atpl) (Refer to figure 033-80) The W/V (°/kts) at 50°N 015°W is: #A) 300/45 B) 120/45 C) 300/25 D) 120/48 28333. (AIR: atpl) (Refer to figure 033-80) What ISA deviation from the mean temperature (°C) is likely on a true course of 270° from 025°E to 010°E at 45°N? A) -49° B) +2° #C) -4° D) -2° 28334. (AIR: atpl) The surface system west of PARIS is a: #A) cold front moving southeast. B) warm front moving north. C) stationary occluded front. D) cold front moving west. 033-04-02 Selection of routes to destination and alternates 1119. (AIR: atpl, ir; HELI: atpl, ir) According to the chart the minimum obstruction clearance altitude (MOCA) is 8.500 ft. The meteorological data gives an outside air temperature of -20 °C at FL85. The QNH, given by a meteorological station at an elevation of 4.000 ft is 1.003 hPa. What is the minimum pressure altitude which should be flown according to the given MOCA? A) 8.500 ft #B) 8.800 ft C) 12.800 ft D) 8.200 ft 1124. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(HI)4 or figure HI-29) The radio navigation aid at ZURICH (47°36 N 008°49 E) is: A) a NDB, frequency 115,0 kHz. #B) a VOR, frequency 115,0 MHz. C) a VOR/DME, frequency 115,0 MHz. D) a TACAN on channel 11. 1134. (AIR: atpl, ir)
On a given path, it is possible to chose between four flight levels (FL), each associated with a mandatory flight Mach number (M). The flight conditions, static air temperature (SAT) and headwind component (HWC) are given below: FL370 M 0,80 Ts: -60 °C HWC: -15 kts FL330 M 0,78 Ts: -60 °C HWC: - 5 kts FL290 M 0,80 Ts: -55 °C HWC: -15 kts FL270 M 0,76 Ts: -43 °C HWC: 0 The flight level allowing the highest ground speed is: #A) FL270 B) FL290 C) FL330 D) FL370 033-04 IFR (AIRWAYS) FLIGHT PLANNING 30 © 2008 AVIATIONEXAM.com 1156 (A) 1157 (D) 1174 (B) 1175 (B) 1176 (A) 1270 (D) 1288 (A) 1304 (D) 1312 (A) 2176 (C) 2178 (B) 2179 (C) 2180 (D) 1156. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(HI)4 or figure HI-01) The radio aid at STAD (51°45 N 004°15 E) is: #A) a NDB, frequency 386 kHz. B) a VOR frequency 386 Mhz. C) a VOR/DME on channel 386. D) a TACAN on channel 386. 1157. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(LO)1 or figure LO-01) From SHANNON (52°43,3 N 008°53,1 W) by W13 to KORAK. What is meant by 5000 by the route centerline? A) MORA 5.000 ft. B) MAA 5.000 ft. C) MOCA 5.000 ft. #D) MEA 5.000 ft. 1174. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(LO)1 or figure LO-01) What radio navigation aid is at SHANNON (52°43 N 008°53 W)? A) VOR SHA 113,3 MHz only. #B) VOR DME SHA 113,3 MHz. C) NDB frequency 353 kHz. D) TACAN frequency 113,3 kHz. 1175. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(LO)5 or figure LO-03) See DENKO (52°49 N 015°50 E). What does 440 DRE mean? A) 440 kHz plus ident. #B) 440 kHz plus ident only when BFO switched on. C) 440 kHz plus ident only when BFO switched off. D) 440 MHz plus ADF only when BFO off. 1176. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(LO)1 or figure LO-02) The radio navigation aid at TOPCLIFFE (54°12 N 001°22 W) is a: #A) TACAN only, channel 84, (frequency 113,7 MHz). B) TACAN, channel 84, and a VOR frequency 113,7 MHz only. C) TACAN, channel 84, and an NDB frequency 92 kHz only. D) VORTAC, frequency 113,7 MHz, and an NDB frequency
92 kHz. 1270. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)4 or figure HI-02) The magnetic course and distance from SALZBURG SBG 113.8 (N48 00 E012 54) to STAUB (N48 44 E 012 38) on airway UB5 is: A) 346 / 43 NM. B) 166 / 64 NM. C) 346 / 64 NM. #D) 346 / 45 NM. 1288. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)4 or figures HI-03_a and HI-03_b) Of the following, the preferred airways routing from FRANKFURT FFM 114,2 (50°03 N 008°38 E) to KOKSY (51°06 N 002°39 E) above FL245, on a Wednesday is: #A) UR10 NTM UB6 BUB ATS. B) UG108 SPI UG1. C) UB69 DINKI UB6 BUB ATS. D) UG1. 1304. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)5 or figure HI-05) Given Leg MOULINS (46°42 N 003°38,0 E) / DIJON (47°16,3 N 005°05,9 E). Find route designator and distance. A) UG12, 69 NM. B) UG21, 70 NM. C) D, 44 NM. #D) Direct route, 69 NM. 1312. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)5 or figure HI-06) What radio navaids are shown at CHIOGGIA (45°04 N 012°16 E)? #A) VOR/DME freq 114,1, NDB freq 408. B) VOR freq 114,1, TACAN freq 408. C) VOR freq 114,1, TACAN channel 408. D) VOR/DME 114,1, DME freq 408. 2176. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)5 or figure HI-07) Of the following, the preferred airways routing from AMBOISE AMB 113,7 (47°26 N 001°04 E) to AGEN AGN (43°53 N 000° 52 E) above FL200 is: A) UB19 POI UB195. B) UH40 FOUCO UH20 PERIG UA34. #C) UA34. D) UB19 CGC UA25. 2178. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(HI)4 or figure HI-08) The magnetic course and distance from ST PREX SPR 113,9 (46°28 N 006°27 E) to FRIBOURG FRI 115,1 (46°47 N 007°14 E) on airway UG60. A) 048° / 46 NM. #B) 061° / 37 NM. C) 061° / 28 NM. D) 041° / 78 NM. 2179. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(LO)5 or figure LO-06) The airway intersection at RONNEBY (56°18 N 015°16 E) is marked by: A) a fan marker callsign LP.
B) a TACAN callsign RON. #C) a NDB callsign N. D) a NDB callsign LF. 2180. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual STAR charts PARIS (CharlesdeGaulle - 20-2) or figure AP-04) The route distance from CHIEVRES (CIV) to BOURSONNE (BSN) is: A) 73 NM B) 83 NM C) 88 NM #D) 96 NM 033-04 IFR (AIRWAYS) FLIGHT PLANNING 31 © 2008 AVIATIONEXAM.com 2182 (B) 2187 (A) 2189 (A) 2192 (A) 2193 (B) 2196 (B) 2197 (C) 2198 (D) 2200 (B) 2202 (B) 2203 (B) 2204 (C) 2182. (AIR: atpl, ir; HELI: atpl, ir) An airway is marked 3500T 2100a. This indicates that: A) the minimum enroute altitude (MEA) is 3.500 ft. #B) the minimum obstruction clearance altitude (MOCA) is 3.500 ft. C) the airway base is 3.500 ft MSL. D) the airway is a low level link route 2.100 ft - 3.500 ft MSL. 2187. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart NAP or figure HI-23) The initial magnetic course from A (64°N 006°E) to C (62°N 020°W) is: #A) 275° B) 267° C) 271° D) 262° 2189. (AIR: atpl, ir; HELI: atpl, ir) An aircraft, following a 215° true track at variation 3°W, must fly over a 10.600 ft obstacle with a minimum obstacle clearance of 1.500 ft. Knowing the QNH received from an airport close by, which is almost at sea-level, is 1.035 and the temperature is ISA -15 °C, the minimum flight level will be: #A) 140 B) 120 C) 130 D) 150 2192. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 5 or figure LO-04) The magnetic course/distance from EELDE EEL 112,4 (53°10 N 006°40 E) to WELGO (54°18 N 007°25 E) on airway A7 are: #A) 024° / 73 NM. B) 023° / 73 NM. C) 024° / 67 NM. D) 023° / 47 NM. 2193. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(HI)5 or figure HI-04) An appropriate FL for flight along airway UG5 from MENDENASBINALS MEN 115,3 (44°36 N 003°10 E) to GAILLAC GAI 115,8 (43°57 N 001°50 E) is: A) FL280
#B) FL290 C) FL300 D) FL310 2196. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)4 or figure HI-15) The magnetic course / distance from DINKESBUHL DKB 117,8 (49°09 N 010°14 E) to ERLANGEN ERL 114,9 (49°39 N 011°09 E) on airway UR11 are: A) 052° / 97 NM. #B) 050° / 47 NM. C) 133° / 85 NM. D) 230° / 97 NM. 2197. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(HI)4 or figure HI-15) An appropriate flight level for flight on airway UG1 from ERLANGEN ERL 114,9 (49°39 N 011°09 E) to FRANKFURT FFM 114,2 (50°03 N 008°38 E) is: A) FL300 B) FL290 #C) FL310 D) FL320 2198. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)4 or figure HI-16) What is the best route from CLACTON CLN (51°50,9 N 001°09,0 E) to MIDHURST MID (51°03,2 N 000°37,4 W)? A) UR12. B) TRIPO UR1 LAM UR1. C) UR123. #D) UB29 LAM UR1. 2200. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(LO)1 or figure LO-07) The magnetic course / distance from WALLASEY WAL 114,1 (53°23 N 003°28 W) to LIFFY (53°29 N 005°30 W) on airway B1 are: A) 279° / 114 NM. #B) 279° / 85 NM. C) 311° / 114 NM. D) 311° / 85 NM. 2202. (AIR: atpl, ir; HELI: atpl, ir) Using the following information, what is the minimum flight level considering the temperature? True track: 215° Mountain elevation: 11.600 ft Local airfield gives QNH as 1.035 mb Required terrain clearance: 1.500 ft Temperature: ISA - 15C A) FL150 #B) FL140 C) FL120 D) FL110 2203. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart 5AT(HI) or figure HI-17) On airway PTS P from VIGRA (62°34 N 006°02 E), the initial great circle grid course is: A) 353° #B) 344° C) 347° D) 350° 2204. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(HI)4 or figure HI-11)
Planning a IFR flight from Paris Charles de Gaulle (49°00,9 N 002°36,9 E) to London Heathrow (51°29,2 N 000°27,9 W). Find the average true course from Paris to London. A) 330° B) 142° #C) 322° D) 343° 033-04 IFR (AIRWAYS) FLIGHT PLANNING 32 © 2008 AVIATIONEXAM.com 2207 (D) 2209 (B) 2210 (D) 2211 (C) 2212 (B) 2213 (C) 2214 (C) 2215 (D) 2216 (B) 2218 (A) 2219 (A) 2223 (D) 2224 (C) 2207. (AIR: atpl, ir; HELI: atpl, ir) An IFR flight is planned outside airways on a course of 235° magnetic. The minimum safe altitude is 7.800 ft. Knowing the QNH is 995 hPa, the minimum flight level you must fly is: A) 80 B) 90 C) 85 #D) 100 2209. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(HI)4 or figure HI-09) An aeroplane has to fly from Abbeville (50°08,1 N 001°51,3 E) to Biggin (51°19,8 N 00°00,2 E). What is the first FL above FL295 that can be flown on an IFR flight plan? A) FL330 #B) FL310 C) FL320 D) FL300 2210. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (HI)5 or figure HI-21) The magnetic course and distance from LIMOGES LMG 114,5 (45°49 N 001°02 E) to CLERMONT FERRAND CMF 117,5 (45°47 N 003°11 E) on airway UG22 are: A) 046° / 70 NM B) 067° / 122 NM C) 113° / 142 NM #D) 094° / 90 NM 2211. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual 5AT(HI) or figures HI-18_a and HI-18_b) Flying from 80°N 170°E to 75°N 11°E. Initial track is 177 grid. What is the initial true track? A) 177° B) 357° #C) 347° D) 167° 2212. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(HI)4 or figure HI-14) An aeroplane has to fly from Salzburg (48°00,2 N 012°53,6 E) to Klagenfurt (46°37,5 N 014°33,8 E). Which statement is correct? A) The minimum enroute altitude (MEA) is 13.400 ft. #B) The minimum grid safe altitude on this route is 13.400 ft above MSL. C) The minimum sector altitude (MSA) is 13.400 ft.
D) The minimum obstacle clearance altitude (MOCA) on this route is 10.800 ft above MSL. 2213. (AIR: atpl, ir; HELI: atpl, ir) You must fly IFR on an airway orientated 135° magnetic with a MSA at 7.800 ft. Knowing the QNH is 1.025 hPa and the temperature is ISA + 10°, the minimum flight level you must fly at is: A) 75 B) 80 #C) 90 D) 70 2214. (AIR: atpl, ir; HELI: atpl, ir) For an IFR flight using ICAO semi-circular cruising levels on a magnetic track of 200, which is a suitable level? A) FL290 B) FL300 #C) FL310 D) FL320 2215. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(HI)4 or figure HI-09) An aeroplane has to fly from Abbeville (50°08,1 N 001°51,3 E) to Biggin (51°19,8 N 000°00,2 E). What is the distance of this leg? A) 62 NM B) 38 NM C) 64 NM #D) 100 NM 2216. (AIR: atpl, ir; HELI: atpl, ir) An appropriate flight level for IFR flight in accordance with semi-circular height rules on a magnetic course of 200° is: A) FL320 #B) FL310 C) FL290 D) FL300 2218. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(LO)2 or figure LO-11) The minimum enroute altitude (MEA) that can be maintained continuously on airway G4 from JERSEY JSY 112,2 (49°13 N 002°03 W) to LIZAD (49°35 N 004°20 W) is: #A) FL140 B) 1.000 ft MSL C) FL60 D) 2.800 ft MSL 2219. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(LO)5 or figure LO-09) The minimum enroute altitude that can be maintained continuously on airway B65/H65 from DOXON (55°27 N 018°10 E) to RONNE ROE 112,0 (55°04 N 014°46 E) is: #A) FL100 B) 1.000 ft C) FL60 D) 2.500 ft 2223. (AIR: atpl, ir; HELI: atpl, ir) An appropriate flight level for IFR flight in accordance with semi-circular height rules on a course of 180° magnetic is: A) FL105 B) FL90 C) FL95 #D) FL100 2224. (AIR: atpl, ir; HELI: atpl, ir)
Unless otherwise stated on charts for standard instrument departures the routes shown are given with: A) magnetic headings. B) true course. #C) magnetic course. D) true headings. 033-04 IFR (AIRWAYS) FLIGHT PLANNING 33 © 2008 AVIATIONEXAM.com 2227 (C) 2228 (D) 2229 (B) 2231 (A) 2232 (A) 2235 (A) 2236 (C) 2237 (B) 2238 (A) 2242 (A) 2244 (A) 2245 (D) 2227. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual STAR 10-2 and instrument approach chart 11-4 ILS/DME Rwy 27R for London Heathrow or figures AP-08 and AP-09) Planning an IFR flight from Paris to London (Heathrow). Name the identifier and frequency of the initial approach fix (IAF) of the BIG2A arrival route: A) EPM; 316 kHz. B) BIG; 115,1 kHz. #C) BIG; 115,1 MHz. D) OCK; 115,3 MHz. 2228. (AIR: atpl, ir; HELI: atpl, ir) An airway is marked 5000 2900a. The notation 5000 is the: A) base of the airway (AGL). B) maximum authorised altitude (MAA). C) minimum holding altitude (MHA). #D) minimum enroute altitude (MEA). 2229. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(HI)4 or figure HI-11) Planning a IFR flight from Paris Charles de Gaulle (N49 00.9 E002 36.9) to London Heathrow (51°29,2 N 000°27,9 E). Determine the preplanning distance by calculating the direct distance plus 10%. A) 188 NM #B) 207 NM C) 308 NM D) 218 NM 2231. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual MADRID BARAJAS 10-2B STAR or figure AP-13) For runway 33 arrivals from the east and south, the Initial Approach Fix (IAF) inbound from airway UR10 is: #A) VTB B) CJN C) CENTA D) MOTIL 2232. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)5 or figure HI-22) The minimum enroute altitude available on airway UR160 from NICE NIZ 112,4 (43°46 N 007°15 E) to BASTIA BTA 116,2 (42°32 N 009°29 E) is: #A) FL250 B) FL260 C) FL210 D) FL200 2235. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual SID chart for AMSTERDAM
ARNEM (10-3B) or figure AP-14) The route distance from DER 27 to ARNEM is: #A) 67 NM B) 35 NM C) 59 NM D) 52 NM 2236. (AIR: atpl, ir; HELI: atpl, ir) (For this question use Route Manual chart E(HI)4 or figure HI-14) An aeroplane has to fly from Salzburg (48°00,2 N 012°53,6 E) to Klagenfurt (46°37,5 N 014°33,8 E). Which statement is correct? A) The airway UB5 is closed for southbound traffic above FL200. B) The airway UB5 cannot be used, there is one way traffic to the north. #C) The airway UB5 can be used for flights to/from Klagenfurt and Salzburg. D) The airway UB5 is closed in this direction except during the weekends. 2237. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(LO)1 or figure LO-08) The minimum enroute altitude that can be maintained continuously on airway G1 from STRUMBLE 113,1 (52°00 N 005°02 W) to BRECON 117,45 (51°43 N 003°16 W) is: A) FL80 #B) FL110 C) 4.100 ft AMSL D) 2.900 ft AMSL 2238. (AIR: atpl, ir; HELI: atpl, ir) On an IFR navigation chart, in a 1° quadrant of longitude and latitude, appears the following information: 80 . This means that within this quadrant: #A) the minimum safe altitude is 8.000 ft. B) the minimum flight level is FL80. C) the altitude of the highest obstacle is 8.000 ft. D) the floor of the airway is at 8.000 ft. 2242. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart 5 AT(HI) or figure HI-20) What is the initial grid track from Stornoway (58°12,4 N 006°11,0 W) to Keflavik (64°00 N 022°40 W)? #A) 320 B) 140 C) 313 D) 133 2244. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(HI)4 or figure HI-14) An aeroplane has to fly from Salzburg (48°00,2 N 012°53,6 E) to Klagenfurt (46°37,5 N 014°33,8 E). At Salzburg there is stated on the chart D 113,8 SBG. That means: #A) VOR/DME with identification SBG frequency 113,8 MHz can be used. B) only the DME with identification SBG can be used, for which frequency 113,8 MHz should be tuned, VOR is not available. C) VOR/DME SBG will be deleted in the future and cannot be used for navigation. D) ILS/DME 113,8 MHz of Salzburg airport can be used for navigation. 2245. (AIR: atpl, ir; HELI: atpl, ir)
(Refer to Jeppesen Manual Munich STAR charts for MUNICH 10-2A,B or figures AP-17, AP-18 and AP-19) With an easterly surface wind, approaching from the west, to Munich via the TANGO VOR. Which is the best STAR and its associated IAF (Initial Approach Fix)? A) Kempten 2T / BETOS. B) NDG 1T / ROKIL. C) RODING 1R / MOOSBURG. #D) AALEN 1T / ROKIL. 033-04 IFR (AIRWAYS) FLIGHT PLANNING 34 © 2008 AVIATIONEXAM.com 2247 (A) 2248 (C) 2253 (B) 2254 (D) 2256 (B) 2907 (D) 12251 (C) 12252 (B) 12253 (B) 12254 (B) 12255 (A) 2247. (AIR: atpl, ir; HELI: atpl, ir) An appropriate flight level for IFR flight in accordance with semi-circular height rules on a course of 180° (M) is: #A) FL100 B) FL90 C) FL95 D) FL105 2248. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(LO)5 or figure LO-10) An appropriate flight level for flight on airway G9 from SUBI SUI 116,7 (52°23 N 014°35 E) to CZEMPIN CZE 114,5 (52°08 N 016°44 E) is: A) FL50 B) FL60 #C) FL70 D) FL80 2253. (AIR: atpl, ir; HELI: atpl, ir) On an instrument approach chart, a minimum sector altitude (MSA) is defined in relation to a radio navigation facility. Without any particular specification on distance, this altitude is valid to: A) 20 NM #B) 25 NM C) 15 NM D) 10 NM 2254. (AIR: atpl, ir; HELI: atpl, ir) An airway is marked FL80 1500 a. This indicates that: A) 1.500 ft MSL is the minimum radio reception altitude (MRA). B) the airway base is 1.500 ft MSL. C) the airways extends from 1.500 ft MSL to FL80. #D) the minimum enroute altitude (MEA) is FL80. 2256. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)4 or figure HI-13) The minimum enroute altitude that can be maintained continuously on airway UA34 from WALLASEY WAL 114,1 (53°23 N 003°08 W) to MIDHURST MID 114,0 (51°03 N 000°37 W) is: A) FL245 #B) FL290 C) 5.300 ft D) 16.800 ft 2907. (AIR: atpl, ir; HELI: atpl, ir) (Refer to SID chart Paris Charles de Gaulle 20-3 or figure
AP-03) Planning an IFR-flight from Paris Charles de Gaulle to London. SID is ABB 8A. Assume: Variation 3° W TAS 430 kts W/V 280/40 Distance to top of climb 50 NM Determine the magnetic course, ground speed and wind correction angle from top of climb to ABB 116.6. A) MC 169°, GS 450 kts, WCA +4°. B) MC 349°, GS 414 kts, WCA +5°. C) MC 169°, GS 414 kts, WCA +5°. #D) MC 349°, GS 414 kts, WCA -5°. 12251. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(HI)4 CAA-Edition, STAR 10-2 and Instrument approach chart 11-4 ILS DME Rwy 27R for London Heathrow or figures HI-09; AP-08 and AP-09) Planning an IFR-flight from Paris to London (Heathrow). Assume: STAR is BIG 2A Variation 5° W Enroute TAS 430 kts W/V 280/40 Descent distance 76NM Determine the magnetic course, ground speed and wind correction angle from ABB 116,6 (50°08,1 N 001°51,3 E) to top of descent. A) MC 319°, GS 396 kts, WCA -3°. B) MC 141°, GS 396 kts, WCA -3°. #C) MC 321°, GS 396 kts, WCA -3°. D) MC141°, GS 396 kts, WCA +3°. 12252. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (HI)4 CAA-Edition or figure HI-30) An appropriate flight level for flight on airway UR1 from ORTAC (50°00 N 002°00 W) to MIDHURST MID 114,0 (51°03 N 000°37 W) is: A) FL230 #B) FL250 C) FL260 D) FL240 12253. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(HI) 5 CAA-Edition or figure HI-36) An appropriate flight level for flight on airway UR24 from NANTES NTS 117,2 (47°09 N 001°37 W) to CAEN CAN (49°10 N 000°27 W) is: A) FL270 #B) FL310 C) FL290 D) FL300 12254. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (LO)2 or figure LO-13) An appropriate flight level for flight on airway B3 from CHATILLON CTL 117,6 (49°08 N 003°35 E) to CAMBRAI CMB 112,6 (50°14 N 003°09 E) is: A) FL50 #B) FL170 C) FL80 D) FL60
12255. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (LO)6 or figure LO-16) An appropriate flight level for flight on airway W37 from CHEB OKG 115,7 (50°04 N 012°24 E) to RODING RDG 114,7 (49°02 N 012°32 E) is: #A) FL80 B) FL40 C) FL50 D) FL70 033-04 IFR (AIRWAYS) FLIGHT PLANNING 35 © 2008 AVIATIONEXAM.com 12256 (B) 12257 (D) 12258 (C) 12273 (B) 12274 (C) 12275 (A) 12276 (C) 12277 (A) 12278 (B) 12279 (C) 12280 (A) 12281 (A) 12256. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(LO)6 or figure LO-17) An appropriate flight level for flight on airway R10 from MONTMEDY MMD 109,4 (49°24 N 005°08 E) to CHATILLON CTL 117,6 (49°08 N 003°35 E) is: A) FL40 #B) FL60 C) FL70 D) FL50 12257. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual Instrument approach charts for ZURICH (10-2,10-2A,10-2B) or figures AP-21, AP-22 and AP-23) Aeroplane arriving via route BLM 2Z only, should proceed via which route to EKRON int? A) TRA R247 outbound to EKRON int. B) WIL R018 outbound to EKRON int. C) HOC R067 via GOLKE to EKRON int. #D) BLM R111 to GOLKE int then TRA R-247 inbound to EKRON int. 12258. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual STAR chart for LONDON HEATHROW (10-2D) or figure AP-25) The minimum holding altitude (MHA) and maximum holding speed (IAS) at MHA at OCKHAM OCK 115,3 are: A) 7.000 ft and 250 kts. B) 9.000 ft and 250 kts. #C) 7.000 ft and 220 kts. D) 9.000 ft and 220 kts. 12273. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (HI)5 CAA-Edition or figure HI-37) Of the following, the preferred airways routing from MARTIGUES MTG 117,3 (43°23 N 005°05 E) to ST PREX SPR 113,9 (46°28 N 006°27 E) above FL245 is: A) UA6 LSA UG52. #B) UB282 DGN UB46. C) UB284 VILAR UB28. D) UB28. 12274. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (HI)4 CAA-Edition or figure HI-31) Of the following, the preferred airways routing from CLACTON CLN 114,55 (51°51 N 001°09 E) to DINARD DIN 114,3
(48°35 N 002°05 W) above FL245 is: A) UR12 MID UR8 SAM UB11 BARLU UW115. B) UB29 LAM UR1 MID UA34 LILAN UR9. #C) UB29 LAM UR1 ORTAC UR14. D) UR12 MID UA47 DPE UA475 SOKMU UH111. 12275. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (HI)4 CAA-Edition or figure HI-32) The magnetic course/distance from DINKELSBUHL DKB 117,8 (49°09 N 010°14 E) to ERLANGEN ERL 114,9 (49°39 N 011°09 E) on airway UR11 is: #A) 050° / 47 NM. B) 230° / 97 NM. C) 133° / 85 NM. D) 052° / 97 NM. 12276. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (LO)6 or figure LO-14) The magnetic course/distance from GROSTENQUIN GTQ 111,25 (49°00 N 006°43 E) to LINNA (49°41 N 006°15 E) on airway R7 is: A) 337° / 31 NM. B) 337° / 58 NM. #C) 337° / 46 NM. D) 157° / 58 NM. 12277. (AIR: atpl, ir; HELI: atpl, ir) (Refer toRoute Manual chart E(LO)5) or figure LO-15) The magnetic course/distance from ELBE LBE 115,1 (53°39 N 009°36 E) to LUNUD (54°50 N 009°19 E) on airway H12 is: #A) 352° / 72 NM. B) 352° / 96 NM. C) 339° / 80 NM. D) 339° / 125 NM. 12278. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (LO)2 or figure LO-13) The magnetic course/distance from CAMBRAI CMB 112,6 (50°14 N 003°09 E) to TALUN (49°33 N 003°25 E) on airway B3 is: A) 349° / 42 NM. #B) 169° / 42 NM. C) 349° / 26 NM. D) 169° / 68 NM. 12279. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (HI)4 CAA-Edition or figure HI-34) The magnetic course/distance from TRENT TNT 115,7 (53°03 N 001°40 W) to WALLASEY WAL 114,1 (53°23 N 003°08 W) on airway UR3 is: A) 297° / 70 NM. B) 117° / 71 NM. #C) 297° / 57 NM. D) 117° / 57 NM. 12280. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (HI)4 CAA-Edition or figure HI-32) The magnetic course/distance from TANGO TGO 112,5 (48°37 N 009°16 E) to DINKELSBUHL DKB 117,8 (49°09 N 010°14 E) on airway UR11 is: #A) 052° / 50 NM. B) 007° / 60 NM.
C) 105° / 105 NM. D) 132° / 43 NM. 12281. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(HI)5 CAA-Edition or figure HI-35) The magnetic course/distance from ELBA ELB 114,7 (42°44 N 010°24 E) to SPEZI (43°49 N 009°34 E) on airway UA35 is: #A) 332° / 76 NM. B) 152° / 42 NM. C) 322° / 60 NM. D) 332° / 118 NM. 033-04 IFR (AIRWAYS) FLIGHT PLANNING 36 © 2008 AVIATIONEXAM.com 12282 (C) 12283 (D) 12284 (A) 12285 (A) 12286 (C) 12292 (B) 14367 (C) 23737 (D) 23738 (C) 23769 (C) 23770 (C) 23771 (D) 23772 (A) 12282. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E(LO)5 or figure LO-05) The VOR and TACAN on airway G9 at OSNABRUCK (52°12 N 008°17 E) are: A) NOT frequency paired, and have the same identifier. B) frequency paired, and have the same identifier. #C) NOT frequency paired, and have different identifiers. D) frequency paired, and have different identifiers. 12283. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart E (HI)4 CAA-Edition or figure HI-33) Aeroplanes intending to use airway UR14 should cross GIBSO intersection (50°45 N 002°30 W) at or above: A) FL140 B) FL160 C) FL200 #D) FL250 12284. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual SID chart for ZURICH (10-3) or figure AP-20) Which is the correct ALBIX departure via AARAU for runway 16? #A) ALBIX 7S. B) ALBIX 7A. C) ALBIX 6H. D) ALBIX 6E. 12285. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart AMSTERDAM JAA MINIMUMS (10-9X) or figure AP-26) The Radio Altimeter minimum altitude for a CAT II ILS DME approach to RWY 01L is: #A) 100 ft B) 88 ft C) 300 ft D) 188 ft 12286. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart PARIS CHARLES DE GAULLE ILS Rwy 27 (21-2) or figure AP-24) The crossing altitude and descent instruction for a propeller aircraft at COULOMMIERS (CLM) are: A) cross at FL80 descend to FL70.
B) cross at FL60 and maintain. #C) cross at FL60 descend to 4.000 ft. D) cross at FL70 descend to 4.000 ft. 12292. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-75) The maximum wind velocity (°/kts) shown in the vicinity of MUNICH (48°N 012°E) is: A) 290/110 #B) 300/140 C) 300/100 D) 300/160 14367. (AIR: atpl, ir; HELI: atpl, ir) The Final Reserve Fuel for aircraft with reciprocating engines should be: A) fuel to fly for 30 minutes. B) fuel to fly for 60 minutes. #C) fuel to fly for 45 minutes. D) 5 minutes fuel at the holding speed at 1.500 ft above the aerodrome in standard conditions. 23737. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(LO)5 or figure LO-03) The NDB at DENKO (52°49 N 015°50 E) can be identified on: A) channel 440, BFO on. B) channel 440, BFO off. C) frequency 440 kHz, BFO off. #D) frequency 440 kHz, BFO on. 23738. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual Munich STAR charts for MUNICH 10-2A,B or figures AP-17, AP-18 and AP-19) The correct arrival route and Initial Approach Fix (IAF) for an arrival from the west via TANGO for runway 08 L/R is: A) NDG 1T, IAF ROKIL. B) DKB 1T, IAF ROKIL. #C) AALEN 1T, IAF ROKIL. D) AALEN 1T, IAF MBG. 23769. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart NAP) On a direct great circle course from REYKJAVIK (64°10 N 020°00 W) to AMSTERDAM (52°32 N 004°50 E), the average true course and distance are: A) 118°, 1.095 NM. B) 311°, 1.824 NM. #C) 131°, 1.095 NM. D) 140°, 1.824 NM. 23770. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) An appropriate flight level for flight on airway A2 from TALLA 113,8 TLA (55°30 N 003°21 W) to DEAN CROSS 115,2 DCS (54°43 N 003°20 W) is: A) FL100 B) FL80 #C) FL90 D) FL50 23771. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) The distance on airway B4 from POLE HILL 112,1 POL (53°45 N 002°06 W) to SHAPP (54°30 N 002°38 W) is: A) 30 NM B) 31 NM
C) 51 NM #D) 49 NM 23772. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) The magnetic course from DEAN CROSS 115,2 DCS (54°43 N 003°20 W) to NEWCASTLE 114,25 NEW (55°02 N 001°41 W) on airway W911D is: #A) 077° B) 083° C) 257° D) 263° 033-04 IFR (AIRWAYS) FLIGHT PLANNING 37 © 2008 AVIATIONEXAM.com 23773 (B) 23774 (D) 23775 (A) 23777 (A) 23778 (D) 23779 (A) 23780 (D) 23781 (D) 23782 (D) 23783 (D) 23784 (D) 23785 (B) 23773. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) The magnetic course/distance from TALLA 113,8 TLA (55°30 N 003°21 W) to DEAN CROSS 115,2 DCS (54°43 N 003°20 W) on airway A2 is: A) 185° / 18 NM. #B) 185° / 47 NM. C) 005° / 47 NM. D) 005° / 18 NM. 23774. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) The minimum enroute altitude (MEA) that can be maintained continuously on advisory route W911D from NEWCASTLE 114,25 NEW (55°02 N 001°24 W) to DEAN CROSS 115,2 DCS (54°43 N 003°20 W) is: A) 4.520 ft B) FL150 C) 4.700 ft #D) FL50 23775. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) The minimum enroute altitude (MEA) that can be maintained continuously on airway B226 from TALLA 113,8 TLA (55°30N 003°21 W) to reporting point ANGUS (56°42 N 003°03 W) is: #A) FL70 B) FL80 C) 5.000 ft D) 5.500 ft 23777. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) The radio navigation aid at LEEDS BRADFORD (53°52 N 001°39 W) is: #A) an NDB, frequency 402,5 kHz, NOT continuous operation. B) a TACAN, channel 402,5. C) a fan marker, frequency 402,5 kHz. D) an NDB, frequency 402,5 kHz, continuous operation. 23778. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) The radio navigation aid at ST. ABBS (55°55 N 002°12 W) is: A) a VOR only, frequency 112,5 MHz.
B) an NDB, frequency 112,5 MHz. C) a TACAN, channel 112,5. #D) a VOR/DME, frequency 112,5 MHz. 23779. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) What is the Minimum Enroute Altitude (MEA) on airway W911D from DEAN CROSS 115,2 DCS (54°43 N 003°20 W) to NEWCASTLE 114,25 NEW (55°02 N 001°41 W)? #A) FL50 B) FL150 C) 4.700 ft D) 4.200 ft 23780. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) The magnetic course / distance from DEAN CROSS 115,2 DCS (54°43 N 003°20 W) to POLE HILL 112,1 POL (53°45 N 002°06 W) on airway A2 is: A) 329° / 53 NM. B) 143° / 53 NM. C) 155° / 73 NM. #D) 149° / 73 NM. 23781. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(LO)1) What is the Maximum Authorised Altitude (MMA) on airway W911D from DEAN CROSS 115,2 DCS (54°43 N 003°20 W) to NEWCASTLE 114,25 NEW (55°02 N 001°41 W)? A) 4.200 ft B) FL50 C) 4.700 ft #D) FL150 23782. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) The initial magnetic course from INVERNESS 109.2 INS (57°32 N 004°03 W) direct to TIREE 117,7 TIR (59°30 N 006°53 W) is: A) 230° B) 237° C) 218° #D) 244° 23783. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) The initial magnetic course from TIREE 117,7 TIR (59°30 N 006°53 W) direct to INVERNESS 109,2 INS (57°32 N 004°03 W) is: A) 236° B) 056° C) 048° #D) 064° 23784. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) The initial magnetic course from TIREE 117,7 TIR (59°30 N 006°53 W) direct to STORNOWAY 115,1 STN (58°12 N 006°11 W) is: A) 003° B) 192° C) 011° #D) 019° 23785. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) The initial true course from INVERNESS 109,2 INS (57°32 N
004°03 W) direct to TIREE 117,7 TIR (59°30 N 006°53 W) is: A) 244° #B) 237° C) 218° D) 230° 033-04 IFR (AIRWAYS) FLIGHT PLANNING 38 © 2008 AVIATIONEXAM.com 23786 (B) 23787 (B) 23788 (B) 23798 (C) 23799 (B) 23800 (D) 23801 (C) 23856 (C) 23857 (A) 23858 (D) 23859 (C) 23860 (D) 23786. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) The initial true course from TIREE 117,7 TIR (59°30 N 006°53 W) direct to INVERNESS 109,2 INS (57°32 N 004°03 W) is: A) 062° #B) 054° C) 048° D) 236° 23787. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) The initial true course from TIREE 117,7 TIR (59°30 N 006°53 W) direct to STORNOWAY 115,1 STN (58°12 N 006°11 W) is: A) 192° #B) 011° C) 019° D) 003° 23788. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) The direct distance from TIREE 117.7 TIR (59°30 N006°53 W) to INVERNESS 109.2 INS (57°32 N004°03 W) is: A) 204 NM #B) 112 NM C) 192 NM D) 360 km 23798. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - TRM, Esbjerg Aerodrome chart (19-2) or figure AP-32) What are the dimensions of runway 08/36 at Esbjerg? A) 8.530 ft x 45 ft. B) 8.530 m x 45 m. #C) 2.600 m x 45 m. D) 2.600 ft x 148 ft. 23799. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - TRM, Esbjerg Aerodrome chart (19-2) or figure AP-32) What is the position of the aerodrome reference point at ESBJERG? A) 55°31,6 N 008°33,1 W #B) 55°31,6 N 008°33,1 E C) 55°32,2 N 008°34,9 E D) 55°32,2 N 008°34,9 W 23800. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - TRM, Esbjerg Area chart (19-1) or figure AP-33) What is the course and distance from Locator HP to the threshold of Runway 08?
A) 080° (T) / 4,2 KM. B) 080° (T) / 4,2 NM. C) 080° (M) / 4,2 km. #D) 080° (M) / 4,2 NM. 23801. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - TRM, Esbjerg Area chart (19-1) or chart E(LO)5). What is the track and distance shown on the chart from VOR/DME SKR (55°13,8 N 009°12,9 E) to overhead Esbjerg (55°31,6 N 008°33,2 E)? A) 308° (T) / 29 NM. B) 308° (M) / 29 km. #C) 308° (M) / 29 NM. D) 308° (T) / 29 km. 23856. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) An aircraft has to fly from TALLA (55°30 N 003°21 W) to FINDO (56°22 N 003°28 W). Excluding RVSM, what is the first flight level above FL400 that can be flown on this leg? A) FL410 B) FL400 #C) FL430 D) FL420 23857. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) An aircraft has to fly from TIREE (56°29 N 006°53 W) direct to ABERDEEN (57°19 N 002°16 W). What is the minimum grid safe altitude for this route? #A) 5.700 ft B) 4.400 ft C) 3.600 ft D) 5.600 ft 23858. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) An aircraft is flying Northbound on the direct route from DEAN CROSS that passes through position 57°00 N 003°10 W. Excluding RVSM, what is the first flight level above FL400 that can be flown on this route? A) FL420 B) FL440 C) FL430 #D) FL450 23859. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) An aircraft is flying towards GOW (55°52 N 004°27W) on airway UN615 prior to an arrival in the London FIR. According to the information on the chart, what is the most appropriate radio frequency to obtain the latest meteorological information for London area? A) 115,4 B) 129,22 #C) 126,60 D) 133,67 23860. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) What is the average magnetic course from ABERDEEN (57°19 N 002°16 W) to TIREE (56°30 N 006°53 W)? A) 267° B) 253° C) 247°
#D) 260° 033-04 IFR (AIRWAYS) FLIGHT PLANNING 39 © 2008 AVIATIONEXAM.com 23861 (D) 23862 (B) 23864 (A) 23865 (D) 23866 (B) 23867 (D) 23868 (C) 23869 (A) 23870 (C) 23871 (B) 23872 (B) 23873 (A) 23861. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) What navigation aid(s) is/are available to civil aircraft at the military airfield of Kinloss (57°40 N 003°32 W)? A) VOR and DME on frequency 109,8. B) TACAN range and bearing on Channel 35. C) The bearing element only of TACAN on VOR frequency 109,8 MHz. #D) The range element only of TACAN on DME frequency 109,8 MHz. 23862. (AIR: atpl, ir; HELI: atpl, ir) (For this question, use Annex 033-006 or Route Manual chart E(HI)1) An aircraft has to fly from Glasgow (55°52 N 004°27 W) to Benbecula (57°29 N 007°22 W), cruising at 320 kts TAS. Assuming a headwind of 40 kts and cruise fuel consumption of 2.300 kg/hrs, what is the fuel consumption for this sector? A) 978 kg #B) 1.117 kg C) 869 kg D) 2.300 kg 23864. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) An aircraft has to fly from GOW (55°52 N 004°27 W) to INS (57°33 N 004°03 W) routing via FINDO (56°22 N 003°28 W). For flight planning purposes, what is the track distance? #A) 117 NM B) 44 NM C) 73 NM D) 102 NM 23865. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) An aircraft has to fly from beacon BEN (57°29 N 007°22 W) to beacon ADN (57°19 N 002°16 W). What is the average true course for this route? A) 109° B) 101° C) 281° #D) 093° 23866. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly from ALMA (55°25 N 013°34 E) to BACKA (57°33 N 011°59 E) on airways UB45 UH40 and UA9. What is the total track distance for this flight? A) 119 NM #B) 143 NM C) 105 NM D) 146 NM 23867. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly from the beacon TNO (55°46 N 011°26 E) on a direct route to the beacon HAR (57°50 N 012°42 E).
What is the magnetic track and distance for this flight? A) 007° / 131 NM. B) 029° / 69 NM. C) 013° / 117 NM. #D) 018° / 129 NM. 23868. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly from Aalborg (57°06 N 010°00 E) to Bottna (57°45 N 013°48 E) on airway UR46. What is the track distance for this flight? A) 260 NM B) 70 NM #C) 130 NM D) 60 NM 23869. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly on airways from ODIN (55°35 N 010°39 E) to BOTTNA (57°45 N 013°48 E). Which of the following is an acceptable route for this flight? #A) ODN UR156 SKA UH42 BTD. B) ODN UR12 PER UG5 SHG UH42 BTD. C) ODN UR156 LAV D17 CINDY UR46 BTD. D) ODN UR12/UN872 HIL UV30 BTD. 23870. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly on airways from SKARA (58°23 N 013°15 E) to SVEDA (56°10 N 012°34 E). Which of the following is an acceptable route for this flight? A) SKA UR156 LAV UB45 SVD. B) SKA UB44 BAK UA9 PAPER UH40 SVD. #C) SKA UH42 BTD UV30 HIL UR1 SVD. D) SKA DCT SVD. 23871. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft is flying from BACKA (57°33 N 011°59 E) to BOTTNA (57°45 N 013°48 E) on airway UR46. Which of the following would be a useful cross-reference to check the airway intersection CINDY? A) BAK078/BTD258 #B) HAR161/LAV092 C) LAV D17 D) BTD D60 23872. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) What is the meaning of the chart information for the beacon(s) at position 55°59 N 014°06 E? A) NDB, ident OE and VOR, ident VEY. #B) NDB only, ident OE. C) VOR only, ident VEY. D) Doppler VOR, ident SUP and NDB, ident OE. 23873. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly from ALMA (55°25 N 013°34 E) to PETER (56°50 N 013°35 E). Excluding RVSM, what is the lowest flight level above FL400 that can be flown on an IFR flight on this leg? #A) FL430 B) FL410 C) FL420 D) FL440
033-04 IFR (AIRWAYS) FLIGHT PLANNING 40 © 2008 AVIATIONEXAM.com 23874 (B) 23875 (B) 23876 (B) 23877 (B) 23878 (A) 23880 (D) 23881 (B) 23882 (C) 23883 (D) 23884 (D) 23885 (D) 23886 (D) 23887 (D) 23874. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly from ODIN (55°35 N 010°39 E) to LANDVETTER (57°39 N 012°17 E). What is the magnetic course on this route? A) 204° #B) 024° C) 052° D) 156° 23875. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly from SHILLING (57°33 N 014°00 E) to ALMA (55°25 N 013°34 E). What is the minimum grid safe altitude for this route? A) 2.700 ft #B) 3.200 ft C) 2.500 ft D) 2.900 ft 23876. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly on airways from ALMA (55°25 N 013°34 E) to SHILLING (57°33 N 014°00 E). What is the distance between these two points? A) 86 NM #B) 131NM C) 45 NM D) 60 NM 23877. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) An aircraft has to fly on airways from SVEDA (56°10 N 012°34 E) to SKARA (58°23 N 013°15 E). Which of the following is the correct route? A) SVD UB45 LAV UR156 SKA. #B) SVD UH40 PAPER UA9 BAK UB44 SKA. C) UR1 HIL UV30 BTD UH42 SKA. D) SVD UH40 PAPER UA9 BAK UR156 SKA. 23878. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) What is the meaning of the chart information for the navaid(s) LANDVETTER (57°39 N 012°17 E)? ##A) VORDME with identification LAV available on frequency 114,6 MHz. B) DME only with identification LAV available on frequency 114,6 MHz. C) Doppler VOR only with identification LAV available on frequency 114,6 MHz. D) VORDME and NDB with identification LAV available on frequency 114,6 MHz. 23880. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) The radio navigation aid(s) at (57°32 N 004°03 W) is/are: A) VORDME, frequency 109,2 kHz. B) VOR, frequency 109,2 MHz, for INS update only.
C) VOR, frequency 109,2 MHz, no DME available. #D) VORDME, frequency 109,2 MHz. 23881. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) The identifier of the radio navigation aid at (56°06 N 012°15 E) is: A) WX #B) NOA C) SVD04 D) NORA 23882. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) The identifier of the radio navigation aid at (56°07 N 012°58 E) is: A) SVD03 B) SVD #C) AOR D) ASTOR 23883. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) The radio navigation aid at (57°45 N 013°48 E) is a: A) VOR, frequency 355 MHz. B) NDB, frequency 355 MHz. C) VOR, frequency 355 kHz. #D) NDB, frequency 355 kHz. 23884. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) The radio navigation aid(s) at (55°26 N 011°38 E) is/are: A) NDB, frequency 112,8 kHz. B) VORDME, frequency 128,15 MHz. C) VORDME, frequency 128,75 MHz. #D) VORDME, frequency 112,8 MHz. 23885. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) The radio navigation aid(s) at (56°09 N 013°14 E) is/are: A) VOR/DME, frequency 116,2 MHz. B) VOR/DME, frequency 116,9 MHz. C) VOR, frequency 116,2 MHz. #D) VOR, frequency 116,9 MHz. 23886. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) The radio navigation aid(s) at (56°17 N 010°47 E) is/are: A) VOR/DME, frequency 374 kHz. B) NDB, frequency 374 kHz, for Temporary Use (TU). C) VOR, frequency 374 MHz. #D) NDB, frequency 374 kHz. 23887. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)2) The radio navigation aid(s) at (55°59 N 014°06 E) is/are: A) VOR/DME, frequency 116,9 MHz. B) NDB, frequency 116,9 khz. C) VOR, frequency 363 kHz. #D) NDB, frequency 363 kHz. 033-04 IFR (AIRWAYS) FLIGHT PLANNING 41 © 2008 AVIATIONEXAM.com 24745 (B) 24747 (B) 24749 (A) 24750 (B) 24753 (D) 24757 (D) 24846 (D) 24847 (A) 24848 (D) 24852 (B) 24889 (A) 24891 (C) 24892 (B)
24745. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual, London Heathrow, pages 10-2, 11-4 or figures AP-08, AP-09) Using STAR Biggin Two Alfa for ILS DME RWY 27R, What is the Initial Approach Fix? A) Epsom, 316. #B) Biggin, 115,1. C) IRR, 110,3. D) Ockham, 115,3. 24747. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual chart 5AT(HI) Route PTS P from VIGRA (62°33 N 006°02 E) to ADOBI (68°30 N 003°00 E). What is the grid track? A) 353° #B) 344° C) 173° D) 349° 24749. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(HI)4) What is the mean true course from Paris Charles de Gaulle to London Heathrow? #A) 321° (T) B) 312° (T) C) 322° (M) D) 142° (T) 24750. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MADRID, BARAJAS page 11-1 or figure AP-15) ILS DME RWY 33. What is the minimum altitude for glideslope interception? A) 3.500 ft #B) 4.000 ft C) 2.067 ft D) 1.567 ft 24753. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - Paris Charles de Gaulle - SID chart 20-3 or figure AP-03) What is the distance to Abbeville on SID ABB 8 A? A) 72 NM B) 74 NM C) 72,5 NM #D) 74,5 NM 24757. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - AMSTERDAM SCHIPOL 11-6 or figure AP-07) ILS DME RWY 22. Complete the blanks for the missed approach: Turn ___ on track ___° climbing to ___. A) left; 005; 2.000 ft (2.012 ft) B) left; 266; 2.000 ft (2.102 ft) C) right; 240; 2.000 ft (2.011 ft) #D) left; 160; 2.000 ft (2.014 ft) 24846. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(HI)3) Are the VOR and TACAN navaids at OSNABRUCH (52°12 N 008°17 E) co-located? A) Yes. B) VOR/DME only. C) VOR/NDB only. #D) No. 24847. (AIR: atpl, ir; HELI: atpl, ir)
(Refer to Jeppesen Manual chart E(HI)4) For a flight from Paris Charles de Gaulle to London Heathrow, what is the average true course? #A) 320° B) 300° C) 120° D) 140° 24848. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(LO)5) OSNABRUCH VOR and TACAN (52°12 N 008°17 E). What can be said about the VOR and TACAN? A) They are frequency paired. B) They are not frequency paired. C) They are frequency paired and have the same ident. #D) They are not frequency paired and have different idents. 24852. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart 5 AT(HI) The initial true course from A (65°N 006°E) to C (62°N 020°W) is: A) 272° #B) 266° C) 256° D) 246° 24889. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 5) This chart is a ___ projection with a scale of ___ . #A) Lambert Conformal Conic; 1 cm = 14,60 km B) transverse Mercator; 1 inch = 15 NM C) Mercator; 1 inch = 20 NM D) Lambert Conformal Conic; 1cm = 10,95 km 24891. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 6) Position NESLA at (49°48,6 N 002°44,4 E) is a ___. A) compulsory reporting point on both G40 and A5 B) non-compulsory reporting point on both G40 and A5 #C) compulsory reporting point G40 only D) non-compulsory reporting point on G40 only 24892. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 5) On what frequency could you expect to receive plain language in-flight weather information for Amsterdam? A) 123,70 MHz #B) 126,20 MHz C) 113,95 MHz D) 124,30 MHz 033-04 IFR (AIRWAYS) FLIGHT PLANNING 42 © 2008 AVIATIONEXAM.com 24894 (A) 24895 (D) 24897 (D) 24899 (D) 24900 (C) 24901 (D) 24903 (B) 24916 (D) 25013 (A) 25014 (B) 25015 (C) 24894. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 6) While flying IFR on A5 between PERON (49°54,8 N 002°50,4 E) and CAMBRAI (50°13,7 N 003°09,1 E) the highest suitable ICAO cruising level would be? #A) FL120 B) FL150 C) FL180
D) FL190 24895. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E(LO) 6) You plan to fly at FL180 from DRESDEN (51°00,9 N 013°35,9 E) to BAROM (50°02,5 N 010°43,9 E) when ED(R)-208 is active, your expected routing is: A) DRN Z715 BAROM. B) DRN Z715 DCT BAROM. C) as directed by ATC. #D) DRN A19 BAROM. 24897. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 5) Flying westbound overhead DOXON (55°26,9 N 018°10,0 E) you fly from ___ into ___. A) Warsaw FIR (ICAO code EPWW); Riga FIR (ICAO code EVRR) B) Latvia; Poland C) Riga FIR (ICAO code EVRR); Malmo FIR (ICAO code ESMM) #D) Riga FIR (ICAO code EVRR); Warsaw FIR (ICAO code EPWW) 24899. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 5) To positively identify the DENKO (52°49,0 N 015°50,1 E) NDB you must ensure the following radio/navigation equipment is on: A) the ADF with the Beat Frequency Oscillator (BFO) off. B) the VOR/DME. C) radio tuned to 134,22 MHz. #D) the ADF with the Beat Frequency Oscillator (BFO) on. 24900. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 6) Overhead STRASBOURG (48°30,4 N 007°34,4 E) the Grid MORA is? A) FL57 B) 5.500 ft #C) 5.700 ft D) 5.700 m 24901. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 6) Overhead PRAGUE (50°05,8 N 014°15,8 E) you should expect to communicate with Prague Control/Radar on: A) 112,60 MHz B) 127,90 MHz C) 120,47MHz #D) 134,00 MHZ 24903. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (LO) 5) You are flying along R12 on track, heading 030° (M) towards HELGOLAND (54°11,1 N 007°54,6 E) and you have 30 NM to run, your RMI indicates a QDM of ___ to HELGOLAND. A) 030° #B) 045° C) 225° D) 054° 24916. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (HI) 4) Your aircraft registered in the UK is outbound from London towards New York via UG1 and Shanwick CTA/FIR, prior to crossing W002 what should you have obtained:
A) airways clearance from London on 133,60 MHz. B) oceanic entry clearance on 133,80 MHz. C) oceanic entry clearance on123,95 MHz. #D) oceanic entry clearance on 127,65 MHz. 25013. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (HI) 4) You are cleared to route LANDS END (50°08,1 N 005°38,2 W) direct to HONILY (52°21,4 N 001°39,7 W) you estimate LANDS END at 09:57. TAS is 500 kts W/V is 270° (M)/50 kts What is your mean magnetic track and estimate for HONILY: #A) 055°, 1019. B) 048°, 1019. C) 053°, 1005. D) 048°, 1021. 25014. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - LONDON AREA chart) You are required to hold at BOVINGDON (51°43,6 N 000°33,0 W) however, the VOR is unserviceable. What procedure should now follow? A) Enter the BOVVA alternate hold which is on the 141° radial at 37 DME BIGGIN. #B) Enter the BOVVA alternate hold which STARTS AT 32 DME BIGGIN on 141° QDM. C) Enter the BOVVA alternate hold which starts at 37 DME BIGGIN on 141° QDM. D) Ask ATC for radar vectors instead. 25015. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (HI) 4) What navigation aids are available at CLACTON (51°50,9 N 001°09,0 E)? A) VOR/DME and NDB always. B) NDB only. #C) VOR/DME and NDB only when the VOR/DME is unserviceable. D) VOR/DME when the NDB is unserviceable. 033-04 IFR (AIRWAYS) FLIGHT PLANNING 43 © 2008 AVIATIONEXAM.com 25017 (B) 25019 (B) 25020 (D) 25022 (D) 25026 (C) 25028 (D) 25029 (A) 25031 (B) 25033 (D) 25035 (A) 25036 (C) 25037 (D) 25017. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (HI) 4) Regarding restricted airspace EG (D)-056 at (50°05 N 000°50 W) it is a: A) permanently active danger area from sea level up to FL550. #B) danger area from sea level up to 55.000 ft activated by NOTAM. C) restricted area from sea level up to 55.000 ft activated by NOTAM. D) permanently active danger area from sea level up to 55.000 ft. 25019. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (HI) 4) How could you confirm your position at SKESO (49°49,5 N 003°02,0 W) if BHD is unserviceable?
A) 339° QDR at 122 DME DIN. #B) 331° QDR at 29 DME GUR. C) 339° QDM at 122 DME DIN. D) 331° QDM at 29 DME GUR. 25020. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (HI) 4) The initial magnetic track and total distance from ROLAMPONT (47°54,4 N 005°15,0 E) to MONUR (49°51,6 N 002°47,3 E) along UB4 are: A) 322° and 99 NM. B) 328° and 53 NM. C) 321° and 69 NM. #D) 322° and 152 NM. 25022. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual chart E (HI) 5) Flying eastbound between BOLOGNA (44°32,2 N 011°17,5 E) and ANCONA (43°35,2 N 013°28,3 E) what is the minimum ICAO IFR cruising level? A) FL250 B) FL310 C) FL260 #D) FL330 25026. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MADRID BARAJAS 10-3H or figure AP-34) You are cleared on a NAVAS THREE DELTA departure, after passing ARGAS what is the maximum IAS in the turn to NVS and at what level should you be by NVS: A) 230 kts, 4.000 ft. B) 250 kts, 4.000 ft. #C) 230 kts, FL80 or above. D) 250 kts, FL80 or above. 25028. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart E (LO) 5) The solid green symbol 10 NM south west of EELDE (53°09,8 N 006°40,0 E) is: A) a VOR/DME with a Morse ident of EEL. B) an NDB with a Morse ident of VZ. C) a fan marker with a Morse ident of VZ. #D) a fan marker with a Morse ident of DN. 25029. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MUNICH 10-2B or figure AP-19) Standard arrival AALEN ONE TANGO with runway 26R in use, therefore your route and track miles to the IAF are expected to be: #A) AALEN - WLD - ROKIL - MBG, 90 NM. B) AALEN - WLD - ROKIL, 51 NM. C) AALEN - WLD - ROKIL, 124 NM. D) WLD - ROKIL, 10 NM. 25031. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - ZURICH 11-2 or figure AP-11) The MSA is based on the ___ and is ___ to the southeast of the reference point. A) aerodrome reference point; 8.600 ft #B) KLOTEN VOR; 8.600 ft C) aerodrome reference point; 5.300 ft D) KLOTEN VOR; 4.400 ft 25033. (AIR: atpl, ir; HELI: atpl, ir)
(Refer to Jeppesen Student Manual - AMSTERDAM SCHIPOL 11-3A or figure AP-36) The touchdown elevation for runway 27 is: A) 12 ft above mean sea level. B) 11 ft above mean sea level. C) 11 ft below mean sea level. #D) 12 ft below mean sea level. 25035. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - LONDON 11-4 or figure AP-09) The frequency, identification and localiser final approach QDM for runway 27R are: #A) 110,3 MHz, IRR, 274°. B) 109,5 MHz, ILL, 274°. C) 110,3 MHz, IRR, 094°. D) 113,6 MHZ, LON, 094°. 25036. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - charts E (LO) 5 and 6) It is August and you are flying overhead Latvia at 0200 Latvia standard time. What is the correct UTC time? A) 0500 hrs. B) 1400 hrs. #C) 2300 hrs. D) 2400 hrs. 25037. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MADRID BARAJAS 11-1 or figure AP-15) The final approach fix is ___ from the runway 33 displaced threshold. A) D1,1 B) D10,7 C) D7,1 #D) D4,7 033-04 IFR (AIRWAYS) FLIGHT PLANNING 44 © 2008 AVIATIONEXAM.com 25038 (A) 25039 (C) 25059 (C) 25061 (C) 25065 (B) 25071 (A) 25073 (A) 25074 (B) 25096 (B) 25097 (C) 25098 (B) 25099 (C) 25038. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - AMSTERDAM SCHIPOL 13-5 or figure AP-37) When carrying out the procedure turn in a category A aeroplane what outbound QDR should you fly: #A) 122° B) 140° C) 266° D) 091° 25039. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MUNICH 11-4 or figure AP-01) If the glidescope was out while carrying out an ILS approach to runway 26R when 4,0 DME your recommended altitude is: A) 1.001 ft B) 2.660 ft #C) 2.450 ft D) 1.211 ft
25059. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart E (HI) 4) You are flying overhead TANGO (48°37,2 N 009°15,6 E) at 0947 maintaining TAS of 480 kts experiencing a 50 kts headwind component while routing UG313 KPT UG60 BRENO UA12 BZO. Your estimate for the LOVV/LIMM FIR boundary is? A) 0958 hrs. B) 0956 hrs. #C) 1005 hrs. D) 1015 hrs. 25061. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart E (LO) 5) The airspace ED (R)-74 centered on 52°25 N 011°30 E is usually active: A) from ground to 39.000 ft AMSL, Monday 0700 to Friday 1800 UTC. B) from MSL to FL39, Monday to Friday 0700 - 1800 LT. #C) from ground to 3.900 ft AMSL, Monday 0700 to Friday 1800 LT. D) activated only by NOTAM. 25065. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-76) Flying north bound just out of Moscow at FL120. What sort of in-flight weather hazard might be encountered? A) None. #B) Moderate icing and turbulence. C) Moderate icing and severe turbulence. D) Severe icing and moderate turbulence. 25071. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart (LO) 5) Regarding airway G5 between HAMBURG (53°41,1 N 010°12,3 E) and GEDSER (54°37,1 N 011°56,0 E) it is true to say: #A) the total distance is 82 NM, FL180 is a suitable IFR level. B) the total distance is 82 NM, FL170 is a suitable IFR level. C) the total distance is 60 NM, FL180 is a suitable IFR level. D) the total distance is 60 NM, FL170 is a suitable IFR level. 25073. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart E (HI) 5) Who should you make your position report to on passing LYON (45°43,5 N 005°05,4 E) if you are maintaining FL350 northwest bound along UA2: #A) Marseille control on 132,25 MHz. B) Marseille control on 133,42 MHz. C) Marseille control on 134,10 MHz. D) Marseille control on 125,85 MHz. 25074. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart E (LO) 6) The symbol at BOULOGNE (50°37,5 N 001°54,5 E) has the meaning: A) VOR/DME ON 113,80 MHz and a compulsory point. #B) VOR on 113,80 MHz and a compulsory reporting point. C) VOR on 113,80 MHz and on request reporting point. D) a compulsory reporting point with no associated navigation aid. 25096. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart E(HI)4 ) To the east of Koksy (51°06 N 002°39 E): A) airway UJ 34 is available not below FL300.
#B) a plain language inflight weather service is available on 127,8 MHz. C) maastricht Control/Radar is the Control Service for use within the portrayed boundaries below FL245. D) brussels Control is the Control Service for use within the portrayed boundaries at FL245 and above. 25097. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart E(LO)1 ) The altimeter setting to be used is: A) QNE. B) QNH until above transition level thereafter QNE. #C) QNH until above transition altitude thereafter QNE. D) QNE until below transition altitude thereafter QNH. 25098. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart E(HI)4 ) Airway UL3 at GIBSO intersection (50°45N 002°30W): A) is available eastbound only. #B) is available at 1000LT on a public holiday. C) is available westbound to Gibso routing thereafter via UR14 below FL245. D) is a Diversionary Route only. 25099. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MADRID BARAJAS (10-2B) or figure AP-13) The IAF for runway 33 arrivals from Airway A869 is: A) CJN. B) ADUXO. #C) a frequency paired VOR and DME. D) CJN and a frequency paired VOR and DME. 033-04 IFR (AIRWAYS) FLIGHT PLANNING 45 © 2008 AVIATIONEXAM.com 25100 (B) 25101 (B) 25106 (B) 25107 (B) 25108 (C) 25109 (D) 25110 (C) 25111 (A) 25112 (A) 25113 (D) 25114 (D) 25115 (C) 25100. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - Munich SID (10-3D) or figure AP-10) Pilots departing Munich via a KPT 5S departure: A) when airborne should contact Munich Departure on 127,95. #B) should climb to FL70. C) may climb to FL110. D) should remain below transition altitude 5.000 feet until otherwise instructed by ATC. 25101. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - Paris Charles-deGaulle - STAR chart (20-2) or figure AP-04) Turboprop aircraft arriving via Chievres should expect: A) a CIV 1P arrival crossing the IAF at FL110. #B) a CIV 1P arrival crossing the IAF at FL60. C) a CIV 1W arrival crossing the IAF at FL110. D) a CIV 1W arrival crossing the IAF at FL80. 25106. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart E(HI)4) An appropriate flight level for flight on airway UR 106 from Rambouillet (48°39,2 N 001°59,7 E) is: A) FL310 #B) FL290
C) FL300 D) FL320 25107. (AIR: atpl, ir; HELI: atpl, ir) An appropriate flight level for IFR flight in accordance with semi-circular height rules on a course of 360° (M) is: A) FL200 #B) FL210 C) FL220 D) FL240 25108. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MUNICH ILS Rwy 26R (11-4) or figure AP-01) The height of the aircraft at the Final Approach Fix (FAF) for the ILS runway 26R is: A) 1.649 feet B) 1.850 feet #C) 3.551 feet D) 5.000 feet 25109. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MUNICH ILS Rwy 26R (11-4) or figure AP-01) DMN is a: A) NDB facility. B) ILS facility with paired DME reading zero NM at runway threshold. C) VOR facility with paired DME reading zero NM at runway threshold. #D) DME facility reading 1 NM at runway threshold. 25110. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - AMSTERDAM SCHIPOL ILS/DME Rwy 22 (11-6) or figure AP-07) The intermediate fix is shown at: A) D6,0 SPL VOR. B) D6,2 SCH ILS. #C) D9,9 SPL VOR. D) D11,7 SPL VOR. 25111. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - LONDON HEATHROW ILS DME Rwy 09R (11-1A) or figure AP-39) The height indicated by the radio altimeter at DA for a CAT II equipped aircraft is: #A) 100 ft B) 175 ft C) 150 ft D) 225 ft 25112. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - Munich NDB DME RW 26L (16-3) or figure AP-02) The frequency and identifier of the NDB for the published approach are: #A) 400 MSW. B) 338 MNW. C) 108,6 DMS. D) 112,3 MUN. 25113. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - Munich NDB DME RW 26L (16-3) or figure AP-02) The missed approach procedure should be executed at or before: A) 0,5 NM from runway 26L threshold.
B) 1,5 NM from runway 26L threshold. C) D1,5 DMS. #D) 0,5 NM from runway 26L threshold and D1,5 DMS. 25114. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MUNICH ILS Rwy 08R (11-2) or figure AP-35) The lowest published authorised RVR for an ILS approach, glide slope out, all other aids serviceable, aeroplane category A, is: A) 1.500 m B) 600 m C) 800 m #D) 720 m 25115. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - MUNICH ILS Rwy 08R (11-2) or figure AP-35) The highest Minimum Safe Altitude (MSA) providing 1.000 feet clearance from obstructions within a radius of 25 NM centered on the MNW locator is ___, while the highest portrayed terrain high point or man-made structure in the chart planview is ___. A) 3.200 feet; 2.631 feet B) 3.200 feet; 3.700 feet #C) 3.700 feet; 2.631 feet D) 3.700 feet; 3.200 feet 033-04 IFR (AIRWAYS) FLIGHT PLANNING 46 © 2008 AVIATIONEXAM.com 25123 (C) 28319 (B) 28321 (C) 1118 (D) 1144 (A) 1147 (A) 1153 (C) 1154 (A) 1177 (B) 1180 (C) 25123. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Manual - chart NAP) Given an initial true heading at Shannon of 270° and a compass deviation of +3°, the corresponding compass heading would be: A) 265° B) 273° #C) 275° D) 281° 28319. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual E(HI)5) The magnetic course/distance from TANGO TGO 112.5 (48°37 N 009°16 E) to DINKELSBUHL DKB 117.8 (49°09 N 010°14 E) on airway UR11 is: A) 007°/60 NM. #B) 052°/50 NM. C) 105°/105 NM. D) 132°/43 NM. 28321. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Manual - London Heathrow, 11-1, ILS DME Rwy 09R) What is the Minimum Descent Altitude (MDA) for an ILS glide slope out? A) 275 ft. B) 405 ft. #C) 480 ft. D) 200 ft. 033-04-03 General flight planning tasks
1118. (AIR: atpl, ir) An aircraft is flying at MACH 0,84 at FL330. The static air temperature is -48 °C and the headwind component 52 kts. At 1338 UTC the controller requests the pilot to cross the meridian of 030W at 1500 UTC. Given the distance to go is 570 NM, the reduced Mach Number should be: A) 0,72 B) 0,78 C) 0,76 #D) 0,80 1144. (AIR: atpl, ir; HELI: atpl, ir) A public transport aeroplane with reciprocating engines is flying from PARlS to LYON. The final reserve corresponds to: #A) 45 minutes at holding speed. B) 2 hours at cruise consumption. C) 1 hour at holding speed. D) 30 minutes at holding speed. 1147. (AIR: atpl, ir; HELI: atpl, ir) A turbine-engined aircraft burns fuel at 200 gals per hour (GPH) with a Fuel Density of 0,8. What is the fuel flow if Fuel Density is 0,75? #A) 213 GPH B) 208 GPH C) 200 GPH D) 188 GPH 1153. (AIR: atpl, ir; HELI: atpl, ir) Given: True course (TC) 017° W/V 340°/30 kts True air speed (TAS) 420 kts Find: Wind correction angle (WCA) and ground speed (GS): A) WCA -2°, GS 426 kts. B) WCA +2°, GS 396 kts. #C) WCA -2°, GS 396 kts. D) WCA +2°, GS 416 kts. 1154. (AIR: atpl, ir; HELI: atpl, ir) Flight planning chart for an aeroplane states, that the time to reach the cruising level at a given gross mass is 36 minutes and the distance travelled is 157 NM (zero-wind). What will be the distance travelled with an average tailwind component of 60 kts? #A) 193 NM B) 128 NM C) 157 NM D) 228 NM 1177. (AIR: atpl, ir; HELI: atpl, ir) An aeroplane flies at an airspeed of 380 kts. lt flies from A to B and back to A. Distance AB = 480 NM. When going from A to B, it experiences a headwind component = 60 kts. The wind remains constant. The duration of the flight will be: A) 3 hrs 00 min #B) 2 hrs 35 min C) 2 hrs 10 min D) 2 hrs 32 min 1180. (AIR: atpl, ir; HELI: atpl, ir) A multi-engined AC on IFR flight. Given: Trip fuel 65 USG Contingency 5% trip
Alternate fuel including final reserve 17 USG Useable fuel at departure 93 USG At a point halfway to destination, fuel consumed is 40 USG Assuming fuel consumption is unchanged Which of the following is correct? A) At departure Reserve Fuel was 28 USG. B) At destination required reserves remain intact. #C) Remaining fuel is insufficient to reach destination with reserves intact. D) Remaining fuel is insufficient to reach destination. 033-04 IFR (AIRWAYS) FLIGHT PLANNING 47 © 2008 AVIATIONEXAM.com 1182 (A) 1193 (A) 1199 (A) 1215 (D) 1220 (D) 1268 (C) 1281 (C) 1292 (C) 2190 (A) 2191 (A) 2230 (B) 2239 (B) 2255 (D) 1182. (AIR: atpl, ir; HELI: atpl, ir) The fuel burn of an aircraft turbine engine is 220 l/hrs with a fuel density of 0,80. If the density is 0,75, the fuel burn will be: #A) 235 l/hrs B) 206 l/hrs C) 220 l/hrs D) 176 l/hrs 1193. (AIR: atpl, ir; HELI: atpl, ir) An aircraft is in cruising flight at FL095, GS 155 kts. The pilot intends to descend at 500 ft/min to arrive overhead the MAN VOR at 2.000 ft (QNH 1.030hPa). The TAS remains constant in the descent, wind is negligible, temperature standard. At which distance from MAN should the pilot commence the descent? #A) 41 NM B) 48 NM C) 38 NM D) 45 NM 1199. (AIR: atpl, ir; HELI: atpl, ir) An executive pilot is to carry out a flight to a French aerodrome, spend the night there and return the next day. Where will he find the information concerning parking and landing fees? #A) In the FAL section of the French Aeronautical Information Publication (AIP). B) In the AGA chapter of the French Aeronautical Information Publication (AIP). C) In the GEN chapter of the French Aeronautical Information Publication (AIP). D) By telephoning the aerodrome s local chamber of commerce, this type of information not being published. 1215. (AIR: atpl, ir; HELI: atpl, ir) Where would you find information regarding Customs and Health facilities? A) ATCC broadcasts. B) NOTAM s. C) NAV/RAD supplements. #D) AIP s. 1220. (AIR: atpl, ir; HELI: atpl, ir) Where would you find information regarding Search and Rescue procedures?
A) ATCC broadcasts. B) NOTAM. C) SIGMET. #D) AIP. 1268. (AIR: atpl, ir; HELI: atpl, ir) A sector distance is 450 NM long. The TAS is 460 kts. The wind component is 50 kts tailwind. What is the still air distance? A) 414 Nautical Air Miles (NAM). B) 499 Nautical Air Miles (NAM). #C) 406 Nautical Air Miles (NAM). D) 511 Nautical Air Miles (NAM). 1281. (AIR: atpl, ir; HELI: atpl, ir) The still air distance in the climb is 189 Nautical Air Miles (NAM) and time 30 minutes. What ground distance would be covered in a 30 kts head wind? A) 188 NM B) 203 NM #C) 174 NM D) 193 NM 1292. (AIR: atpl, ir; HELI: atpl, ir) The fuel burn - off is 200 kg/hrs with a relative fuel density of 0,8. If the relative fuel density is 0,75, the fuel burn will be: A) 267 kg/hrs B) 213 kg/hrs #C) 200 kg/hrs D) 188 kg/hrs 2190. (AIR: atpl, ir; HELI: atpl, ir) From which of the following would you expect to find information regarding known short unserviceability of VOR, TACAN, and NDB? #A) NOTAM. B) AIP (Air Information Publication). C) SIGMET. D) ATCC broadcasts. 2191. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figure 033-01) Given: Aerodrome elevation 2.500 ft OAT +10 °C Initial weight: 3.500 lbs Climb to FL140 OAT -5 °C What is the climb time, fuel, and NAM? #A) 22 min, 6,5 GAL, 46 NAM. B) 24 min, 7,5 GAL, 50 NAM. C) 2 min, 1,0 GAL, 4 NAM. D) 26 min, 8,5 GAL, 54 NAM. 2230. (AIR: atpl, ir; HELI: atpl, ir) From which of the following would you expect to find the dates and times when temporary danger areas are active? A) Only AIP (Air Information Publication). #B) NOTAM and AIP (Air Information Publication). C) SIGMET. D) RAD/NAV charts. 2239. (AIR: atpl, ir; HELI: atpl, ir) From which of the following would you expect to find details of the Search and Rescue organisation and procedures (SAR)? A) ATCC broadcasts.
#B) AIP (Air Information Publication). C) NOTAM. D) SIGMET. 2255. (AIR: atpl, ir; HELI: atpl, ir) From which of the following would you expect to find facilitation information (FAL) regarding customs and health formalities? A) NOTAM. B) NAV/RAD charts. C) ATCC. #D) AIP (Air Information Publication). 033-04 IFR (AIRWAYS) FLIGHT PLANNING 48 © 2008 AVIATIONEXAM.com 12240 (C) 12248 (D) 12527 (A) 12556 (B) 12557 (D) 12558 (B) 12563 (C) 12564 (D) 12565 (C) 12566 (D) 12567 (B) 12568 (B) 12240. (AIR: atpl, ir; HELI: atpl, ir) You are flying a constant compass heading of 252°. Variation is 22°E, deviation is 3°W and your INS is showing a drift of 9° to the right. True track is? A) 242° B) 262° #C) 280° D) 224° 12248. (AIR: atpl, ir) (Refer to figure 033-37) Planning an IFR-flight from Paris to London for the twin jet aeroplane. Given: Estimated Landing Mass: 49.700 kg FL280 W/V 280°/40 kts Average True Course: 320° Procedure for descent: 0,74 M/250 KIAS Determine the time from the top of descent to London (elevation 80 ft). A) 10 min B) 17 min C) 8 min #D) 19 min 12527. (AIR: atpl, ir; HELI: atpl, ir) (Refer to figures 033-71) True Air speed: 170 kts Wind in the area: 270° / 40 kts According to the attached the navigation log, an aircraft performs a turn overhead BULEN to reroute to ARD via TGJ. The given wind conditions remaining constant. The fuel consumption during the turn is 20 litres. The total fuel consumption at position overhead ARD will be: #A) 1.545 litres B) 1.182 litres C) 1.326 litres D) 1.600 litres 12556. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-24) On a direct great circle course from Shannon (52°43 N 008°53 W) to Gander (48°54 N 054°32 W), what is the average true course and distance? A) 281°, 1.877 NM.
#B) 262°, 1.720 NM. C) 281°, 2.730 NM. D) 244°, 1.520 NM. 12557. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart 5 AT(HI) or figure HI-25) The initial great circle true course from Keflavik (64°00 N 022°36 W) to Vigra (62°33 N 006°02 E) measures 084°. On a polar enroute chart where the grid is aligned with the 000° meridian the initial grid course will be: A) 080° B) 096° C) 066° #D) 106° 12558. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart 5 AT(HI) or figures HI-18_a and HI-18_b) The initial great circle course from position A (80°N 170°E) to position B (75°N 011°E) is 177° (G). The final grid course at position B will be: A) 353° (G) #B) 177° (G) C) 194° (G) D) 172° (G) 12563. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-23) The average magnetic course from C (62°N 020 W) to B (58°N 004 E) is: A) 099° B) 118° #C) 119° D) 109° 12564. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-23) The average true course from C (62°N 020 W) to B (58°N 004 E) is: A) 119° B) 099° C) 120° #D) 109° 12565. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-23) The initial magnetic course from C (62°N 020°W) to B (58°N 004°E) is: A) 098° B) 113° #C) 116° D) 080° 12566. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-23) The initial true course from C (62°N 020°W) to B (58°N 004°E) is: A) 116° B) 080° C) 278° #D) 098° 12567. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-23) The distance (NM) from C (62°N 020°W) to B (58°N 004°E) is: A) 775
#B) 760 C) 725 D) 700 12568. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-23) The distance (NM) from A (64°N 006°E) to C (62°N 020°W) is: A) 1.440 #B) 720 C) 690 D) 1.590 033-04 IFR (AIRWAYS) FLIGHT PLANNING 49 © 2008 AVIATIONEXAM.com 12569 (D) 12570 (A) 12571 (A) 23739 (A) 23863 (D) 28322 (B) 28344 (D) 28345 (B) 12569. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-23) The average magnetic course from A (64°N 006°E) to C (62°N 020°W) is: A) 259° B) 247° C) 279° #D) 271° 12570. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-23) The average true course from A (64°N 006°E) to C (62°N 020°W) is: #A) 259°. B) 247°. C) 271°. D) 079°. 12571. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Route Manual chart NAP or figure HI-23) The initial true course from A (64°N 006°E) to C (62°N 020°W) is: #A) 271° B) 275° C) 267° D) 246° 23739. (AIR: atpl, ir) A twin-jet aeroplane carries out the WASHINGTON - PARIS flight. When it reaches point K (35°N 048°W) a non-mechanical event makes the Captain consider rerouting to one of the three following fields. The flight conditions are: from K to BERMUDAS (distance 847 NM, headwind component 18 kts) from K to SANTA MARIA (distance 1.112 NM, tailwind component 120 kts) from K to GANDER (distance 883 NM, wind component 0) With an aeroplane true airspeed of 460 kts, the field selected will be that more rapidly reached: #A) BERMUDAS, GANDER, or SANTA MARIA. B) SANTA MARIA. C) BERMUDAS. D) either GANDER or BERMUDAS. 23863. (AIR: atpl, ir; HELI: atpl, ir) (Refer to Jeppesen Student Route Manual chart E(HI)1) An aircraft has to fly from the airport at Aberdeen (57°19 N
002°16 W) to the airport at Benbecula (57°29 N 007°22 W). Given: Time to climb: 11 min Time to descend: 9 min TAS: 170 kts W/V: 230/50 What is the flight time during the cruise? A) 16 min B) 47 min C) 28 min #D) 54 min 28322. (AIR: atpl) LFPG ILS Rwy 09: The ILS localizer course is: A) 100° #B) 088° C) 118° D) 268° 28344. (AIR: atpl, ir; HELI: atpl, ir) Which approach segment starts at the point were you report established ? A) Final approach. B) Initial approach. C) Go around. #D) Intermediate approach. 28345. (AIR: atpl, ir; HELI: atpl, ir) Which approach segment starts at the FAF and ends at the MAP? A) Initial approach. #B) Final approach. C) Go around. D) Intermediate approach. 033-05 JET AEROPLANES FLIGHT PLANNING 50 © 2008 AVIATIONEXAM.com 1128 (B) 1136 (D) 1140 (B) 1143 (B) 1148 (A) 1149 (C) 1151 (D) 1152 (B) 1160 (C) 1162 (D) 033-05-01 Advanced flight planning aspects for jet aeroplanes 1128. (AIR: atpl) What is decision point procedure? It is a procedure to reduce the amount of fuel carried on a flight by: A) reducing contingency fuel from 10% to 5% of trip fuel. #B) reducing contingency fuel to only that required from decision point to destination. C) reducing trip fuel to only that required from decision aerodrome to destination. D) reducing trip distance. 1136. (AIR: atpl) (Refer to figures 033-23) Given: Brake release mass: 62.000 kg Temperature: ISA + 15 °C The fuel required for a climb from Sea Level to FL330 is: A) 1.800 kg B) 1.650 kg C) 1.750 kg #D) 1.700 kg 1140. (AIR: atpl) (Refer to figure 033-21)
The fuel required for 30 minutes holding, in a racetrack pattern, at PA 1.500 ft, at mean gross mass of 45.000 kg, is: A) 1.010 kg #B) 1.090 kg C) 1.310 kg D) 2.180 kg 1143. (AIR: atpl) (Refer to figures 033-25 and 033-36) Given: Distance B - C: 350 NM Cruise 300 KIAS at FL210 Temperature: - 40 °C Tailwind component: 70 kts Gross mass at B: 53.200 kg The fuel required from B - C is? A) 1.810 kg #B) 1.940 kg C) 2.800 kg D) 2.670 kg 1148. (AIR: atpl) (Refer to figure 033-21) The fuel required for 45 minutes holding, in a racetrack pattern, at PA 5.000 ft, mean gross mass 47.000 kg, is: #A) 1.635 kg B) 1.090 kg C) 1.690 kg D) 1.125 kg 1149. (AIR: atpl) (Refer to figure 033-19) Given: Head wind component 50 kts Temperature ISA + 10 °C Brake release mass 65.000 kg Trip fuel available 18.000 kg What is the maximum possible trip distance? A) 3.480 NM B) 3.100 NM #C) 2.740 NM D) 2.540 NM 1151. (AIR: atpl) (Refer to figure 033-15) For a flight of 2.800 ground nautical miles the following applies: Head wind component: 15 kts Temperature: ISA + 15 °C Cruise altitude: 35.000 ft Landing mass: 50.000 kg The trip fuel and trip time respectively are: A) 20.000 kg; 7 hrs 00 min. B) 16.200 kg; 6 hrs 20 min. C) 17.000 kg; 6 hrs 10 min. #D) 17.600 kg; 6 hrs 50 min. 1152. (AIR: atpl) The Trip Fuel for a jet aeroplane to fly from the departure aerodrome to the destination aerodrome is 5.350 kg. Fuel consumption in holding mode is 6.000 kg/hrs. The quantity of fuel which is needed to carry out one go-around and land on the alternate airfield is 4.380 kg. The destination aerodrome has a single runway. What is the minimum quantity of fuel which should be on board at takeoff? A) 13.000 kg #B) 13.230 kg
C) 14.730 kg D) 11.730 kg 1160. (AIR: atpl) (Refer to figure 033-19) For a flight of 2.800 ground nautical miles the following applies: Head wind component: 20 kts Temperature: ISA + 15 °C Brake release mass: 64.700 kg The trip fuel and trip time respectively are: A) 16.200 kg; 6 hrs 20 min. B) 15.800 kg; 6 hrs 15 min. #C) 17.000 kg; 6 hrs 45 min. D) 18.400 kg; 7 hrs 00 min. 1162. (AIR: atpl) A turbo-jet AC is enroute to an isolated destination. On top of taxi, trip and contingency fuel, what fuel is required? A) Greater of 45 mins + 15% of trip or 2 hours. B) 30 mins holding at 450 m AMSL. C) 30 mins holding at 450 m AAL. #D) 2 hours at normal cruise consumption. 033-05 JET AEROPLANES FLIGHT PLANNING 51 © 2008 AVIATIONEXAM.com 1163 (B) 1178 (D) 1179 (B) 1184 (A) 1186 (C) 1189 (B) 1196 (B) 1197 (B) 1198 (A) 1163. (AIR: atpl) (Refer to figures 033-25 and 033-28) Given: Distance C-D: 680 NM Long Range Cruise at FL340 Temperature Deviation from ISA: 0 °C Headwind component: 60 kts Gross mass at C: 44.700 kg The fuel required from C - D is: A) 3.400 kg #B) 3.700 kg C) 3.100 kg D) 4.000 kg 1178. (AIR: atpl) (Refer to figure 033-19) The following apply: Temperature ISA +15 °C Brake release mass 62.000 kg Trip time 5 hrs 20 min What is the trip fuel? A) 13.800 kg. B) 13.000 kg. C) 13.200 kg. #D) 13.500 kg. 1179. (AIR: atpl) Which is true regarding a balanced field? A) Provides largest gap between net and gross margins. #B) Provides minimum field length required in the case of an engine failure. C) Takeoff distance will always be more than stopping distance. D) Distances will remain equal, even if engine failure speed is changed. 1184. (AIR: atpl)
(Refer to figure 033-15) For a flight of 2.400 ground nautical miles the following apply: Tail wind component: 25 kts Temperature: ISA -10 °C Cruise altitude: 31.000 ft Landing mass: 52.000 kg The trip fuel and trip time respectively are: #A) 14.200 kg; 5 hrs 30 min. B) 16.200 kg; 5 hrs 45 min. C) 13.600 kg; 6 hrs 30 min. D) 12.000k g; 5 hrs 15 min. 1186. (AIR: atpl) (Refer to figure 033-19) The following apply: Tail wind component 10 kts Temperature ISA +10 °C Brake release mass 63.000 kg Trip fuel available 20.000 kg What is the maximum possible trip distance? A) 3.500 NM B) 3.640 NM #C) 3.740 NM D) 3.250 NM 1189. (AIR: atpl) (Refer to figures 033-25 and 033-35) Given: Distance B-C: 1.200 NM Cruise Mach 0,78 at FL300 Temperature Deviation from ISA: -14 °C Tailwind component: 40 kts Gross mass at B: 50.200 kg The fuel required from B to C is: A) 5.850 kg #B) 6.150 kg C) 7.300 kg D) 7.050 kg 1196. (AIR: atpl) (Refer to figures 033-25 and 033-36) Given: Distance C-D: 540 NM Cruise 300 KIAS at FL210 Temperature Deviation from ISA: +20 °C Headwind component: 50 kts Gross mass at C: 60.000 kg The fuel required from C to D is: A) 3.680 kg #B) 4.200 kg C) 3.350 kg D) 4.620 kg 1197. (AIR: atpl) Given: Dry operating mass (DOM): 33.510 kg Load: 7.600 kg Trip fuel (TF): 2.040 kg Final reserve fuel: 983 kg Alternate fuel: 1.100 kg Contingency fuel: 5% of trip fuel Which of the listed estimated masses is correct? A) Estimated takeoff mass is 45.233 kg. #B) Estimated landing mass at destination is 43.295 kg.
C) Estimated landing mass at destination is 43.193 kg. D) Estimated takeoff mass is 43.295 kg. 1198. (AIR: atpl) What is the purpose of decision point procedure? #A) Carry minimum fuel to increase Traffic Load. B) Increase safety of the flight. C) Reduce landing mass to avoid stressing the aircraft. D) To assist in decision making at refuelling. 033-05 JET AEROPLANES FLIGHT PLANNING 52 © 2008 AVIATIONEXAM.com 1201 (C) 1203 (D) 1204 (D) 1206 (D) 1207 (D) 1225 (C) 2181 (A) 2251 (B) 1201. (AIR: atpl) Turbo-jet AC: Taxi fuel: 600 kg Fuel flow cruise: 10.000 kg/hrs Fuel flow hold: 8.000 kg/hrs Alternate fuel: 10.200 kg Flight time: 6 hours Visibility at destination: 2.000 m What is the minimum ramp fuel? A) 80.500 kg B) 79.200 kg #C) 77.800 kg D) 76.100 kg 1203. (AIR: atpl) Given: Maximum allowable takeoff mass: 64.400 kg Maximum landing mass: 56.200 kg Maximum zero fuel mass: 53.000 kg Dry operating mass: 35.500 kg Estimated load: 14.500 kg Estimated trip fuel: 4.900kg Minimum takeoff fuel: 7.400 kg Find the maximum allowable takeoff fuel: A) 8.600 kg B) 11.400 kg C) 14.400 kg #D) 11.100 kg 1204. (AIR: atpl) Following in-flight depressurisation, a turbine powered aeroplane is forced to divert to an enroute alternate airfield. If actual flight conditions are as forecast, the minimum quantity of fuel remaining on arrival at the airfield will be: A) at least equivalent to 45 minutes flying time. B) at least equivalent to the quantity required to fly to another aerodrome in the event that weather conditions so require. C) laid down by the operator, with the quantity being specified in the operating manual. #D) at least equivalent to 30 minutes flying time. 1206. (AIR: atpl) (Refer to figure 033-15) For a flight of 2.400 ground nautical miles the following apply: Temperature: ISA -10 °C Cruise altitude: 29.000 ft Landing mass: 45.000 kg Trip fuel available: 16.000 kg
What is the maximum headwind component which may be accepted? A) zero B) 15 kts C) 70 kts #D) 35 kts 1207. (AIR: atpl) (Refer to figure 033-20) Given: Distance to Alternate: 450 NM Landing mass at Alternate: 45.000 kg Tailwind component: 50 kts The Alternate fuel required is: A) 2.900 kg B) 2.750 kg C) 3.050 kg #D) 2.500 kg 1225. (AIR: atpl) Given: Maximum allowable takeoff mass: 64.400 kg Maximum landing mass: 56.200 kg Maximum zero fuel mass: 53.000 kg Dry operating mass: 35.500 kg Estimated load: 14.500 kg Estimated trip fuel: 4.900 kg Minimum takeoff fuel: 7.400 kg Find maximum additional load: A) 7.000 kg B) 4.000 kg #C) 3.000 kg D) 5.600 kg 2181. (AIR: atpl) An aeroplane has the following masses: Estimated LM: 50.000 kg Trip fuel: 4.300 kg Contingency fuel: 215 kg Alternate fuel (final reserve included): 2.100kg Taxi: 500 kg Block fuel: 7.115 kg Before departure the captain orders to make the block fuel 9 000 kg. The trip fuel in the operational flight plan should read: #A) 4.300 kg B) 6.185 kg C) 9.000 kg D) 6.400 kg 2251. (AIR: atpl) (Refer to figure 033-12) Find the optimum altitude for the twin jet aeroplane, given: Cruise mass: 50.000 kg MACH 0,78 A) 36.200 ft. #B) 35.500 ft. C) 36.700 ft. D) maximum operating altitude. 033-05 JET AEROPLANES FLIGHT PLANNING 53 © 2008 AVIATIONEXAM.com
2252 (A) 2260 (A) 2261 (A) 2262 (D) 2264 (B) 2265 (D) 2267 (B) 2272 (C) 2273 (C) 2274 (B) 2252. (AIR: atpl) (Refer to figure 033-12 and 033-65) Find the fuel mileage penalty for the twin jet aeroplane with regard to the given flight level. Given: Long range cruise Cruise mass: 53.000 kg FL310 #A) 4% B) 1% C) 10% D) 0% 2260. (AIR: atpl) (Refer to figure 033-15) For a flight of 2.400 ground nautical miles the following apply: Temperature: ISA -1° C Cruise altitude: 29.000 ft Landing mass: 45.000 kg Trip fuel available: 16.000 kg What is the maximum headwind component which may be accepted? #A) 35 kts B) 15 kts C) 0 kts D) 70 kts 2261. (AIR: atpl) (Refer to figure 033-39) ETOPS - AC can not travel more than 120 minutes from a suitable (should read adequate) airfield. Assume LRC and diversion weight of 40.000 kg, what is the still air diversion distance? #A) 735 B) 794 C) 810 D) 875 2262. (AIR: atpl) (Refer to figures 033-25 and 033-28) Long range cruise at FL340 Distance C-D: 3.200 NM Temperature: deviation from ISA +12 °C Tailwind component: 50 kts Gross mass at C: 55.000 kg The fuel required from C to D is: A) 17.500 kg B) 14.200 kg C) 17.800 kg #D) 14.500 kg 2264. (AIR: atpl) Mark the correct statement. If a decision point procedure is applied for flight planning: A) the trip fuel to the destination aerodrome is to be calculated via the suitable enroute alternate. #B) the trip fuel to the destination aerodrome is to be calculated via the decision point. C) a destination alternate is not required. D) the fuel calculation is based on a contingency fuel from departure aerodrome to the decision point. 2265. (AIR: atpl) (Refer to figure 033-15)
Tail wind component: 45 kts Temperature: ISA -10 °C Cruise altitude: 29.000 ft Landing mass: 55.000 kg For a flight of 2.800 ground nautical miles, the trip fuel and trip time respectively are: A) 16.000 kg; 6 hrs 25 min. B) 18.000 kg; 5 hrs 50 min. C) 20.000 kg; 6 hrs 40 min. #D) 17.100 kg; 6 hrs 07 min. 2267. (AIR: atpl) (Refer to figure 033-20) Distance to alternate: 400 NM Landing mass at alternate: 50.000kg Headwind component: 25 kts The alternate fuel required is: A) 2.550 kg #B) 2.800 kg C) 2.900 kg D) 2.650 kg 2272. (AIR: atpl) The quantity of fuel which is calculated to be necessary for a jet aeroplane to fly IFR from departure aerodrome to the destination aerodrome is 5.352 kg. Fuel consumption in holding mode is 6.000 kg/hrs. Alternate fuel is 4.380 kg. Contingency should be 5% of trip fuel. What is the minimum required quantity of fuel which should be on board at takeoff? A) 13.370 kg B) 14.500 kg #C) 13.000 kg D) 13.220 kg 2273. (AIR: atpl) (Refer to figure 033-27) Given: LRC FL330 Temp -63 °C Mass 54.100 kg Time 29 min Find the fuel consumed. A) 1.207 kg B) 1.197 kg #C) 1.100 kg D) 1.000 kg 2274. (AIR: atpl) The required time for final reserve fuel for turbojet aeroplane is: A) 45 min. #B) 30 min. C) 60 min. D) variable with wind velocity. 033-05 JET AEROPLANES FLIGHT PLANNING 54 © 2008 AVIATIONEXAM.com 2276 (D) 2277 (A) 2280 (A) 2285 (C) 2287 (D) 2294 (B) 2295 (B) 2299 (D) 2276. (AIR: atpl) (Refer to figure 033-40)
Given: Diversion distance: 650 NM Diversion pressure altitude: 16.000 ft Mass at point of diversion: 57.000 kg Head wind component: 20 kts Temperature: ISA + 15 °C The diversion fuel required and time are approximately: A) 4.400 kg; 1 hrs 35 min. B) 3.900 kg; 1 hrs 45 min. C) 6.200 kg; 2 hrs 10 min. #D) 4.800 kg; 2 hrs 03 min. 2277. (AIR: atpl) (Refer to figure 033-20) In order to find alternate fuel and time to alternate, the aeroplane operating manual shall be entered with: #A) distance in nautical miles (NM), wind component, landing mass at alternate. B) distance in nautical air miles (NAM), wind component, landing mass at alternate. C) distance in nautical miles (NM), wind component, zero fuel mass. D) distance in nautical miles (NM), wind component, dry operating mass plus holding fuel. 2280. (AIR: atpl) (Refer to figures 033-25 nad 033-36) Given: Distance C-D: 540 NM Cruise: 300 KIAS at FL210 Temperature: ISA +2 °C Headwind component: 50 kts Gross mass at C: 60.000 kg The fuel required from C to D is: #A) 4.200 kg B) 4.620 kg C) 3.680 kg D) 3.350 kg 2285. (AIR: atpl) The purpose of the decision point procedure is? A) To increase the safety of the flight. B) To reduce the landing weight and thus reduce the structural stress on the aircraft. #C) To reduce the minimum required fuel and therefore be able to increase the traffic load. D) To increase the amount of extra fuel. 2287. (AIR: atpl) When using decision point procedure, you reduce the: A) holding fuel by 30%. B) contingency fuel by adding contingency only from the burn off between the decision airport and destination. C) reserve fuel from 10% down to 5%. #D) contingency fuel by adding contingency only from the burn off between decision point and destination. 2294. (AIR: atpl) Planning a flight from Paris (Charles de Gaulle) to London (Heathrow) for a twin - jet aeroplane. Preplanning: Maximum Takeoff Mass: 62.800 kg Maximum Zero Fuel Mass: 51.250 kg Maximum Landing Mass: 54.900 kg Maximum Taxi Mass: 63.050 kg Assume the following preplanning results:
Trip fuel: 1.800 kg Alternate fuel: 1.400 kg Holding fuel (final reserve): 1.225 kg Dry Operating Mass: 34.000 kg Traffic Load: 13.000 kg Catering: 750 kg Baggage: 3.500 kg Find the Takeoff Mass (TOM): A) 55.765 kg #B) 51.515 kg C) 51.425 kg D) 52.265 kg 2295. (AIR: atpl) (Refer to figure 033-12) Given: Cruise mass: 54.000 kg Long Range Cruise or Mach 0,74 Find the optimum altitude for the twin-jet aeroplane. A) 35.300 ft. #B) 34.500 ft. C) maximum operating altitude. D) 33.800 ft. 2299. (AIR: atpl) (Refer to figure 033-21) Given: Dry operating mass: 35.500 kg Estimated load: 12.000 kg Contingency approach and landing fuel: 2.500 kg Elevation at departure aerodrome: 500 ft Elevation at alternate aerodrome: 30 ft Find the final reserve fuel for a jet aeroplane (holding) and give the elevation which is relevant. A) 2.360 kg; destination elevation. B) 2.360 kg; alternate elevation. C) 1.180 kg; destination elevation. #D) 1.180 kg; alternate elevation. 033-05 JET AEROPLANES FLIGHT PLANNING 55 © 2008 AVIATIONEXAM.com 2301 (C) 2304 (B) 2305 (A) 2307 (D) 2312 (A) 2314 (B) 2315 (B) 2316 (D) 2301. (AIR: atpl) (Refer to figure 033-13) Given: Brake release mass: 45.000 kg Temperature: ISA + 20 °C Trip distance: 50 Nautical Air Miles (NAM) Find the short distance cruise altitude for the twin-jet aeroplane. A) 11.000 ft B) 12.500 ft #C) 10.000 ft D) 7.500 ft 2304. (AIR: atpl) (Refer to figure 033-40) Given: Diversion distance: 720 NM Tail wind component: 25 kts Mass at point of diversion: 55.000 kg Temperature: ISA
Diversion fuel available: 4.250 kg What is the minimum pressure altitude at which the above conditions may be met? A) 26.000 ft #B) 20.000 ft C) 16.000 ft D) 14.500 ft 2305. (AIR: atpl) (Refer to figures 033-25 and 033-33) For a flight from B to C: FL310 M 0,74 ISA - 12 °C 957 MGN 40 kts tailwind Weight 50.100 kg How much fuel is required to fly to C? #A) 4.600 kg B) 4.500 kg C) 5.000 kg D) 4.100 kg 2307. (AIR: atpl) (Refer to figure 033-33) Find the FUEL FLOW for the twin jet aeroplane with regard to the following data. Given: Mach 0,74 cruise Flight level 310 Gross mass 50.000 kg ISA conditions A) 1.497 kg/hrs B) 1.150 kg/hrs C) 2.994 kg/hrs #D) 2.300 kg/hrs 2312. (AIR: atpl) The following fuel consumption figures are given for a jet aeroplane: Standard taxi fuel: 600 kg Average cruise consumption: 10.000 kg/hrs Holding fuel consumption at 1.500 ft above alternate airfield elevation: 8.000 kg/hrs Flight time from departure to destination: 6 hours Fuel for diversion to alternate: 10.200 kg Forecast visibility at destination: 2.000 m The minimum ramp fuel load is: #A) 77.800 kg B) 74.800 kg C) 79.800 kg D) 77.200 kg 2314. (AIR: atpl) (Refer to figure 033-20) Given: Estimated dry operation mass: 35.500 kg Estimated load: 14.500 kg Final reserve fuel: 1.200 kg Distance to alternate: 95 NM Average true track: 219° Head wind component: 10 kts Find fuel and time to alternate. A) 1.100 kg; 44 min. #B) 1.100 kg; 25 min.
C) 800 kg; 24 min. D) 800 kg; 40 min. 2315. (AIR: atpl) (Refer to figure 033-17) Given: Cruise M 0,78 FL280 50.000 kg 200 NM Headwind component 30 kts Find the fuel required. A) 1.470 kg #B) 1.740 kg C) 1.620 kg D) 1.970 kg 2316. (AIR: atpl) (Refer to figures 033-23) Given: Brake release mass: 58.000 kg Temperature: ISA + 15 °C The fuel required to climb from an airfield at elevation 4.000 ft to FL300 is: A) 1.350 kg B) 1.400 kg C) 1.450 kg #D) 1.250 kg 033-05 JET AEROPLANES FLIGHT PLANNING 56 © 2008 AVIATIONEXAM.com 2318 (C) 2320 (A) 2321 (B) 2322 (D) 2323 (A) 2324 (A) 2331 (C) 2332 (C) 2334 (D) 2336 (A) 2318. (AIR: atpl) The final reserve fuel for aeroplanes with turbine engines is: A) fuel to fly for 45 minutes at holding speed at 1.000 ft (300 m) above aerodrome elevation in standard conditions. B) fuel to fly for 45 minutes at holding speed at 1.500 ft (450 m) above aerodrome elevation in standard conditions. #C) fuel to fly for 30 minutes at holding speed at 1.500 ft (450 m) above aerodrome elevation in standard conditions. D) fuel to fly for 60 minutes at holding speed at 1.500 ft (450 m) above aerodrome elevation in standard conditions. 2320. (AIR: atpl) Which of the following statements is relevant for forming route portions in integrated range flight planning? #A) The distance from takeoff up to the top of climb has to be known. B) No segment shall be more than 30 minutes of flight time. C) Each reporting point requires a new segment. D) A small change of temperature (2 °C) can divide a segment. 2321. (AIR: atpl) A jet aeroplane is to fly from A to B. The minimum final reserve fuel must allow for: A) 20 minutes hold over alternate airfield. #B) 30 minutes hold at 1.500 ft above destination aerodrome elevation, when no alternate is required. C) 30 minutes hold at 1.500 ft above mean sea level. D) 15 minutes hold at 1.500 ft above destination aerodrome
elevation. 2322. (AIR: atpl) (Refer to figure 033-19) Given: Headwind: 50 kts Temperature: ISA +1 °C Brake release mass: 65.000 kg Trip fuel: 18.000 kg What is the maximum possible trip distance? A) 3.480 NGM B) 2.540 NGM C) 3.100 NGM #D) 2.740 NGM 2323. (AIR: atpl) (Refer to figure 033-21) The final reserve fuel taken from the holding planning table for the twin-jet aeroplane is based on the following parameters: #A) pressure altitude, aeroplane mass and flaps up with minimum drag airspeed. B) pressure altitude, aeroplane mass and flaps down with maximum range speed. C) pressure altitude, aeroplane mass and flaps up with maximum range speed. D) pressure altitude, aeroplane mass and flaps down with minimum drag airspeed. 2324. (AIR: atpl) (Refer to figure 033-15) Within the limits of the data given, a mean temperature increase of 30 °C will affect the trip time by approximately: #A) -5% B) +5% C) +8% D) -7% 2331. (AIR: atpl) (Refer to figure 033-37) A descent is planned at 0,74M/250 KIAS from 35.000 ft to 5.000 ft. How much fuel will be consumed during this descent? A) 278 kg B) 290 kg #C) 150 kg D) 140 kg 2332. (AIR: atpl) An operator (turbojet engine) shall ensure that calculation of usable fuel for a flight for which no destination alternate is required includes, taxi fuel, trip fuel, contingency fuel and fuel to fly for: A) 45 minutes plus 15% of the flight time planned to be spent at cruising level or two hours whichever is less. B) 2 hours at normal cruise consumption. #C) 30 minutes at holding speed at 450 m above aerodrome elevation in standard conditions. D) 30 minutes at holding speed at 450 m above MSL in standard conditions. 2334. (AIR: atpl) (Refer to figure 033-22) Given: Track 340° (T) W/V 280/40 kts Aerodrome elevation: 387 ft
ISA -10 °C Brake release mass: 52.000 kg Cruise at FL280 What are the climb fuel and time? A) 15 min, 1.100 kg. B) 12 min, 1.100 kg. C) 10 min, 1.000 kg. #D) 11 min, 1.000 kg. 2336. (AIR: atpl) (Refer to figure 033-13, 033-30, 033-31 and 033-34) Given: Estimated takeoff mass: 57.000 kg Ground distance: 150 NM Temperature: ISA -10 °C Cruise at Mach 0,74 Find cruise altitude and expected true air speed #A) 25.000 ft, 435 kts. B) 24.000 ft, 445 kts. C) 33.500 ft, 430 kts. D) 33.900 ft, 420 kts. 033-05 JET AEROPLANES FLIGHT PLANNING 57 © 2008 AVIATIONEXAM.com 2891 (C) 2894 (B) 4283 (C) 4284 (A) 4285 (C) 4286 (A) 4287 (A) 4288 (A) 2891. (AIR: atpl) (Refer to figures 033-74) The planned flight is over a distance of 440 NM. Based on the wind charts at altitude the following components are found: FL50: -30 kts FL100: -50 kts FL180: -70 kts The Operations Manual in appendix details the aircraft performances. Which of the following flight levels (FL) gives the best range performance? A) FL050 B) Either FL050 or FL100 #C) FL180 D) FL100 2894. (AIR: atpl) (Refer to figure 033-15) For a flight of 2.000 ground nautical miles, cruising at 30.000 ft, within the limits of the data given, a headwind component of 25 kts will affect the trip time by approximately: A) +5,3% #B) +7,6% C) -3,6% D) +2,3% 4283. (AIR: atpl) (Refer to figure 033-18) Given: Ground distance to destination aerodrome: 1.600 NM Headwind component: 50 kts FL330 Cruise Mach 0,78 ISA +20 °C Estimated landing weight: 55.000 kg Find simplified flight planning to determine estimated trip
fuel and trip time. A) 12.400 kg, 04 hrs 12 min. B) 11.400 kg, 04 hrs 12 min. #C) 12.400 kg, 03 hrs 55 min. D) 11.400 kg, 03 hrs 55 min. 4284. (AIR: atpl) (Refer to figure 033-29) Long Range Cruise at FL350 OAT: -45 °C Gross mass at the beginning of the leg: 40.000 kg Gross mass at the end of the leg: 39.000 kg Find: True airspeed (TAS) and cruise distance (NAM) for a twin jet aeroplane. #A) TAS 433 kts, 227 NAM. B) TAS 423 kts, 227 NAM. C) TAS 431 kts, 1.163 NAM. D) TAS 423 kts, 936 NAM. 4285. (AIR: atpl) (Refer to figure 033-21) Given: Mean gross mass: 47.000 kg The fuel required for 45 minutes holding in a racetrack pattern at 5.000 ft is: A) 1.690 kg B) 1.090 kg #C) 1.635 kg D) 1.125 kg 4286. (AIR: atpl) (Refer to figure 033-15) For a flight of 1.900 ground nautical miles the following conditions apply: Head wind component: 10 kts Temperature: ISA -5 °C Trip fuel available: 15.000 kg Landing mass: 50.000 kg What is the minimum cruise level (pressure altitude) which may be planned? #A) 17.000 ft B) 10.000 ft C) 14.000 ft D) 22.000 ft 4287. (AIR: atpl) (Refer to figure 033-18) Using the following information, find fuel required and trip time with simplified flight planning for twin-jet aeroplane: Ground distance to destination: 1.600 NM Headwind component: 50 kts FL330 Cruise Mach 0,78 ISA Deviation +2 °C Landing mass: 55.000 kg #A) 12.250 kg, 04 hrs 00 min. B) 11.400 kg, 04 hrs 12 min. C) 11.600 kg, 04 hrs 15 min. D) 12.000 kg, 03 hrs 51 min. 4288. (AIR: atpl) (Refer to figure 033-14) Given: Estimated zero fuel mass: 50.000 kg Estimated landing mass at alternate: 52.000 kg
Final reserve fuel: 2.000 kg Alternate fuel: 1.000 kg Flight to destination, distance 720 NM: TC 030°, W/V 340/30 Cruise: long range FL330, OAT -30 °C Find: estimated trip fuel and time. #A) 4.800 kg; 01:45. B) 4.400 kg; 02:05. C) 4.750 kg; 02:00. D) 4.600 kg; 02:05. 033-05 JET AEROPLANES FLIGHT PLANNING 58 © 2008 AVIATIONEXAM.com 4289 (A) 4290 (B) 4294 (B) 4296 (B) 4298 (D) 4299 (B) 4301 (C) 4303 (D) 4289. (AIR: atpl) (Refer to figure 033-40) Given: Distance to alternate: 950 NM Head wind component: 20 kts Mass at point of diversion: 50.000 kg Diversion fuel available: 5.800 kg The minimum pressure altitude at which the above conditions may be met is: #A) 22.000 ft B) 20.000 ft C) 26.000 ft D) 18.000 ft 4290. (AIR: atpl) (Refer to figure 033-16) Planning a flight from Paris (CDG) to London (Heathrow) for a twin-jet aeroplane. Power setting: M 0,74 FL280 Landing Mass: 50.000 kg Distance to use: 200 NM W/V from Paris to London: 280/40 Mean track: 340° (T) Find the estimated trip fuel. A) 1.550 kg #B) 1.740 kg C) 1.900 kg D) 1.450 kg 4294. (AIR: atpl) A jet aeroplane has a cruising fuel consumption of 4.060 kg/hrs, and 3.690 kg/hrs during holding. If the destination is an isolated airfield, the aeroplane must carry, in addition to contingency reserves, additional fuel of: A) 7.380 kg #B) 8.120 kg C) 1.845 kg D) 3.500 kg 4296. (AIR: atpl) Which of the following is correct? Given: DOM: 33.510 kg Traffic load: 7.600 kg Trip fuel: 2.040 kg Final reserve: 983 kg
Alternative fuel: 1.100 kg Contingency: 5% of trip fuel A) Est landing mass at destination is 43.193 kg. #B) Est landing mass at destination is 43.295 kg. C) Est takeoff mass is 43.295 kg. D) Est takeoff mass is 45.233 kg. 4298. (AIR: atpl) (Refer to figure 033-33) Find the specific range for the twin jet aeroplane flying below the optimum altitude (range loss = 6%) and using the following data: Mach 0,74 cruise Flight level 310 Gross mass: 50.000 kg ISA conditions A) 2.807 NAM / 1.000 kg. B) 187 NAM / 1.000 kg. C) 2.994 NAM / 1.000 kg. #D) 176 NAM / 1.000 kg. 4299. (AIR: atpl) (Refer to figure 033-12 and 033-65) Given: Cruise weight: 56.000 kg Cruise at Mach 0,78 Cruise at FL310 What is the fuel penalty? A) 0% #B) 1% C) 4% D) 10% 4301. (AIR: atpl) (Refer to figure 033-22) Planning an IFR-flight from Paris (Charles de Gaulle) to London (Heathrow) for the twin jet aeroplane. Given: Estimated Takeoff Mass (TOM): 52.000 kg Airport elevation: 387 ft FL280 W/V 280°/40 kts ISA Deviation: -10 °C Average True Course: 340° Find time to the top of climb (TOC). A) 12 min B) 3 min #C) 11 min D) 15 min 4303. (AIR: atpl) (Refer to figure 033-20) Given for the twin jet aeroplane: Dry operating mass: 35.500 kg Traffic load: 14.500 kg Final reserve fuel: 1.200 kg Distance to alternate: 95 NM Tailwind component: 10 kts Find fuel required and trip time to alternate with simplified flight planning (alternate planning): A) 800 kg, 0,4 hrs. B) 1.000 kg, 40 min. C) 800 kg, 24 min. #D) 1.000 kg, 24 min.
033-05 JET AEROPLANES FLIGHT PLANNING 59 © 2008 AVIATIONEXAM.com 4305 (D) 4308 (D) 4309 (C) 4310 (A) 4311 (B) 4312 (A) 4321 (D) 4322 (D) 4305. (AIR: atpl) (Refer to figures 033-23) Find time, fuel, still air distance and TAS for an enroute climb 280/0,74 to FL350, given: Brake release mass: 64.000 kg ISA +10 °C Airport elevation 3.000 ft A) 25 min, 1.875 kg, 148 Nautical Air Miles (NAM), 391 kts. B) 26 min, 2.050 kg, 157 Nautical Air Miles (NAM), 399 kts. C) 20 min, 1.750 kg, 117 Nautical Air Miles (NAM), 288 kts. #D) 26 min, 1.975 kg, 157 Nautical Air Miles (NAM), 399 kts. 4308. (AIR: atpl) When calculating the fuel required to carry out a given flight, one must take into account: 1) the wind 2) foreseeable airborne delays 3) other weather forecasts 4) any foreseeable conditions which may delay landing The combination which provides the correct statement is: A) 1, 2, 3 B) 1, 3 C) 2, 4 #D) 1, 2, 3, 4 4309. (AIR: atpl) (Refer to figure 033-22 and 033-64) Planning an IFR-flight from Paris to London for a twin jet aeroplane. Given: Estimated Takeoff Mass (TOM): 52.000 kg Airport elevation: 387 ft FL280 W/V 280°/40 kts ISA Deviation: -10 °C Average True Course: 340° Find ground distance to the top of climb (TOC). A) 53 NM B) 56 NM #C) 50 NM D) 47 NM 4310. (AIR: atpl) Given: Dry operating mass (DOM): 33.500 kg Load: 7.600 kg Maximum allowable takeoff mass: 66.200 kg Standard taxi fuel: 200 kg Tank capacity: 16.100 kg The maximum possible takeoff fuel is: #A) 15.900 kg B) 17.100 kg C) 16.300 kg D) 17.300 kg 4311. (AIR: atpl) (Refer to figure 033-18) Given for the twin jet aeroplane: Ground distance to destination aerodrome: 1.600 NM
Headwind component: 50 kts FL330 Cruise 0,78 Mach ISA Deviation: +20 °C Landing mass: 55.000 kg Find fuel required and trip time with simplified flight planning. A) 11.400 kg, 04 hrs 12 min. #B) 12.400 kg, 04 hrs 00 min. C) 11.600 kg, 04 hrs 15 min. D) 12.000 kg, 03 hrs 51 min. 4312. (AIR: atpl) (Refer to figure 033-26) Given: Flight time from top of climb to the enroute point in FL280: 48 min Cruise procedure is long range cruise (LRC) Temp: ISA -5 °C Takeoff mass: 56.000 kg Climb fuel: 1.100 kg Find: distance in nautical air miles (NAM) for this leg and fuel consumption: #A) 345 NAM; 2.000 kg. B) 350 NAM; 2.000 kg. C) 345 NAM; 2.100 kg. D) 437 NAM; 2.100 kg. 4321. (AIR: atpl) (Refer to figure 033-32) Planning an IFR-flight from Paris to London for the twin jet aeroplane. Given: Gross mass: 50.000 kg FL280 ISA Deviation: -10 °C Cruise procedure: Mach 0,74 Determine the TAS: A) 417 kts B) 440 kts C) 427 kts #D) 430 kts 4322. (AIR: atpl) (Refer to figure 033-21) Planning a flight from Paris Charles de Gaulle to London Heathrow for a twin-jet aeroplane. Preplanning: Dry Operating Mass (DOM): 34.000 kg Traffic Load: 13.000 kg The holding is planned at 1.500 ft above alternate elevation (256 ft) The holding is planned for 30 minutes with no reductions Determine the estimated landing mass at alternate Manchester: A) 48.675 kg B) 49.250 kg C) 2.250 kg #D) 48.125 kg 033-05 JET AEROPLANES FLIGHT PLANNING 60 © 2008 AVIATIONEXAM.com 4323 (D) 4324 (B) 4329 (A) 4333 (C) 4334 (C) 4338 (D) 4341 (A) 4342 (C) 4323. (AIR: atpl) (Refer to Route Manual chart E(HI)4 or figure HI-12 and figure
033-20) Planning a flight from Paris Charles-de-Gaulle (49°00,9 N 002°36,9 W) to London Heathrow (51°29,2 N 000°27,9 W) for a twin-jet aeroplane. The alternate airport is Manchester (53°21,4 N 002°15,7 W). Preplanning: The wind from London to Manchester: 250°/30 kts The distance from London to Manchester: 160 NM Assume the estimated landing mass at alternate is 50.000 kg Find the alternate fuel and time: A) 1.200 kg and 26 minutes. B) 1.300 kg and 28 minutes. C) 1.600 kg and 36 minutes. #D) 1.450 kg and 32 minutes. 4324. (AIR: atpl) (Refer to figure 033-22) Given: Brake release mass: 57.500 kg Temperature: ISA -10 °C Head wind component: 16 kts Initial FL280 Find still air distance (NAM) and ground distance (NM) for the climb. A) 59 NAM; 62 NM. #B) 62 NAM; 59 NM. C) 67 NAM; 71 NM. D) 71 NAM; 67 NM. 4329. (AIR: atpl) (Refer to figure 033-13) Find the short distance cruise altitude for the twin jet aeroplane. Given: Brake release mass: 40.000 kg Temperature: ISA +20 °C Trip distance: 150 Nautical Air Miles (NAM) #A) 30.000 ft B) 25.000 ft C) 21.000 ft D) 27.500 ft 4333. (AIR: atpl) (Refer to figure 033-14 and 033-27) Given for the twin jet aeroplane: Zero fuel mass: 50.000 kg Landing mass at alternate: 52.000 kg Final reserve fuel: 2.000 kg Alternate fuel: 1.000 kg Flight to destination: Distance 720 NM, TC 030°, W/V 340°/30 kts Cruise: LRC, FL330, OAT -30 °C Find: Estimated trip fuel and time with simplified flight planning. A) 4.750 kg, 02:00. B) 4.400 kg, 02:05. #C) 4.800 kg, 01:51. D) 4.600 kg, 02:05. 4334. (AIR: atpl) (Refer to figure 033-21) Given for the twin jet aeroplane: Estimated mass on arrival at the alternate: 50.000 kg Estimated mass on arrival at the destination: 52.525 kg Alternate elevation: MSL
Destination elevation: 1.500 ft Find final reserve fuel and corresponding time. A) 2.360 kg, 01 hrs 00 min. B) 2.360 kg, 30 min. ##C) 1.180 kg, 30 min. D) 1.180 kg, 45 min. 4338. (AIR: atpl) (Refer to figure 033-20) In order to get alternate fuel and time, the twin-jet aeroplane operations manual graph shall be entered with: A) distance (NM), wind component, zero fuel mass. B) still air distance, wind component, zero fuel mass. C) flight time, wind component, landing mass at alternate. #D) distance (NM), wind component, landing mass at alternate. 4341. (AIR: atpl) (Refer to figure 033-22) Given: Mass at brake release: 57.500 kg Temperature: ISA -10 °C Average head wind component: 16 kts Initial cruise: FL280 Find the climb fuel. #A) 1.138 kg B) 1.238 kg C) 1.387 kg D) 1.040 kg 4342. (AIR: atpl) (Refer to figure 033-22) Given: Estimated takeoff mass: 57.500 kg Initial cruise: FL280 Average temperature during climb: ISA -10 °C Average head wind component: 18 kts Find the climb time for enroute climb 280/0,74 A) 15 min B) 11 min #C) 13 min D) 14 min 033-05 JET AEROPLANES FLIGHT PLANNING 61 © 2008 AVIATIONEXAM.com 4344 (C) 4347 (B) 4352 (A) 4354 (D) 4357 (C) 4358 (C) 12247 (D) 12249 (C) 4344. (AIR: atpl) (Refer to figure 033-22) Planning an IFR flight from Paris to London for the twin jet aeroplane. Given: Estimated Takeoff Mass (TOM): 52.000 kg Airport elevation: 387 ft FL280 W/V 280°/40 kts ISA Deviation: -10 °C Average True Course: 340° Find fuel to the top of climb (TOC). A) 1.100 kg B) 1.000 lbs #C) 1.000 kg D) 1.500 lbs 4347. (AIR: atpl)
For flight planning purposes the landing mass at alternate is taken as: A) Landing Mass at destination plus Alternate Fuel. #B) Zero Fuel Mass plus Final Reserve Fuel. C) Zero Fuel Mass plus Final Reserve Fuel and Alternate Fuel. D) Zero Fuel Mass plus Final Reserve Fuel and Contingency Fuel. 4352. (AIR: atpl) (Refer to figure 033-27) Given: FL330 Long range cruise OAT: -63 °C Gross mass: 50.500 kg Find true airspeed (TAS). #A) 420 kts B) 433 kts C) 431 kts D) 418 kts 4354. (AIR: atpl) (Refer to Route Manual chart E(HI)4 or figure HI-11 and figure 033-16) Planning a flight from Paris Charles de Gaulle (49°00,9 N 002°36,9 E) to London Heathrow (51°29,2 N 000°27,9 W) for a twin-jet aeroplane. Preplanning: Powersetting: Mach 0,74 Planned flight level: FL280 Landing Mass in the fuel graph: 50.000 kg Trip distance used for calculation: 200 NM Wind from Paris to London: 280°/40 kts Find the estimated trip fuel. A) 1.450 kg B) 1.550 kg C) 1.900 kg #D) 1.740 kg 4357. (AIR: atpl) (Refer to figure 033-21) Given for the twin jet aeroplane: Estimated mass on arrival at the alternate: 50.000 kg Elevation at destination aerodrome: 3.500 ft Elevation at alternate aerodrome: 30 ft Find final reserve fuel. A) 1.150 kg B) 2.360 kg #C) 1.180 kg D) 2.300 kg 4358. (AIR: atpl) (Refer to figure 033-29) The aeroplane gross mass at top of climb: 61.500 kg The distance to be flown: 385 NM at FL350 OAT: -54 °C Wind component: 40 kts tailwind Using long range cruise procedure what fuel is required? A) 2.350 kg B) 2.250 kg #C) 2.150 kg D) 2.050 kg 12247. (AIR: atpl) (Refer to figure 033-37)
Planning an IFR flight from Paris to London for the twin jet aeroplane. Given: Estimated Landing Mass: 49.700 kg FL280 W/V 280°/40 kts Average True Course: 320° Procedure for descent: M0,74/250 KIAS Determine the distance from the top of descent to London (elevation 80 ft). A) 87 NM B) 97 NM C) 65 NM #D) 76 NM 12249. (AIR: atpl) (Refer to figure 033-37) Planning an IFR flight from Paris to London for the twin jet aeroplane. Given: Estimated Landing Mass: 49.700 kg FL280 W/V 280°/40 kts Average True Course: 320° Procedure for descent: M0,74/250 KIAS Determine the fuel consumption from the top of descent to London (elevation 80 ft). A) 210 kg B) 320 kg #C) 273 kg D) 263 kg 033-05 JET AEROPLANES FLIGHT PLANNING 62 © 2008 AVIATIONEXAM.com 12553 (B) 12554 (C) 12555 (C) 12559 (C) 12560 (B) 12561 (A) 12562 (A) 14551 (A) 14553 (B) 12553. (AIR: atpl) (Refer to figure 033-19) Given a trip time of about 9 hours, within the limits of the data given, a temperature decrease of 30 °C will affect the trip time by approximately: A) -10% #B) +7% C) +3% D) -4% 12554. (AIR: atpl) (Refer to figure 033-19) For a flight of 3.500 ground nautical miles, the following apply: Tail wind component: 50 kts Temperature: ISA +10 °C Brake release mass: 65.000 kg The trip fuel and trip time respectively are: A) 21.800 kg, 9 hrs 25 min. B) 19.000 kg, 7 hrs 45 min. #C) 18.100 kg, 7 hrs 20 min. D) 15.800 kg, 6 hrs 00 min. 12555. (AIR: atpl) (Refer to figure 033-19) For a flight of 2.400 ground nautical miles, the following apply:
Tail wind: 25 kts Temperature: ISA -10 °C Brake release mass: 66.000 kg The trip fuel and trip time respectively are: A) 14.600 kg, 5 hrs 45 min. B) 15.000 kg, 6 hrs 00 min. #C) 14.000 kg, 5 hrs 35 min. D) 15.800 kg, 6 hrs 20 min. 12559. (AIR: atpl) (Refer to figure 033-40) Given: Diversion fuel available: 8.500 kg Diversion cruise altitude: 10.000 ft Mass at point of diversion: 62.500 kg Head wind component: 50 kts Temperature: ISA -5 °C The maximum diversion distance, and elapsed time alternate, are approximately: A) 760 NM, 4 hrs 30 min. B) 1.130 NM, 3 hrs 30 min. #C) 860 NM, 3 hrs 20 min. D) 1.000 NM, 3 hrs 40 min. 12560. (AIR: atpl) (Refer to figure 033-39) For the purpose of planning an extended range flight it is required that with a start of diversion mass of 55.000 kg a diversion of 600 nautical miles should be achieved in 90 minutes. Using the above table, the only listed cruise technique to meet that requirement is: A) LRC #B) M 0,74 / 330 KIAS C) M 0,74 / 290 KIAS D) M 0,70 / 280 KIAS 12561. (AIR: atpl) (Refer to figure 033-39) Using the above table, in ISA conditions and at a speed of M 0,70/280 KIAS, in an elapsed time of 90 minutes an aircraft with mass at point of diversion 48.000 kg could divert a distance of: #A) 584 NM B) 563 NM C) 603 NM D) 608 NM 12562. (AIR: atpl) (Refer to figure 033-39) An aircraft on an extended range operation is required never to be more than 120 minutes from an alternate, based on 1 engine inoperative LRC conditions in ISA. Using the above table and a given mass of 40.000 kg at the most critical point, the maximum air distance to the relevant alternate is: #A) 735 NM B) 794 NM C) 810 NM D) 875 NM 14551. (AIR: atpl) (Refer to figure 033-41 and 033-42) An aircraft is planned to fly a LRC at FL350, ISA -10 °C, at an average gross cruise weight of 55.000 kg and a Landing Weight (Without Tankered Fuel) of 47.500 kg; the wind component
is -30 kts and the trip distance 1.600 NGM. Calculate the Break Even Fuel Price Destination Airport if the Fuel Price at Departure Airport is 75 cents/US Gallon. #A) 90 cents B) 80 cents C) 95 cents D) 85 cents 14553. (AIR: atpl) (Refer to figure 033-41 and 033-42) An aircraft is tasked to fly a 0,74 Mach cruise at FL310, ISA +15 °C with a Landing Weight(Without Tankered Fuel) of 40.000 kg. The sector distance is 1.050 NGM, wind component +35 kts. Calculate the Break Even Fuel Price at Destination if the Fuel price at Departure is 85 cents/US Gallon. A) 85 cents #B) 92 cents C) 98 cents D) 80 cents 033-05 JET AEROPLANES FLIGHT PLANNING 63 © 2008 AVIATIONEXAM.com 17198 (B) 17199 (B) 17200 (A) 22884 (A) 22885 (A) 22886 (D) 22887 (A) 17198. (AIR: atpl) (Refer to figures 033-48, 033-60, 033-62) The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg ground distance: 4.000 NM Flight Level 370 Long range flight regime Effective wind at this level: 50 kts head Temperature: ISA Centre of Gravity (CG): 37% Pack Flow: LOW (LO) Anti Ice: OFF Reference Landing mass: 140.000 kg Taxi Fuel: 500 kg Final Reserve Fuel: 2.400 kg The fuel quantity which must be loaded on board the aircraft is: A) 41.590 kg #B) 51.860 kg C) 52.060 kg D) 46.340 kg 17199. (AIR: atpl) (Refer to figure 033-43 and 033-63) A turbojet aeroplane is prepared for a 1.300 NM flight at FL350, with a true airspeed of 460 kts and a headwind of 160 kts. The takeoff runway limitation is 174.000 kg, the planned departure mass is 160.000 kg. The departure fuel price is equal to 0,92 times the arrival fuel price (fuel price ratio = 0,92). In order for the airline to optimize its savings, the additional fuel quantity that must be loaded onboard is: A) 0 kg #B) 14.000 kg C) 30.000 kg D) 12.000 kg
17200. (AIR: atpl) (Refer to figure 033-43 and 033-63) Assuming a departure/destination fuel price ratio of 0,91, the commander decides to optimize fuel tankering by using the following data: Cruise flight level: FL350 Air distance to be covered: 2.500 NM Planned takeoff mass: 200.000 kg (with the minimum prescribed fuel quantity of 38.000 kg that includes a trip fuel of 29.000 kg) Maximum landing mass: 180.000 kg Maximum takeoff mass: 205.000 kg Maximum tank capacity: 40.000 kg The additional fuel quantity will be: #A) 0 kg B) 3.000 kg C) 2.000 kg D) 5.000 kg 22884. (AIR: atpl) (Refer to figures 033-45 and 033-46) In standard atmosphere, assuming a mass of 197.000 kg, in order to fly at FL370 and to be at the optimum altitude, your Mach number should be: #A) 0,82. B) 0,84. C) 0,80. D) the same as for LRC (Long Range Cruise). 22885. (AIR: atpl) (Refer to figures 033-47, 033-50 and 033-62) Given: Mass at brake release: 210.000 kg Selected cruise speed: Mach 0,82 Flight leg distance: 3.000 NM Cruise level: optimum Air conditioning: standard Anti-icing: OFF Temperature: ISA CG: 37 Assuming zero wind, the planned landing mass at destination will be: #A) 172.300 kg B) 170.400 kg C) 171.300 kg D) 176.100 kg 22886. (AIR: atpl) (Refer to figures 033-47, 033-49 and 033-62) Given: Mass at brake release: 190.000 kg Selected cruise speed: Mach 0,82 Flight leg distance: 1.500 NM Cruise level: optimum Air conditioning: standard Anti-icing: OFF Temperature: ISA CG: 37% Assuming zero wind, the planned landing mass at destination will be: #A) 169.200 kg B) 170.200 kg C) 174.800 kg
#D) 171.200 kg 22887. (AIR: atpl) (Refer to figures 033-47, 033-49 and 033-62) Given: Mass at brake release: 190.000 kg Selected cruise speed: Mach 0,82 Flight leg distance: 1.500 NM Cruise level: optimum Air conditioning: standard Anti-icing: OFF Temperature: ISA CG: 37% Assuming zero wind, the planned flight time from takeoff to landing needed to complete this flight will be: #A) 209 minutes B) 191 minutes C) 198 minutes D) 203 minutes 033-05 JET AEROPLANES FLIGHT PLANNING 64 © 2008 AVIATIONEXAM.com 22888 (C) 22889 (C) 22890 (A) 22891 (B) 22892 (A) 22893 (C) 22888. (AIR: atpl) (Refer to figures 033-47, 033-50 and 033-62) Given: Mass at brake release: 210.000 kg Selected cruise speed: Mach 0,82 Air distance: 3.000 NM Cruise level: optimum Air conditioning: standard Anti-icing: OFF Temperature: ISA CG: 37% Assuming zero wind, the planned flight time from takeoff to landing needed to complete this flight will be: A) 394 minutes B) 389 minutes #C) 400 minutes D) 381 minutes 22889. (AIR: atpl) (Refer to figures 033-48) For a long distance flight at FL370, Long Range regime, divided into four flight legs with the following specifications: Leg 1 - Ground distance: 2.000 NM, headwind component: 50 kts Leg 2 - Ground distance: 1.000 NM, headwind component: 30 kts Leg 3 - Ground distance: 500 NM, tailwind component: 70 kts Leg 4 - Ground distance: 1.000 NM, headwind component: 20 kts The total air distance is approximately: A) 4.580 NM B) 4.820 NM #C) 4.800 NM D) 4.940 NM 22890. (AIR: atpl) (Refer to figures 033-45)
For a turbojet aeroplane flying with a mass of 190.000 kg, at Mach 0,82, and knowing that the temperature at flight level FL370 is - 35 °C, the optimum flight altitude calculated using the annex is: #A) 37.400 ft B) 37.800 ft C) 34.800 ft D) 38.600 ft 22891. (AIR: atpl) (Refer to figure 033-55) The flight crew of a turbojet aeroplane prepares a flight using the following data: Takeoff mass: 168.500 kg Flight leg ground distance: 2.000 NM Flight level FL370; Long Range flight regime Tailwind component at this level: 30 kts Total anti-ice set on ON Fixed taxi fuel: 500 kg; final reserve: 2.000 kg Ignore alternate fuel The effects of climb and descent are not corrected for consumption. The prescribed quantity of trip fuel for the flight leg is: A) 23.300 kg #B) 20.500 kg C) 23.000 kg D) 22.500 kg 22892. (AIR: atpl) (Refer to figure 033-57) The flight crew of a turbojet aeroplane prepares a flight using the following data: Takeoff mass: 210.500 kg Flight leg ground distance: 2.500 NM FL330 Long Range flight regime Tailwind component at this level: 70 kts Total anti-ice set on ON Fixed taxi fuel: 500 kg; final reserve: 2.400 kg Ignore alternate fuel. The effects of climb and descent are not corrected for consumption. The quantity of fuel that must be loaded at the parking area is: #A) 31.840 kg B) 31.340 kg C) 30.200 kg D) 39.750 kg 22893. (AIR: atpl) (Refer to figure 033-52) A turbojet aeroplane flies using the following data: Flight level: FL330 Flight regime: Long Range (LR) Mass: 156.500 kg Tailwind component at this level: 40 kts With a remaining flight time of 1 hrs 10 min the ground distance that can be covered by the aeroplane at cruising speed is: A) 471 NM B) 518 NM #C) 539 NM D) 493 NM
033-05 JET AEROPLANES FLIGHT PLANNING 65 © 2008 AVIATIONEXAM.com 22894 (B) 22895 (D) 22896 (B) 22897 (B) 22899 (B) 22900 (A) 22901 (B) 22894. (AIR: atpl) (Refer to figure 033-44 and 033-63) The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg air distance: 2.700 NM Flight level FL310, true airspeed: 470 kts Tailwind component at this level: 35 kts Initially planned takeoff mass (without extrafuel on board): 195.000 kg Fuel price: 0,28 Euro/l at departure; 0,26 Euro/l at destination To maximize savings, the commander chooses to carry extra fuel in addition to that which is necessary. The optimum quantity of fuel which should be carried in addition to the prescribed quantity is: A) 10.000 kg. #B) the fuel transport operation is not recommended in this case. C) 5.000 kg. D) 8.000 kg. 22895. (AIR: atpl) (Refer to figure 033-44 and 033-63) The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg air distance: 2.700 NM FL310 True airspeed: 470 kts Tailwind component at this level: 35 kts Initially planned takeoff mass (without extra fuel on board): 180.000 kg Fuel price: 0,28 Euro/l at departure; 0,26 Euro/l at destination To maximize savings, the commander chooses to carry extra fuel in addition to that which is necessary. The optimum quantity of fuel which should be carried in addition to the prescribed quantity is: A) 4.000 kg. B) 6.000 kg. C) 10.000 kg. #D) the fuel transport operation is not recommended in this case. 22896. (AIR: atpl) (Refer to figure 033-52, 033-58 and 033-59) Given: Takeoff mass: 150.000 kg Planned cruise at FL350 Long range MACH Standard Atmosphere (ISA) CG: 37% You have to cover an air distance of 2.000 NM. Your flight time will be: A) 359 minutes #B) 304 minutes C) 288 minutes D) 298 minutes 22897. (AIR: atpl) (Refer to figures 033-48)
For a long distance flight at FL390, Long Range regime, divided into four flight legs with the following characteristics: Leg 1 - Ground distance: 2.000 NM, head wind component: 50 kts Leg 2 - Ground distance: 1.000 NM, head wind component: 30 kts Leg 3 - Ground distance: 500 NM, tail wind component: 100 kts Leg 4 - Ground distance: 1.000 NM, head wind component: 70 kts The air distance of the entire flight is approximately: A) 5.040 NM #B) 4.900 NM C) 5.120 NM D) 4.630 NM 22899. (AIR: atpl) (Refer to figures 033-47, 033-49, 033-50 and 033-62) Planning a MACH 0,82 cruise at FL390, the estimated landing mass is 160.000 kg. The ground distance is 2.800 NM and the mean wind is equal to zero. ISA conditions. Fuel consumption will be: A) 30.371 kg #B) 32.657 kg C) 30.117 kg D) 27.577 kg 22900. (AIR: atpl) (Refer to figures 033-47, 033-49, 033-50 and 033-62) Planning a Mach 0,82 cruise at FL390, the estimated landing mass is 160.000 kg, the ground distance is 2.800 NM and the mean tailwind is 100 kt, ISA conditions. Fuel consumption will be: #A) 26.950 kg B) 22.860 kg C) 24.900 kg D) 30.117 kg 22901. (AIR: atpl) (Refer to figure 033-54) A turbojet aeroplane, weighing 200.000 kg, initiates its cruise at the optimum level at M 0,84 (ISA, CG=37%, Total Anti Ice ON). A head wind of 30 kts is experienced and, after a distance of 500 NM, severe icing is encountered and this requires an immediate descent. The aeroplane mass at start of descent is: A) 193.800 kg #B) 192.500 kg C) 193.000 kg D) 193.400 kg 033-05 JET AEROPLANES FLIGHT PLANNING 66 © 2008 AVIATIONEXAM.com 22902 (B) 22903 (A) 22904 (D) 22905 (C) 22906 (A) 22907 (A) 23735 (A) 22902. (AIR: atpl) (Refer to figure 033-52, 033-58 and 033-59) Given: Takeoff mass: 150.000 kg Planned cruise at FL350 Long range Mach Standard Atmosphere (ISA)
CG: 37% Covering an air distance of 2.000 NM, your trip fuel from takeoff to landing will be: A) 20.260 kg #B) 22.360 kg C) 19.660 kg D) 21.760 kg 22903. (AIR: atpl) (Refer to figure 033-51) A turbojet aeroplane is flying using the following data: Flight level FL250, Long Range (LR) cruise, mass of 150.000 kg Temperature: ISA Head wind component: 100 kts Remaining flight time: 1 hrs 40 min The ground distance that can be covered during the cruise flight is: #A) 445 NM B) 612 NM C) 841 NM D) 2.031 NM 22904. (AIR: atpl) (Refer to figure 033-53) A turbojet aeroplane is flying using the following data: Optimum flight level, Mach 0,80, mass of 190.000 kg Temperature: ISA Tailwind component: 100 kts The fuel mileage and the fuel consumption per hour are: A) 105 NM / 1.000 kg; 6.515 kg/hrs. B) 86 NM / 1.000 kg; 6.515 kg/hrs. C) 71 NM / 1.000 kg; 5.330 kg/hrs. #D) 105 NM / 1.000 kg; 5.330 kg/hrs. 22905. (AIR: atpl) (Refer to figures 033-49 and 033-62) Assuming the following data: Ground distance to be covered: 2.600 NM Cruise flight level: FL370 Cruising speed: Mach 0,82 (true airspeed: 470 kt) Wind: zero wind during flight Planned destination landing mass: 140.000 kg Temperature: ISA +15 °C CG: 37% Total anti-ice: ON Air conditioning: normal Fuel consumption for such a flight is: A) 29.400 kg B) 27.400 kg #C) 31.500 kg D) 29.100 kg 22906. (AIR: atpl) (Refer to figures 033-49 and 033-62) Assuming the following data: Ground distance to be covered: 2.500 NM Cruise flight level: FL350 Cruising speed: Mach 0,82 (true airspeed: 470 kt) Tailwind component: 40 kts Planned destination landing mass: 150.000 kg Temperature: ISA CG: 37% Total anti-ice: OFF
Air conditioning: normal Fuel consumption for such a flight is: #A) 27.800 kg B) 27.000 kg C) 28.300 kg D) 29.200 kg 22907. (AIR: atpl) (Refer to figures 033-49 and 033-62) Assuming the following data: Ground distance to be covered: 1.500 NM Cruise flight level: FL310 Cruising speed: Mach 0,82 (true airspeed: 470 kts) Head wind component: 40 kts Planned destination landing mass: 140.000 kg Temperature: ISA +15 °C CG: 37% Total anti-ice: ON Pack flow: HI Fuel consumption for such a flight is: #A) 23.500 kg B) 21.500 kg C) 21.700 kg D) 19.900 kg 23735. (AIR: atpl) (Refer to figure 033-43 and 033-63) Assuming a departure/destination fuel price ratio of 0,92, the commander decides to optimize fuel tankering by using the following data: Cruise flight level: FL350 Air distance to be covered: 1.830 NM Planned takeoff mass: 190.000 kg (with a minimum prescribed fuel quantity of 30.000 kg that includes a trip fuel of 22.000 kg) Maximum landing mass: 180.000 kg Maximum takeoff mass: 205.000 kg Maximum tank capacity: 40.000 kg The additional fuel quantity will be: #A) 10.000 kg B) 20.000 kg C) 12.000 kg D) 15.000 kg 033-05 JET AEROPLANES FLIGHT PLANNING 67 © 2008 AVIATIONEXAM.com 23736 (D) 23740 (B) 23741 (D) 23742 (D) 23743 (B) 23744 (B) 23736. (AIR: atpl) (Refer to figures 033-49 and 033-62) Assuming the following data: Ground distance to be covered: 2.000 NM Cruise flight level: FL330 Cruising speed: Mach 0,82 (true airspeed: 470 kts) Head wind component: 30 kts Planned destination landing mass: 160.000 kg Temperature: ISA CG: 37% Total anti-ice: ON Pack flow: HI Time needed to carry out such a flight is:
A) 4 hrs 26 min B) 5 hrs 02 min C) 4 hrs 10 min #D) 4 hrs 43 min 23740. (AIR: atpl) (Refer to figure 033-44 and 033-63) The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg distance: 3.500 NM Flight level FL310, true airspeed: 450 kts Headwind component at this level: 5 kts Initially planned takeoff mass (without extra fuel on board): 180.000 kg Fuel price: 0,35 $/l at departure; 0,315 $/l at destination To maximize savings, the commander chooses to carry extra fuel in addition to that which is necessary. Using the appended annex, the optimum quantity of fuel which should be carried in addition to the prescribed quantity is: A) 8.000 kg. #B) the fuel transport operation is not recommended in this case. C) 22.000 kg. D) 15.000 kg. 23741. (AIR: atpl) (Refer to figure 033-44 and 033-63) The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg distance: 4.000 NM Flight level FL310, true airspeed: 450 kts Headwind component at this level: 50 kts Initially planned takeoff mass (without extra fuel on board): 170.000 kg Fuel price: 0,27 Euro/l at departure; 0,30 Euro/l at destination To maximize savings, the commander chooses to carry extra fuel in addition to that which is necessary. Using the appended annex, the optimum quantity of fuel which should be carried in addition to the prescribed quantity is: A) the fuel transport operation is not recommended in this case. B) 18.000 kg. C) 32.000 kg. #D) 8.000 kg. 23742. (AIR: atpl) (Refer to figure 033-44 and 033-63) The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg distance: 3.500 NM Flight level FL310, true airspeed: 450 kts Headwind component at this level: 55 kts Initially planned takeoff mass (without extra fuel on board): 180.000 kg Fuel price: 0,30 Euro/l at departure; 0,27 Euro/l at destination To maximize savings, the commander decides to carry extra fuel in addition to that which is necessary. Using the appended annex, the optimum quantity of fuel which should be carried in addition to the prescribed quantity is: A) 22.000 kg. B) 15.000 kg. C) 8.000 kg. #D) the fuel transport operation is not recommended in this
case. 23743. (AIR: atpl) (Refer to figure 033-56) The flight crew of a turbojet aeroplane prepares a flight using the following data: FL370 at Long Range (LR) cruise regime Mass at brake release: 212.800 kg Flight leg ground distance: 2.500 NM Temperatures: ISA CG: 37% Headwind component: 30 kts Total anti-ice set on ON for the entire flight No requested climb and descent correction of the fuel consumption The fuel consumption (from takeoff to landing) is: A) 30.440 kg #B) 34.430 kg C) 32.480 kg D) 28.720 kg 23744. (AIR: atpl) (Refer to figure 033-44 and 033-63) The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg distance: 3.500 NM FL310 True airspeed: 450 kts Headwind component at this level: 55 kts Initially planned takeoff mass (without extra fuel on board): 180.000 kg Fuel price: 0,27 $/l at destination The commander may carry on board 8.000 kg more fuel than that which is necessary. For this fuel transport operation to be cost effective, the maximum fuel price at departure must be: A) 0,38 $/l #B) 0,30 $/l C) 0,24 $/l D) 0,21 $/l 033-05 JET AEROPLANES FLIGHT PLANNING 68 © 2008 AVIATIONEXAM.com 23745 (A) 23746 (D) 23888 (B) 24754 (D) 24756 (A) 24759 (C) 24770 (D) 24793 (C) 23745. (AIR: atpl) (Refer to figure 033-44 and 033-63) The flight crew of a turbojet aeroplane prepares a flight using the following data: Flight leg distance: 3.500 NM Flight level FL310, true airspeed: 450 kts Headwind component at this level: 55 kts Initially planned takeoff mass (without extra fuel on board): 180.000 kg Fuel price: 0,30 $/l at departure The commander may carry a fuel quantity of 8.000 kg in addition to that which is necessary. For this fuel transport operation to be cost effective, the maximum fuel price at arrival must be: #A) 0,27 $/l B) 0,26 $/l C) 0,28 $/l
D) 0,33 $/l 23746. (AIR: atpl) (Refer to figure 033-56) The flight crew of a turbojet aeroplane prepares a flight using the following data: FL370 at Long Range (LR) cruise regime (Prescribed) mass at brake release: 204.500 kg Flight leg ground distance: 2.000 NM Temperatures: ISA Headwind component: 70 kts Total anti-ice set on ON for the entire flight No requested climb and descent correction of the fuel consumption The fuel required from takeoff to landing is: A) 27.770 kg B) 20.900 kg C) 22.160 kg #D) 29.440 kg 23888. (AIR: atpl) Given: FL370 M 0,74 OAT - 47 °C The TAS is: A) 424 kts #B) 434 kts C) 417 kts D) 428 kts 24754. (AIR: atpl) (Refer to figures 033-25 and 033-28) Given: Long range cruise at FL340 Distance C-D: 3.200 NM Temperature deviation from ISA: +12 °C Tailwind component: 50 kts Gross mass at C: 55.000 kg The fuel required from C to D is: A) 17.500 kg B) 14.200 kg C) 17.800 kg #D) 14.400 kg 24756. (AIR: atpl) (Refer to figure 033-29) Given: Long Range Cruise at FL350 OAT -45 °C Gross mass at the beginning of the leg: 40.000 kg Gross mass at the end of the leg: 39.000 kg Find:True airspeed (TAS) and cruise distance (NAM) for a twin jet aeroplane: #A) TAS 433 kts, 227 NAM. B) TAS 423 kts, 227 NAM. C) TAS 433 kts, 1.163 NAM. D) TAS 423 kts, 936 NAM. 24759. (AIR: atpl) (Refer to figure 033-22) Given: Aerodrome at MSL Cruise at FL280 ISA -10 °C Brake release mass: 57.500 kg
What is the climb fuel required? A) 1.100 kg B) 1.150 kg #C) 1.138 kg D) 2.200 kg 24770. (AIR: atpl) (Refer to figure 033-37 and Jeppesen Student Manual LONDON Heathrow 10-2 STAR or figure AP-08) Given: Aircraft mass: 49.700 kg FL280 Plan a descent to Heathrow elevation. What is the descent time? A) 8 min B) 10 min C) 17 min #D) 19 min 24793. (AIR: atpl) (Refer to figure 033-27) Given: Long range cruise: temp. -63 °C at FL330 Initial gross mass enroute: 54.100 kg Leg flight time: 29 min Find fuel consumption for this leg: A) 1.100 kg B) 1.107 kg #C) 1.093 kg D) 1.000 kg 033-05 JET AEROPLANES FLIGHT PLANNING 69 © 2008 AVIATIONEXAM.com 24872 (A) 24890 (A) 24893 (D) 24898 (D) 25023 (C) 25025 (D) 25032 (B) 25052 (A) 25057 (A) 25072 (D) 25102 (C) 25103 (C) 24872. (AIR: atpl) (Refer to figure 033-15) Given: Trip distance: 1.900 NM Fuel on board: 15.000 kg Landing weight: 50.000 kg What is the minimum pressure altitude for this flight? #A) 17.000 ft B) 10.000 ft C) FL370 D) FL250 24890. (AIR: atpl) (Refer to figure 033-20) Alternate airfield is 300 NGM, 50 kts tailwind and a landing weight of 50.000 kg, what is the fuel and time to the alternate? #A) 1.950 kg, 48 min. B) 1.650 kg, 48 min. C) 2.100 kg, 57 min. D) 1.950 kg, 57 min. 24893. (AIR: atpl) (Refer to figure 033-37) What is the time, fuel required and nautical air miles to descend from FL350 to sea level in turbulent air given an estimated landing weight of 50.000 kg? A) 20 min, 325 kg, 99 NAM.
B) 22 min, 290 kg, 108 NAM. C) 22 min, 290 kg, 105 NAM. #D) 20 min, 275 kg, 99 NAM. 24898. (AIR: atpl) (Refer to figure 033-38) After suffering undercarriage and pressurISAtion problems the aircraft is to be flown, undercarriage down, 400 NGM at FL100 for repairs. The estimated landing weight is 30.000 kg, the temperature is ISA+20 °C and a 50 kts headwind is expected. What is the fuel and time required for the trip? A) 7.500 kg, 2 hrs. B) 6.400 kg, 2 hrs 5 min. C) 4.600 kg, 1 hrs 40 min. #D) 5.800 kg, 2 hrs. 25023. (AIR: atpl) (Refer to figure 033-12) With a cruise weight of 50.000 kg, Cruising at Mach 0,78, what is the optimum altitude? A) 36.200 ft B) 35.800 ft #C) 35.400 ft D) 36.700 ft 25025. (AIR: atpl) (Refer to figure 033-24) An aircraft climbs out from an aerodrome at MSL to FL250, under ISA +20 °C conditions. If the brake release weight is 60.000 kg, what is the fuel and ground distance covered with a 40 kts tailwind? A) 1.100 kg, 62 NGM. B) 1.100 kg, 48 NGM. C) 1.300 kg, 64 NGM. #D) 1.300 kg, 81 NGM. 25032. (AIR: atpl) (Refer to figure 033-21) An aircraft weighing 56.000 kg is required to carry on an enroute straight and level hold at FL350 for 50 minutes. How much fuel will be used in the hold? A) 2.017 kg #B) 1.917 kg C) 2.133 kg D) 2.027 kg 25052. (AIR: atpl) (Refer to figure 033-29) An aircraft cruising at FL350 in light and variable winds turn at waypoint ALPHA weighing 53.500 kg and later turns waypoint BRAVO now weighing 50.200 kg. Assuming standard conditions what is the TAS, distance and specific fuel consumption between Alpha and BRAVO? #A) 429 kts, 627 NM, 5,26 kg/NM. B) 426 kts, 631 NM, 5,22 kg/NM. C) 429 kts, 627 NM, 6,25 kg/NM. D) 429 kts, 573 NM, 5,24 kg/NM. 25057. (AIR: atpl) (Refer to figure 033-42) The surplus burn off for tankering fuel is 20%, if the price at the departure airfield is 100 cents/gallon, what is the breakeven price at the destination airfield? #A) 125 cents/gallon. B) 100 cents/gallon. C) 80 cents/gallon.
D) 103 cents/gallon. 25072. (AIR: atpl) (Refer to figure 033-14) Given a distance of 1.000 NGM, 50 kts tailwind, ISA +0 °C, cruise FL370 and landing weight of 35.000 kg. What is the fuel and time for the trip? A) 4.950 kg, 2 hrs 15 mins. B) 5.350 kg, 2 hrs 15 mins. C) 4.300 kg, 2 hrs 40 mins. #D) 4.300 kg, 2 hrs 15 mins. 25102. (AIR: atpl) Given Mach number 0,82 and COAT -50 °C, TAS is: A) 466 kts B) 470 kts #C) 476 kts D) 496 kts 25103. (AIR: atpl) Given TAS 500 kts and COAT -40 °C, Mach number is: A) 0,80 B) 0,82 #C) 0,84 D) 0,88 033-05 JET AEROPLANES FLIGHT PLANNING 70 © 2008 AVIATIONEXAM.com 25116 (B) 25118 (B) 25119 (D) 25125 (D) 25126 (D) 25157 (C) 25167 (D) 25169 (A) 25116. (AIR: atpl) (Refer to figure 033-20) Given: Estimated dry operating mass: 35.500 kg Estimated load: 14.500 kg Final reserve fuel: 1.200 kg Distance to alternate: 95 NM Average true track: 219° Head wind component: 10 kts Find fuel to alternate and time to alternate: A) 1.100 kg, 44 min. #B) 1.100 kg, 25 min. C) 800 kg, 24 min. D) 800 kg, 40 min. 25118. (AIR: atpl) (Refer to figure 033-37) Assume M0,74/250 KIAS descent profile. How much time will elapse from top of descent (FL350) to level off at 5.000 feet? A) 6 minutes. #B) 16 minutes. C) 22 minutes. D) 23 minutes. 25119. (AIR: atpl) (Refer to figure 033-27) Given: Long range cruise at FL330 OAT -63 °C Gross mass: 50.500 kg Find the true air speed (TAS): A) 433 kts B) 418 kts
C) 431 kts #D) 420 kts 25125. (AIR: atpl) (Refer to figure 033-29) Given: Long range cruise OAT -45 °C FL350 Headwind component: 40 kts Start mass: 60.000 kg End mass: 55.000 kg Find the TAS at the end of the leg and the distance (NGM): A) 429 kts, 864 NGM. B) 430 kts, 864 NGM. C) 440 kts, 864 NGM. #D) 440 kts, 785 NGM. 25126. (AIR: atpl) (Refer to figure 033-20) Planning a flight from Paris (Charles de Gaulle) to London (Heathrow) for a twin jet aeroplane with alternate Manchester. Given: Headwind component from London to Manchester: 10 kts Distance from London to Manchester: 160 NM Assume the Estimated Landing Mass at the alternate is 50.000 kg Find the alternate fuel and the corresponding time: A) 1.200 kg, 26 minutes. B) 1.300 kg, 28 minutes. C) 1.600 kg, 36 minutes. #D) 1.450 kg, 33 minutes. 25157. (AIR: atpl) (Refer to figure 033-26) What would be the required change in fuel required if the temperature at FL280 was -31 °C? A) + 0,3% B) - 0,3% #C) + 0,6% D) - 0,6% 25167. (AIR: atpl) (Refer to figure 033-15) Given: Cruising altitude: 29.000 ft Temperature: ISA -10 °C Tailwind component: 45 kts Landing Mass: 55.000 kg Distance: 2.800 nautical ground miles Find trip time and fuel burn: A) 6 hrs 25 min, 16.000 kg. B) 6 hrs 40 min, 20.000 kg. C) 5 hrs 50 min, 18.000 kg. #D) 6 hrs 7 min, 17.100 kg. 25169. (AIR: atpl) (Refer to figure 033-20) Given: Estimated Dry Operating Mass: 35.500 kg Estimated load: 14.500 kg Final Reserve fuel: 1.200 kg Distance to alternate: 95 NM Average True Track: 219° Headwind component: 10 kts
Find fuel and time to alternate: #A) 1.100 kg, 25 min. B) 1.100 kg, 44 min. C) 800 kg, 24 min. D) 800 kg, 40 min. 033-05 JET AEROPLANES FLIGHT PLANNING 71 © 2008 AVIATIONEXAM.com 25170 (B) 25172 (A) 25176 (A) 25177 (A) 25178 (B) 26300 (B) 28314 (A) 28325 (D) 25170. (AIR: atpl) (Refer to figure 033-22) Given: Estimated Takeoff Mass: 52.000 kg Airport elevation: 387 ft Cruise: FL280 Wind velocity: 280/40 Temperature: ISA -10 °C Average Course: 340° (T) Find the ground distance to Top of Climb (TOC): A) 56 NM #B) 50 NM C) 53 NM D) 47 NM 25172. (AIR: atpl) (Refer to figures 033-23) Given: Brake release mass: 64.000 kg Temperature: ISA +10 °C Airport elevation: 3.000 ft Find time, fuel, atill air distance and TAS for an enroute climb at Mach 0,74/280 kts to FL350: #A) 26 min, 1.975 kg, 157 NAM, 399 kts. B) 26 min, 2.050 kg, 157 NAM, 399 kts. C) 20 min, 1.750 kg, 117 NAM, 288 kts. D) 25 min, 1.875 kg, 148 NAM, 391 kts. 25176. (AIR: atpl) (Refer to figure 033-16) Given: Cruise profile: Mach 0,74 Planned flight level: FL280 Estimated Landing Mass: 50.000 kg Trip distance: 200 NM Wind component: 30 kts headwind Find the estimated trip fuel: #A) 1.740 kg B) 1.550 kg C) 1.900 kg D) 1.450 kg 25177. (AIR: atpl) (Refer to figure 033-26) Given: Flight time from top of climb at FL280 to the enroute point is 48 minutes Cruise procedure is long range cruise Temperature is ISA -5 °C The takeoff mass is 56.000 kg and climb fuel 1.100 kg Find air distance in Nautical Air Miles (NAM) for this leg and fuel consumption for this leg:
#A) 345 NAM, 1.994 kg. B) 349 NAM, 2.000 kg. C) 345 NAM, 2.000 kg. D) 345 NAM, 2.006 kg. 25178. (AIR: atpl) (Refer to figure 033-22) Given: Mass at brake release: 57.500 kg Temperature: ISA -10° Headwind component: 16 kts Initial cruise: FL280 Find climb fuel: A) 1.238 kg #B) 1.138 kg C) 1.387 kg D) 1.040 kg 26300. (AIR: atpl) (Refer to figure 033-12, 033-13 and 033-31) Given: Estimated takeoff mass 57.000 kg Still air distance 150 NAM Outside air temperature (OAT) ISA -10° Cruise at Mach 0,74 Find cruise altitude and expected true airspeed: A) 25.000 ft; 445 kts. ##B) 25.000 ft; 435 kts. C) 22.000 ft; 441 kts. D) 22.000 ft; 451 kts. 28314. (AIR: atpl) (Refer to figure 033-85) You have a decompression at your cruising altitude and following information: Tailwind: 25 kts Distance to diversion airport: 820 kts ISA: +20 °C Weight: 55.000 kg Icing conditions: No What is your diversion fuel? A) 7.270 kg B) 7.000 kg C) 8.581 kg D) 7.480 kg 28325. (AIR: atpl) (Refer to figures 033-23) Given: Brake release mass: 58.000 kg Temperature: ISA +15 The fuel required to climb from an aerodrome at elevation 4.000 ft to FL300 is: A) 1.350 kg B) 1.400 kg C) 1.450 kg #D) 1.250 kg 033-05 JET AEROPLANES FLIGHT PLANNING 72 © 2008 AVIATIONEXAM.com 28327 (A) 28328 (B) 28329 (A) 28330 (D) 28331 (D) 29197 (D) 2270 (C) 2313 (C) 28327. (AIR: atpl)
(Refer to figure 033-83) Given : Distance B - C: 350 NM Cruise 300 KlAS at FL210 Temperature: - 40 °C Tailwind component: 70 kts Gross mass at B: 53.200 kg The fuel required from B - C is: #A) 1.940 kg B) 1.810 kg C) 2.800 kg D) 2.670 kg 28328. (AIR: atpl) (Refer to figure 033-21) The fuel required for 30 minutes holding, in a racetrack pattern, at PA 1.500 ft, mean gross mass 45.000 kg, is: A) 1.010 kg. #B) 1.090 kg. C) 1.310 kg. D) 2.180 kg. 28329. (AIR: atpl) (Refer to figure 033-21) The fuel required for 45 minutes holding, in a racetrack pattern, at PA 5.000 ft, mean gross mass 47 000 kg, is: #A) 1.635 kg B) 1.090 kg C) 1.690 kg D) 1.125 kg 28330. (AIR: atpl) (Refer to figure 033-20) Given: Distance to alternate 450 NM Landing mass at alternate: 45.000 kg Tailwind component: 50 kts The Alternate fuel required is: A) 2.900 kg B) 2.750 kg C) 3.050 kg #D) 2.500 kg 28331. (AIR: atpl) (Refer to figure 033-20) Given: Distance to Alternate: 400 NM Landing mass at Alternate: 50.000 kg Headwind component: 25 kts The alternate fuel required is: A) 2.650 kg B) 2.550 kg C) 2.900 kg #D) 2.800 kg 29197. (AIR: atpl) (Refer to figure 033-84) You have an engine failure and a decompression at the same time. Your data are: Tailwind: 25 kts Distance to diversion airport: 820 kts ISA +10° Weight: 55.000 kg Icing conditions: YES What is your diversion fuel?
A) 8.300 kg B) 7.035 kg C) 7.000 kg #D) 8.440 kg 033-05-02 Computerised flight planning 2270. (AIR: atpl) Which of the following statements is (are) correct with regard to computer flight plans? 1) The computer takes account of bad weather on the route and adds extra fuel. 2) The computer calculates alternate fuel sufficient for a missed approach, climb, cruise, descent and approach and landing at the destination alternate. A) Statement 1 only. B) Both statements. C) Statement 2 only. D) Neither statement. 2313. (AIR: atpl) Reference computer flight plans. Are they able to account for bad weather in calculating fuel required? A) Can automatically allow extra consumption for anti-icing use. B) Can automatically divert route around forecast thunderstorms. #C) No. D) Can automatically allow for poorly maintained engines. 033-05 JET AEROPLANES FLIGHT PLANNING 73 © 2008 AVIATIONEXAM.com 2317 (A) 2335 (A) 28323 (C) 2317. (AIR: atpl) Which of the following statements is (are) correct with regard to the advantages of computer flight plans? 1) The computer can file the ATC flight plan 2) Wind data used by the computer is always more up-todate than that available to the pilot #A) Statement 1 only. B) Statement 2 only. C) Both statements. D) Neither statement. 2335. (AIR: atpl) Which of the following statements is (are) correct with regard to the operation of flight planning computers ? 1) The computer can file the ATC flight plan. 2) In the event of inflight re-routing the computer produces a new plan #A) 1 only. B) 2 only. C) Neither D) Both. 28323. (AIR: atpl) Which of the following statements is (are) correct with regard to computer flight plans? 1) The computer takes account of bad weather on the route and adds extra fuel. 2) The computer calculates alternate fuel sufficient for a missed approach, climb, cruise, descent and approach and landing at the destination alternate.
A) 1. B) 1, 2. #C) 2. D) Neither statement. 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 74 © 2008 AVIATIONEXAM.com 1139 (C) 1145 (A) 1161 (A) 1190 (D) 1194 (B) 1200 (C) 1291 (A) 1293 (D) 2177 (D) 2183 (B) 033-06-01 Extraction of data 1139. (all) (Refer to figure 033-03) Given: FL75 OAT +10 °C Lean mixture at 2.300 RPM Find the fuel flow in gallons per hour (GPH) and TAS. A) 71,1 GPH, 143 kts. B) 11,6 GPH, 143 kts. #C) 11,6 GPH, 160 kts. D) 68,5 GPH, 160 kts. 1145. (all) (Refer to figure 033-01) Given: FL75 OAT: +5 °C During climb: average head wind component 20 kts Takeoff from MSL with the initial mass of 3.650 lbs Find the still air distance (NAM) and ground distance (NM) using the graph TIME, FUEL, DISTANCE TO CLIMB: #A) 18 NAM, 15 NM. B) 16 NAM, 18 NM. C) 18 NAM, 13 NM. D) 14 NAM, 18 NM. 1161. (all) (Refer to figure 033-01) Given: Takeoff mass 3.500 lbs Departure aerodrome pressure altitude 2.500 ft, OAT +10 °C First cruising level: FL140, OAT -5 °C Find the time, fuel and still air distance to climb: #A) 22 min; 6,7 GAL; 45 NAM. B) 24 min; 7,7 GAL; 47 NAM. C) 16,5 min; 4,9 GAL; 34,5 NAM. D) 23 min; 7,7 GAL; 50 NAM. 1190. (all) (Refer to figure 033-11) A flight is to be made to an airport, pressure altitude 3.000 ft, in a multi engine piston aeroplane (MEP1). The forecast OAT for the airport is -1 °C. The cruising level will be FL110, where OAT is -10 °C. Calculate the still air descent distance for: 145 KIAS Rate of descent 1.000 ft/min Gear and flaps up A) 25 NM B) 29 NM
C) 36 NM #D) 20 NM 1194. (all) (Refer to figure 033-06) A flight is to be made from one airport (elevation 3.000 ft) to another in a multi engine piston aeroplane (MEP1). The cruising level will be FL110. The temperature at FL110 is ISA-10 °C. The temperature at the departure aerodrome is -1 °C. Calculate the fuel to climb with mixture rich. A) 9 US gallon. #B) 6 US gallon. C) 12 US gallon. D) 3 US gallon. 1200. (all) (Refer to figure 033-01) Given: L75 OAT: +5 °C During climb: average head wind component 20 kts Takeoff from MSL with the initial mass of 3.650 lbs. Find time and fuel to climb. A) 7 min; 2,6 USG. B) 10 min; 3,6 USG. #C) 9 min; 3,3 USG. D) 9 min; 2,7 USG. 1291. (all) (Refer to Jeppesen Manual MUNICH ILS Rwy 26R (11-4) or figure AP-01) The ILS frequency and identifier are: #A) 108,7 IMNW B) 108,7 IMSW C) 108,3 IMNW D) 108,3 IMSW 1293. (all) (Refer to Jeppesen Manual MUNICH NDB DME Rwy 26L approach (16-3) or figure AP-02) The frequency and identifier of the NDB for the published approaches are: A) 112,3 MUN B) 108,6 DMS #C) 338 MNW D) 400 MSW 2177. (all) (Refer to Jeppesen Manual, SID charts for Paris CharlesdeGaulle (20-3) or figure AP-03) Determine the distance of the departure route ABB 8A: A) 72 NM B) 74 NM C) 72,5 NM #D) 74,5 NM 2183. (all) (Refer to Jeppesen Manual LONDON HEATHROW ILS DME Rwy 09L (11-2) or figure AP-05). The decision altitude for an ILS straight-in landing is: A) 480 ft #B) 280 ft C) 200 ft D) 400 ft 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN
75 © 2008 AVIATIONEXAM.com 2185 (C) 2188 (A) 2195 (B) 2201 (B) 2205 (C) 2206 (B) 2221 (D) 2233 (B) 2240 (B) 2241 (C) 2257 (A) 2185. (all) (Refer to Jeppesen Manual SID chart for AMSTERDAM SCHIPOL (10-3) or figure AP-06) Which statement is correct for ANDIK departures from runway 19L? A) Maximum IAS 250 kts turning left at SPL 3,1 DME. B) Cross ANDIK below FL60. #C) Contact SCHIPOL DEPARTURE 119,05 passing 2.000 ft and report altitude. D) The distance to ANDIK is 25 NM. 2188. (all) (Refer to Jeppesen Manual AMSTERDAM SCHIPOL - ILS DME RWY 22 (11-6) or figure AP-07) The missed approach procedure is to climb to an altitude of ___ on a track of ___. #A) 2.000 ft; 160° B) 200 ft; 223° C) 3.000 ft; 160° D) 3.000 ft; 223° 2195. (all) (Refer to Jeppesen Manual Munich SID (10-3D) or figure AP-10) Which is the correct departure via KEMPTEN from runway 26L? A) KEMPTEN THREE ECHO. #B) KEMPTEN FIVE SIERRA. C) KEMPTEN THREE QUEBEC. D) KEMPTEN THREE NOVEMBER. 2201. (all) (Refer to Route Manual chart STAR LONDON Heathrow (10-2) or figure AP-08) Planning a IFR flight from Paris (Charles de Gaulle) to London (Heathrow). Find the elevation of the destination aerodrome. A) 77 ft #B) 80 ft C) 177 ft D) 100 ft 2205. (all) (Refer to Jeppesen Manual - ZURICH ILS Rwy 16 (11-2) or figure AP-11) The lowest published authorised RVR for an ILS approach, glide slope out, all other aids serviceable, aeroplane category A, is: A) 800 m B) 600 m #C) 720 m D) 1.500 m 2206. (all) (Refer to Jeppesen Manual - LONDON HEATHROW ILS DME Rwy 09R (11-1) or figure AP-12) The Minimum Descent Altitude (MDA) for an ILS approach, glide slope out, is: A) 405 ft #B) 480 ft C) 275 ft
D) 200 ft 2221. (all) (Refer to Jeppesen Manual, any SID or approach chart for London Heathrow or figure AP-12). Which of the following is the correct Minimum Safe Altitude (MSA) for the airport? A) East sector 2.300 ft within 50 NM. B) West sector 2.300 ft within 25 NM. C) East sector 2.100 ft within 50 NM. #D) West sector 2.100 ft within 25 NM. 2233. (all) (Refer to Route Manual chart E(HI)4 or figure HI-09) An aeroplane has to fly from Abbeville (50°08,1 N 001°51,3 E) to Biggin (51°19,8 N 00°00,2 E). At Biggin you can find: 141°. This is: A) the average true course of the great circle from Biggin to Abbeville. #B) the magnetic great circle course from Biggin to Abbeville. C) the radial, referenced to true north, of Biggin to fly inbound. D) the magnetic course to fly inbound to Biggin. 2240. (all) (Refer to Jeppesen Manual MADRID, BARAJAS page 11-1. ILS DME RWY 33 or figure AP-15) The minimum glide slope interception altitude for a full ILS is: A) 3.500 ft #B) 4.000 ft C) 2.067 ft D) 1.567 ft 2241. (all) (Refer to Route Manual chart SID PARIS Charles-De-Gaulle (20-3) or figure AP-03) Planning a IFR flight from Paris (Charles de Gaulle) to London (Heathrow). Find the elevation of the departure aerodrome. A) 217 ft B) 268 ft #C) 387 ft D) 2 ft 2257. (all) (Refer to Jeppesen Manual Paris Charles-de-Gaulle (21-7) ILS rwy 10 or figure AP-16) What is the ILS course? #A) 088° B) 100° C) 118° D) 268° 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 76 © 2008 AVIATIONEXAM.com 2271 (B) 2282 (C) 2284 (C) 2286 (C) 2296 (B) 2303 (D) 2306 (D) 2308 (B) 2319 (A) 2271. (AIR: atpl; HELI: atpl, cpl) Given: 15.000 kg total fuel Reserve 1.500 kg TAS 440 kts Wind component 45 head outbound Average fuel flow 2.150 kg/hrs
What is the distance to the point of safe return? A) 1.520 NM #B) 1.368 NM C) 1.702 NM D) 1.250 NM 2282. (AIR: atpl; HELI: atpl, cpl) If CAS is 190 kts, Altitude 9.000 ft, Temp. ISA - 10 °C, True Course (TC) 350°, W/V 320/40, distance from departure to destination is 350 NM, endurance 3 hours and actual time of departure is 1105 UTC. The distance from departure to Point of Equal Time (PET) is: A) 183 NM B) 147 NM #C) 203 NM D) 167 NM 2284. (AIR: atpl; HELI: atpl, cpl) Given: Distance from A to B: 2.050 NM Mean groundspeed on 440 kts Mean groundspeed back 540 kts The distance to the point of equal time (PET) between A and B is: A) 920 NM B) 1.025 NM #C) 1.130 NM D) 1.153 NM 2286. (AIR: atpl; HELI: atpl, cpl) Find the time to the Point of Safe Return (PSR). Given: Maximum usable fuel: 15.000 kg Minimum reserve fuel: 3.500 kg TAS out: 425 kts Head wind component out: 30 kts TAS return: 430 kts Tailwind component return: 20 kts Average fuel flow: 2.150 kg/hrs A) 2 hrs 59 min B) 3 hrs 43 min #C) 2 hrs 51 min D) 2 hrs 43 min 2296. (AIR: atpl; HELI: atpl, cpl) Given: Course A to B: 088° (T) Distance: 1.250 NM Mean TAS: 330 kts Mean W/V: 340°/60 kts The time from A to the PET between A and B is: A) 1 hour 54 minutes. B) 1 hour 42 minutes. #C) 1 hour 39 minutes. D) 2 hours 02 minutes. 2303. (AIR: atpl; HELI: atpl, cpl) Given: Fuel flow: 2.150 kg/hrs Total fuel in tanks: 15.000 kg Fuel reserve required on arrival: 3.500 kg TAS outbound: 420 kts, wind -30 kts TAS home bound: 430 kts, wind +20 kts Find the time to Point of Safe Return. A) 2 hrs 06 min B) 1 hrs 26 min
C) 3 hrs 33 min #D) 2 hrs 52 min 2306. (AIR: atpl; HELI: atpl, cpl) Given: Distance A to B: 3.060 NM Mean ground speed OUT: 440 kts Mean ground speed BACK: 540 kts Safe Endurance: 10 hours The time to the Point of Safe Return (PSR) is: A) 5 hours 20 minutes. B) 5 hours 45 minutes. C) 3 hours 55 minutes. #D) 5 hours 30 minutes. 2308. (AIR: atpl) Given: Distance X to Y: 2.700 NM Mach number: 0,75 Temperature: -45 °C Mean wind component ON: 10 kts Tailwind Mean wind compontent BACK: 35 kts tailwind The distance from X to the point of equal time (PET) between X and Y is: A) 1.350 NM #B) 1.386 NM C) 1.313 NM D) 1.425 NM 2319. (AIR: atpl; HELI: atpl, cpl) Given the following: D = flight distance X = distance to Point of Equal Time GSo = groundspeed out GSr = groundspeed return The correct formula to find distance to Point of Equal Time is: #A) x = D x GSr / (GSo + GSr) B) x = D x GSo / (GSo + GSr) C) x = (D/2) x GSo / (GSo + GSr) D) x = (D/2) + GSr / (GSo + GSr) 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 77 © 2008 AVIATIONEXAM.com 2913 (D) 4291 (C) 4325 (C) 4327 (D) 4362 (D) 12246 (C) 12250 (D) 12266 (A) 14161 (A) 2913. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 500 NM True track: 090° Wind: 090°/20 TAS: 150 kts What is the distance and time of the PET from the departure point? A) Distance: 382 NM; Time: 176 min. B) Distance: 250 NM; Time: 88 min. C) Distance: 217 NM; Time: 100 min. #D) Distance: 283 NM; Time: 131 min. 4291. (AIR: atpl; HELI: atpl, cpl) Given: X = Distance A to point of equal time (PET) between A and
B E = Endurance D = Distance A to B O = Groundspeed ON H = Groundspeed BACK The formula for calculating the distance X to point of equal time (PET) is: A) x = (E x O x H) / (O + H) B) x = (D x O) / (O + H) #C) x = (D x H) / (O + H) D) x = (D x O x H) / (O + H) 4325. (AIR: atpl; HELI: atpl, cpl) Find the distance to the Point of Safe Return (PSR), given: Maximum usable fuel: 15.000 kg Minimum reserve fuel: 3.500 kg OUTBOUND: TAS 425 kts, head wind component 30 kts, fuel flow 2.150 kg/hrs RETURN: TAS 430 kts, tailwind component 20 kts, fuel flow 2.150 kg/hrs A) 1.463 NM B) 1.143 NM #C) 1.125 NM D) 1.491 NM 4327. (all) Integrated range curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is: A) to determine the optimum speed considering the fuel cost as well as the time related cost of the aeroplane. B) to determine the flight time for a certain leg under consideration of temperature deviations. C) to determine the still air distance for a wind components varying with altitude. #D) to determine the fuel consumption for a certain still air distance considering the decreasing fuel flow with decreasing mass. 4362. (AIR: atpl; HELI: atpl, cpl) A flight is planned from L to M, distance 850 NM. Using the following data, calculate the time and distance to PSR: Wind component out: 35 kts (TWC) TAS 450 kts Mean fuel flow out: 2.500 kg/hrs Mean fuel flow inbound: 1.900 kg/hrs Fuel available: 6.000 kg A) 1 hrs 30 min; 660 NM. B) 1hrs 30 min; 616 NM. C) 1 hrs 16 min; 606 NM. #D) 1 hrs 16 min; 616 NM. 12246. (all) (Refer to Route Manual SID chart 20-3 for PARIS CharlesdeGaulle or figure AP-03) Planning an IFR-flight from Paris (Charles de Gaulle) RWY 27 to London. Given: Distance from PARIS Charles-de-Gaulle to top of climb: 50 NM. Determine the distance from the top of climb (TOC) to ABB 116,6. A) 36,5 NM B) 31 NM #C) 24,5 NM
D) 33 NM 12250. (all) (Refer to Route Manual chart E(HI)4 CAA-Edition, Instrument approach chart ILS DME Rwy 27R or figures HI-09; AP-08 and AP-09) Planning an IFR-flight from Paris to London (Heathrow) via initial approach fix (IAF) Biggin VOR. The distance from top of descent (TOD) to Rwy 27R is 76 NM. Determine the distance from ABB 116,6 to TOD. A) 60 NM B) 100 NM C) 55 NM #D) 49 NM 12266. (AIR: atpl; HELI: atpl, cpl) Find the distance from waypoint 3 (WP 3) to the critical point. Given: Distance from WP 3 to WP 4: 750 NM TAS out: 430 kts TAS return: 425 kts Tailwind component out: 30 kts Headwind component return: 40 kts #A) 342 NM B) 375 NM C) 408 NM D) 403 NM 14161. (AIR: all) (Refer to figure 033-09) For the MEP, if the OAT is -20 °C at 19.000 ft the TAS at 45% power is: #A) 159 knots B) 162 knots C) 165 knots D) 168 knots 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 78 © 2008 AVIATIONEXAM.com 17201 (A) 23811 (A) 23812 (B) 23879 (C) 23890 (D) 23892 (D) 23893 (C) 23896 (D) 23898 (D) 23900 (D) 17201. (AIR: atpl; HELI: atpl, cpl) If CAS is 190 kts, Altitude 9.000 ft. Temp. ISA - 10 °C, True Course (TC) 350°, W/V 320/40, distance from departure to destination is 350 NM, endurance 3 hours, and actual time of departure is 1105 UTC. The Point of Equal Time (PET) is reached at: #A) 1213 UTC B) 1221 UTC C) 1233 UTC D) 1203 UTC 23811. (all) (Refer to figures 033-66, 033-67 and 033-68) What is the local time (LT) in Greece in Winter and Summer? #A) LT = UTC + 2 Hours; LT = UTC + 3 Hours B) LT = UTC - 2 Hours; LT = UTC - 3 Hours C) LT + 2 Hours = UTC; LT + 3 Hours = UTC D) LT - 3 Hours = UTC; LT - 2 Hours = UTC 23812. (all) (Refer to figures 033-66, 033-67 and 033-68) What is the local time (LT) in the Netherlands in Winter and
Summer? A) LT - 2 Hours = UTC; LT - 1 Hour = UTC #B) LT - 1 Hour = UTC; LT - 2 Hours = UTC C) LT = UTC + 2 Hours; LT = UTC + 1 Hour D) LT = UTC - 1 Hour; LT = UTC - 2 Hours 23879. (AIR: all) An operator shall ensure that calculation of usable fuel for an IFR flight with a turbojet aeroplane for which no destination alternate is required includes, taxi fuel, trip fuel, contingency fuel and fuel to fly for: A) 45 minutes plus 10% of the flight time planned to be spent at cruising level or two hours whichever is less. B) 2 hours at normal cruise consumption. #C) 45 minutes at holding speed at 450 m above aerodrome elevation in standard conditions. D) 45 minutes at holding speed at 450 m above MSL in standard conditions. 23890. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 140 NM GS Out: 90 kts GS Home: 80 kts What is the distance of the PET from the departure point? A) 122 NM B) 74 NM C) 70 NM #D) 66 NM 23892. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 150 NM True track: 020 W/V: 180/30 TAS: 130 kts What is the distance of the PET from the departure point? A) 65 NM B) 75 NM C) 91 NM #D) 59 NM 23893. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 150 NM True track: 142 W/V: 200/15 TAS: 132 kts What is the distance of the PET from the departure point? A) 75 NM B) 71 NM #C) 79 NM D) 134 NM 23896. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 165 NM True track: 055 W/V: 360/20 TAS: 105 kts What is the distance of the PET from the departure point? A) 132 NM B) 73 NM C) 83 NM #D) 92 NM
23898. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 180 NM True track: 310 W/V: 010/20 TAS: 115 kts What is the distance of the PET from the departure point? A) 92 NM B) 82 NM C) 90 NM #D) 98 NM 23900. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 220 NM True track: 175 W/V: 220/10 TAS: 135 kts What is the distance of the PET from the departure point? A) 136 NM B) 103 NM C) 110 NM #D) 116 NM 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 79 © 2008 AVIATIONEXAM.com 23902 (D) 23903 (A) 23905 (C) 23907 (D) 23909 (D) 23911 (C) 23913 (C) 23915 (D) 23917 (D) 23902. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 250 NM GS Out: 130 kts GS Home: 100 kts What is the distance of the PET from the departure point? A) 192 NM B) 141 NM C) 125 NM #D) 109 NM 23903. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 2.500 NM GS Out: 540 kts GS Home: 470 kts What is the time of the PET from the departure point? #A) 129 min B) 171 min C) 28 min D) 149 min 23905. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 256 NM GS Out: 160 kts GS Home: 110 kts What is the distance of the PET from the departure point? A) 128 NM B) 152 NM #C) 104 NM D) 176 NM 23907. (AIR: atpl; HELI: atpl, cpl)
Given: Distance from departure to destination: 270 NM True track: 030° W/V: 120/35 TAS: 125 kts What is the distance and time of the PET from the departure point? A) Distance: 141 NM; Time: 68 min. B) Distance: 141 NM; Time: 65 min. C) Distance: 130 NM; Time: 68 min. #D) Distance: 135 NM; Time: 65min. 23909. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 285 NM True track: 348° W/V: 280/25 TAS: 128 kts What is the distance of the PET from the departure point? A) 123 NM B) 130 NM C) 143 NM #D) 154 NM 23911. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 315 NM True track: 343° W/V: 015/15 TAS: 100 kts What is the distance of the PET from the departure point? A) 167 NM B) 139 NM #C) 176 NM D) 148 NM 23913. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 338 NM True track: 045° W/V: 225/35 TAS: 120 kts What is the distance and time of the PET from the departure point? A) Distance: 169 NM; Time: 85 min. B) Distance: 218 NM; Time: 85 min. #C) Distance: 120 NM; Time: 46 min. D) Distance: 185 NM; Time: 72 min. 23915. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 340 NM GS Out: 150 kts GS Home: 120 kts What is the distance of the PET from the departure point? A) 272 NM B) 189 NM C) 170 NM #D) 151 NM 23917. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 340 NM True track: 320° W/V: 160/40
TAS: 110 kts What is the distance of the PET from the departure point? A) 219 NM B) 228 NM C) 121 NM #D) 112 NM 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 80 © 2008 AVIATIONEXAM.com 23919 (A) 23921 (A) 23923 (C) 23925 (A) 23926 (C) 23928 (D) 23929 (C) 23930 (D) 23931 (B) 23919. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 350 NM True track: 320° W/V: 350/30 TAS: 130 kts What is the distance and time of the PET from the departure point? #A) Distance: 210 NM; Time: 122 min. B) Distance: 139 NM; Time: 54 min. C) Distance: 123 NM; Time: 74 min. D) Distance: 139 NM; Time: 81 min. 23921. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 435 NM GS Out: 110 kts GS Home: 130 kts What is the distance of the PET from the departure point? #A) 236 NM B) 199 NM C) 218 NM D) 368 NM 23923. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 470 NM True track: 237° W/V: 300/25 TAS: 125 kts What is the distance of the PET from the departure point? A) 235 NM B) 214 NM #C) 256 NM D) 205 NM 23925. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 500 NM GS Out: 95 kts GS Home: 125 kts What is the distance of the PET from the departure point? #A) 284 NM B) 216 NM C) 250 NM D) 380 NM 23926. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 875 NM True track: 240°
W/V: 060/50 TAS: 500 kts What is the distance and time of the PET from the departure point? A) Distance: 716 NM; Time: 78 min. B) Distance: 481 NM; Time: 64 min. #C) Distance: 394 NM; Time: 43 min. D) Distance: 438 NM; Time: 53 min. 23928. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 95 NM True track: 105° W/V: 060/15 TAS: 140 kts What is the distance of the PET from the departure point? A) 44 NM B) 47,5 NM C) 82 NM #D) 51 NM 23929. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 950 NM GS Out: 275 kts GS Home: 225 kts What is the time of the PET from the departure point? A) 114 min B) 139 min #C) 93 min D) 39 min 23930. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 1.100 NM True track: 280° W/V: 100/80 TAS: 440 kts What is the distance time of the PET from the departure point? A) Distance: 550 NM; Time: 75 min. B) Distance: 650 NM; Time: 108 min. C) Distance: 650 NM; Time: 75 min. #D) Distance: 450 NM; Time: 52 min. 23931. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 1.345 NM GS Out: 480 kts GS Home: 360 kts What is the time of the PET from the departure point? A) 128 min #B) 72 min C) 96 min D) 50 min 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 81 © 2008 AVIATIONEXAM.com 23932 (C) 23933 (B) 23934 (A) 23935 (C) 23936 (D) 23937 (D) 23938 (A) 23939 (B) 23941 (A) 23932. (AIR: atpl; HELI: atpl, cpl) Given:
Distance from departure to destination: 1.860 NM GS Out: 360 kts GS Home: 400 kts What is the time of the PET from the departure point? A) 147 min B) 132 min #C) 163 min D) 22 min 23933. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 1.950 NM GS Out: 400 kts GS Home: 300 kts What is the time of the PET from the departure point? A) 223 min #B) 125 min C) 167 min D) 29 min 23934. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 2.200 NM True track: 150° W/V: 330/50 TAS: 460 kts What is the distance and time of the PET from the departure point? #A) Distance: 980 NM; Time: 115 min. B) Distance: 1.120 NM; Time: 179 min. C) Distance: 1.100 NM; Time: 179 min. D) Distance: 980 NM; Time: 144 min. 23935. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 2.380 NM GS Out: 420 kts GS Home: 520 kts What is the time of the PET from the departure point? A) 152 min B) 123 min #C) 188 min D) 19 min 23936. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 2.800 NM True track: 140° W/V: 140/100 TAS: 500 kts What is the distance and time of the PET from the departure point? A) Distance: 1.120 NM; Time: 134 min. B) Distance: 1.120 NM; Time: 114 min. C) Distance: 1.440 NM; Time: 168 min. #D) Distance: 1.680 NM; Time: 252 min. 23937. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 330 NM Safe Endurance: 5 hrs True Track: 170° W/V: 140/25 TAS: 125 kts What is the distance of the PSR from the departure point?
A) 30 NM B) 194 NM C) 150 NM #D) 303 NM 23938. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 1.000 NM Safe Endurance: 4 hrs TAS: 500 kts Ground speed out: 550 kts Ground speed home: 450 kts What is the distance of the PSR from the departure point? #A) 990 NM B) 450 NM C) 495 NM D) 10 NM 23939. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 150 NM Safe Endurance: 2,4 hrs True Track: 250° W/V: 280/15 TAS: 120 kts What is the distance of the PSR from the departure point? A) 83 NM #B) 142 NM C) 71 NM D) 98 NM 23941. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 150 NM Safe Endurance: 3,2 hrs TAS: 90 kts Ground speed out: 100 kts Ground speed home: 80 kts What is the distance and time of the PSR from the departure point? #A) Distance: 142 NM; Time: 85 min. B) Distance: 67 NM; Time: 50 min. C) Distance: 71 NM; Time: 47 min. D) Distance: 8 NM; Time: 5 min. 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 82 © 2008 AVIATIONEXAM.com 23942 (C) 23944 (D) 23946 (C) 23948 (A) 23950 (D) 23951 (A) 23953 (B) 23955 (B) 23942. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 1.500 NM Safe endurance: 4,5 hrs TAS: 450 kts Ground speed out: 480 kts Ground speed home: 410 kts What is the time of the PSR from the departure point? A) 66 min B) 101 min #C) 124 min D) 63 min 23944. (AIR: atpl; HELI: atpl, cpl)
Given: Distance from departure to destination: 180 NM Safe endurance: 2 hrs TAS: 120 kts Ground speed out: 135 kts Ground speed home: 105 kts What is the distance and time of the PSR from the departure point? A) Distance: 62 NM; Time: 28 min. B) Distance: 79 NM; Time: 45 min. C) Distance: 59 NM; Time: 30 min. #D) Distance: 118 NM; Time: 53 min. 23946. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 180 NM Safe endurance: 2,8 hrs True track: 065° W/V: 245/25 TAS: 100 kts What is the distance of the PSR from the departure point? A) 66 NM B) 68 NM #C) 131 NM D) 49 NM 23948. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 190 NM Safe endurance: 2,4 hrs True track: 120° W/V: 030/40 TAS: 130 kts What is the distance of the PSR from the departure point? #A) 148 NM B) 95 NM C) 73 NM D) 44 NM 23950. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 200 NM Safe endurance: 3 hrs TAS: 130 kts Ground speed out: 150 kts Ground speed home: 110 kts What is the distance PSR from the departure point? A) 10 NM B) 85 NM C) 95 NM #D) 190 NM 23951. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 2.000 NM Safe endurance: 5 hrs TAS: 500 kts Ground speed out: 480 kts Ground speed home: 520 kts What is the distance of the PSR from the departure point? #A) 1.248 NM B) 1.040 NM C) 624 NM D) 752 NM
23953. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 210 NM Safe endurance: 2,5 hrs True track: 035° W/V: 250/20 TAS: 105 kts What is the distance of the PSR from the departure point? A) 88 NM #B) 127 NM C) 64 NM D) 172 NM 23955. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 210 NM Safe endurance: 3,5 hrs True track: 310° W/V: 270/30 TAS: 120 kts What is the distance of the PSR from the departure point? A) 125 NM #B) 200 NM C) 100 NM D) 10 NM 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 83 © 2008 AVIATIONEXAM.com 23957 (B) 23959 (A) 23960 (B) 23962 (B) 23964 (C) 23965 (A) 23967 (B) 23968 (A) 23957. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 215 NM Safe endurance: 3,3 hrs True track: 005° W/V: 290/15 TAS: 125 kts What is the distance of the PSR from the departure point? A) 112 NM #B) 205 NM C) 103 NM D) 9 NM 23959. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 240 NM Safe endurance: 3,5 hrs TAS: 125 kts Ground speed out: 110 kts Ground speed home: 140 kts What is the distance and time of the PSR from the departure point? #A) Distance: 216 NM; Time: 118 min. B) Distance: 134 NM; Time: 58 min. C) Distance: 108 NM; Time: 52 min. D) Distance: 24 NM; Time: 13 min. 23960. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 2.450 NM Safe endurance: 7,5 hrs TAS: 410 kts
Ground speed out: 360 kts Ground speed home: 460 kts What is the time of the PSR from the departure point? A) 198 min #B) 252 min C) 111 min D) 156 min 23962. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 260 NM Safe endurance: 4,1 hrs True track: 150° W/V: 100/30 TAS: 110 kts What is the distance of the PSR from the departure point? A) 154 NM #B) 213 NM C) 107 NM D) 47 NM 23964. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 300 NM Safe endurance: 4 hrs TAS: 110 kts Ground speed out: 120 kts Ground speed home: 100 kts What is the distance of the PSR from the departure point? A) 109 NM B) 136 NM #C) 218 NM D) 82 NM 23965. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 3.000 NM Safe endurance: 8 hrs TAS: 520 kts Ground speed out: 600 kts Ground speed home: 440 kts What is the time of the PSR from the departure point? #A) 203 min B) 173 min C) 277 min D) 117 min 23967. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 320 NM Safe endurance: 4,3 hrs True track: 120° W/V: 180/40 TAS: 130 kts What is the distance of the PSR from the departure point? A) 185 NM #B) 263 NM C) 131NM D) 59 NM 23968. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 330 NM Safe endurance: 5 hrs True track: 170°
W/V: 140/25 TAS: 125 kts What is the distance of the PSR from the departure point? #A) 302 NM B) 194 NM C) 150 NM D) 30 NM 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 84 © 2008 AVIATIONEXAM.com 23970 (A) 23971 (C) 23973 (C) 23975 (B) 23976 (A) 23978 (A) 23980 (D) 23981 (B) 23970. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 360 NM Safe endurance: 4,5 hrs True track: 345° W/V: 260/30 TAS: 140 kts What is the distance of the PSR from the departure point? #A) 308 NM B) 185 NM C) 154 NM D) 52 NM 23971. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 3.750 NM Safe endurance: 9,5 hrs True track: 360° W/V: 360/50 TAS: 480 kts What is the distance of the PSR from the departure point? A) 1.128 NM B) 2.070 NM #C) 2.255 NM D) 1.495 NM 23973. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 400 NM Safe endurance: 2,5 hrs TAS: 115 kts Ground speed out: 130 kts Ground speed home: 105 kts What is the distance of the PSR from the departure point? A) 73 NM B) 179 NM #C) 145 NM D) 255 NM 23975. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 410 NM Safe endurance: 3,6 hrs True track: 055° W/V: 180/35 TAS: 120 kts What is the distance of the PSR from the departure point? A) 169 NM #B) 210 NM C) 102 NM
D) 203 NM 23976. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 4.630 NM Safe endurance: 12,4 hrs True track: 240° W/V: 060/80 TAS: 530 kts What is the distance of the PSR from the departure point? #A) 3.211 NM B) 1.966 NM C) 6.106 NM D) 1.419 NM 23978. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 480 NM Safe endurance: 5 hrs True track: 315° W/V: 100/20 TAS: 115 kts What is the distance of the PSR from the departure point? #A) 280 NM B) 205 NM C) 141 NM D) 199 NM 23980. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 500 NM Safe endurance: 4 hrs TAS: 140 kts Ground speed out: 150 kts Ground speed home: 130 kts What is the distance and time of the PSR from the departure point? A) Distance: 221 NM; Time: 89 min. B) Distance: 232 NM; Time: 107 min. C) Distance: 139 NM; Time: 60 min. #D) Distance: 279 NM; Time: 111 min. 23981. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 5.000 NM Safe endurance: 10 hrs TAS: 450 kts Ground speed out: 500 kts Ground speed home: 400 kts What is the distance of the PSR from the departure point? A) 2.500 NM #B) 2.222 NM C) 1.111 NM D) 2.778 NM 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 85 © 2008 AVIATIONEXAM.com 23983 (A) 23984 (B) 23985 (B) 23986 (A) 24741 (D) 24844 (C) 25021 (D) 25122 (C) 25185 (A) 23983. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 550 NM
Safe endurance: 3,6 hrs True track: 200° W/V: 220/15 TAS: 130 kts What is the distance of the PSR from the departure point? #A) 231 NM B) 305 NM C) 116 NM D) 319 NM 23984. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 6.340 NM Safe endurance: 15 hrs True track: 090° W/V: 270/100 TAS: 520 kts What is the distance of the PSR from the departure point? A) 2.560 NM #B) 3.756 NM C) 1.878 NM D) 2.584 NM 23985. (AIR: atpl; HELI: atpl, cpl) Given: Distance from departure to destination: 950 NM Safe endurance: 3,5 hrs TAS: 360 kts Ground speed out: 320 kts Ground speed home: 400 kts What is the distance and time of the PSR from the departure point? A) Distance: 528 NM; Time: 79 min. #B) Distance: 622 NM; Time: 117 min. C) Distance: 311 NM; Time: 52 min. D) Distance: 328 NM; Time: 62 min. 23986. (all) Given: Fuel density: 0,78 kg/l Dry Operating Mass: 33.500 kg Traffic load: 10.600 kg Maximum allowable takeoff mass: 66.200 kg Taxi fuel: 200 kg Tank capacity: 22.500 l The maximum possible takeoff fuel is: #A) 17.350 kg B) 22.100 kg C) 17.550 kg D) 21.900 kg 24741. (AIR: atpl; HELI: atpl, cpl) Given: Track: 355° (T) Wind velocity: 340/30 kts TAS: 140 kts Total distance A to B: 350 NM What are the time and distance to the point of equal time between A and B? A) 75 mins; 211 NM. B) 75 mins; 140 NM. C) 50 mins; 140 NM. #D) 114 mins; 211 NM. 24844. (AIR: atpl; HELI: atpl, cpl)
Flying from A to B, 270 NM, true track 030°, wind velocity 120/35, TAS 125 kts. What are the distance and time to the Point of Equal Time? A) 141 NM; 65 min. B) 141 NM; 68 min. #C) 135 NM; 68 min. D) 150 NM; 65 min. 25021. (AIR: atpl; HELI: atpl, cpl) An aircraft is to fly from B to C. The total fuel available is 50.000 kg but the aircraft must land with at least 5.000 kg. From B to C the TAS is 400 kts, wind component 30 kts headwind, fuel flow 7.800 kg/hrs. Should the aircraft have to return from the PSR its TAS shall be 380 kts, wind component 30 kts tailwind and fuel flow 7.500kg/hrs. What is the distance and time to the point of safe return (PSR) from B? A) 1.270 NM; 206 min. B) 1.250 NM; 174 min. C) 1.071 NM; 174 min. #D) 1.143 NM; 185 min. 25122. (AIR: atpl; HELI: atpl, cpl) Given: X = Distance A to Point of Safe Return (PSR) between A and B E = Endurance D = Distance A to B O = Ground speed on H = Ground speed back The formula for calculating the distance X to PSR is: A) X = D H / (O + H) B) X = D O / (O + H) #C) X = E O H / (O + H) D) X = D O H / (O + H) 25185. (AIR: atpl; HELI: atpl, cpl) Track A to B: 088° (T) Distance: 1.250 NM Mean TAS: 330 kts Mean wind: 340/60 kts Find the time from A to PET: #A) 1 hrs 44 min B) 1 hrs 39 min C) 2 hrs 02 min D) 1 hrs 54 min 033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN 86 © 2008 AVIATIONEXAM.com 25561 (A) 25561. (AIR: all) (Refer to figures 033-72) Finish the endurance / fuel calculations and determine ATC endurance for a twin jet aeroplane, with the help of the table provided. Contingency is 5% of the planned trip fuel and fuel flow for extra fuel is 2.400 kg/hrs: #A) ATC endurance: 04:07 B) ATC endurance: 03:52 C) ATC endurance: 03:37 D) ATC endurance: 04:12
033-07 OFFSHORE OR REMOTE AREA OPERATION 87 © 2008 AVIATIONEXAM.com 22881 (B) 22883 (A) 22881. (HELI: atpl, cpl) To carry out a VFR flight to an off-shore platform, the minimum fuel quantity on board is: A) that defined for VFR flights over land increased by 10%. #B) identical to that defined for VFR flights over land. C) at least equal to that defined for IFR flights. D) that defined for VFR flights over land increased by 5%. 22883. (HELI: atpl, cpl) For a flight to an offshore platform, an alternate aerodrome is compulsory, except if: 1) flight duration does not exceed two hours 2) during the period from two hours before to two hours after the estimated landing time, the forecast conditions of ceiling and visibility are not less than one and a half times the applicable minima 3) the platform is available and no other flight either from or to the platform is expected between the estimated time of departure and one half hour after the estimated landing time #A) 1, 2, 3 B) 1, 2 C) 1, 3 D) 2, 3 88 © 2008 AVIATIONEXAM.com PICTURE SUPLEMENTS 90 © 2008 AVIATIONEXAM.com 033 PICTURE SUPPLEMENTS 91 © 2008 AVIATIONEXAM.com Time, Fuel and Distance to Climb 0 10 20 30 40 TIME TO CLIMB - MINUTES -50 -40 -30 -20 -10 0 10 20 30 40 50 60 OUTSIDE AIR TEMPERATURE°C FUEL TO CLIMB - GALLONS 0 1 2 3 4 5 6 7 8 9 10 11 DISTANCE TO CLIMB - NAUTICAL MILES 0 10 20 30 40 50 60 70 80 ISA 16,000 14,000 12,000 10,000 8000 6000 4000
2000 PRESSUREALTITUDEFEET SL 3650 3400 3000 2600 INITIAL MASS - LB POWER............................FULL THROTTLE, 2500 RPM FUEL DENSITY................6.0 LB/GALL MIXTURE.........................FULL RICH COWL FLAPS..................AS REQUIRED ASSOCIATED CONDITIONS: EXAMPLE: OAT AT TAKE-OFF...............................15°C OAT AT CRUISE..................................-5°C AIRPORT PRESSURE ALTITUDE......5653 FT CRUISE PRESSURE ALTITUDE........11,500 FT INITIAL CLIMB MASS.........................3650 LB TIME TO CLIMB (18 - 6.5)..................11.5 MIN FUEL TO CLIMB 6.0 - 2.5)..................3.5 GAL DISTANCE TO CLIMB (36 - 12.5).......23.5 NM CLIMB SPEED 110 KT ALL WEIGHTS FIGURE 033-01 033 PICTURE SUPPLEMENTS 92 © 2008 AVIATIONEXAM.com Table 2.2.2 25.0 in. Hg (or full throttle) @ 2,100 rpm Off-peak EGT Cruise lean mixture @ cruise weight 3,400 lb Recommended Cruise Power Settings (continued) NOTE 1: Full-throttle manifold pressure settings are approximate. NOTE 2: Shaded areas represent operation with full throttle. NOTE 3: Fuel ows are to be used for ight planning. Lean using the EGT. ISA Dev. Press. Alt. IOAT Man. Press. Fuel Flow Airspeed oC Feet oC oF In. Hg PPH GPH KIAS KTAS 0 -3 26 25.0 63.8 10.6 148 140 2,000 -7 19 25.0 66.4 11.1 149 145 4,000 -11 12 25.0 68.9 11.5 149 150 -20 6,000 -15 5 24.3 68.3 11.4 147 152 8,000 -19 -2 22.5 63.9 10.7 139 148 10,000 -23 -9 20.8 60.1 10.0 132 144 12,000 -27 -17 19.3 56.7 9.5 123 139 14,000 -31 -24 17.9 54.5 9.1 113 132 16,000 -35 -32 16.5 52.2 8.7 95 114 0 17 62 25.0 61.9 10.3 143 140 2,000 13 55 25.0 64.2 10.7 143 145 4,000 9 48 25.0 66.6 11.1 144 150 0 6,000 5 41 24.3 66.1 11.0 141 152 8,000 1 34 22.5 61.9 10.3 134 148 10,000 -3 27 20.8 58.5 9.8 126 143
12,000 -7 19 19.3 55.6 9.3 116 136 14,000 -11 12 17.9 53.5 8.9 103 125 16,000 - - - - - - 0 37 98 25.0 60.1 10.0 138 140 2,000 33 91 25.0 62.1 10.4 138 145 4,000 29 84 25.0 64.4 10.7 139 150 +20 6,000 25 77 24.3 63.9 10.7 136 151 8,000 21 70 22.5 60.2 10.0 128 147 10,000 17 63 20.8 56.8 9.5 119 141 12,000 13 55 19.3 54.5 9.1 108 131 14,000 - - - - - - 16,000 - - - - - - FIGURE 033-02 033 PICTURE SUPPLEMENTS 93 © 2008 AVIATIONEXAM.com Table 2.2.3 23.0 in. Hg (or full throttle) @ 2,300 rpm Off-peak EGT Cruise lean mixture @ cruise weight 3,400 lb Recommended Cruise Power Settings (continued) NOTE 1: Full-throttle manifold pressure settings are approximate. NOTE 2: Shaded areas represent operation with full throttle. NOTE 3: Fuel ows are to be used for ight planning. Lean using the EGT. ISA Dev. Press. Alt. IOAT Man. Press. Fuel Flow Airspeed oC Feet oC oF In. Hg PPH GPH KIAS KTAS 0 -3 26 23.0 67.6 11.3 152 144 2,000 -7 20 23.0 69.7 11.6 152 149 4,000 -11 13 23.0 72.1 12.0 153 154 -20 6,000 -15 6 23.0 74.4 12.4 153 158 8,000 -18 -1 22.4 73.8 12.3 150 160 10,000 -23 -9 20.7 68.4 11.4 143 157 12,000 -27 -16 19.2 63.8 10.6 135 153 14,000 -31 -23 17.8 60.0 10.0 127 148 16,000 -35 -31 16.4 56.3 9.4 117 141 0 17 62 23.0 65.4 10.9 147 145 2,000 13 56 23.0 67.4 11.2 147 149 4,000 9 49 23.0 69.4 11.6 148 154 0 6,000 5 42 23.0 71.7 12.0 148 159 8,000 2 35 22.4 71.1 11.9 145 160 10,000 -3 27 20.7 66.2 11.0 137 157 12,000 -7 20 19.2 61.8 10.3 129 152 14,000 -11 13 17.8 58.5 9.8 120 146 16,000 -15 5 16.4 55.3 9.2 109 137 0 37 98 23.0 63.2 10.5 142 145 2,000 33 92 23.0 65.1 10.9 143 149 4,000 29 85 23.0 67.1 11.2 143 154 +20 6,000 25 78 23.0 69.0 11.5 142 158 8,000 22 71 22.4 68.5 11.4 140 160 10,000 17 63 20.7 64.0 10.7 132 156 12,000 13 56 19.2 60.0 10.0 123 151 14,000 9 48 17.8 57.1 9.5 113 142 16,000 - - - - - - -
FIGURE 033-03 033 PICTURE SUPPLEMENTS 94 © 2008 AVIATIONEXAM.com Range SL 1000 2000 3000 4000 5000 6000 7000 8000 9000 10,000 11,000 12,000 13,000 14,000 620 640 660 680 700 720 740 760 780 800 820 840 860 880 900 920 RANGE - NAUTICAL MILES NOTE: RANGE INCLUDES CRUISE CLIMB & ALLOWS FOR TAXI, RUNUP, & 45 MINUTES RESERVE FUEL AT ECONOMY CRUISE POWER FULL THROTTLE 2500 RPM FULL THROTTLE 2100 RPM 21 IN HG / 2100 RPM FULL THROTTLE 2300 RPM 23 IN HG / 2300 RPM 25 IN HG / 2100 RPM ASSOCIATED CONDITIONS: MASS....................................... FUEL........................................ FUEL DENSITY........................ INITIAL FUEL LOAD................. TAKE-OFF ALTITUDE.............. WIND........................................ 3663 LB BEFORE ENGINE START AVIATION GASOLINE 6.0 LB/GAL 74 U.S. GAL (444 LB)
SEA LEVEL ZERO EXAMPLE: CRUISE ALTITUDE.............11,500 FT POWER SETTING..............FULL THROTTLE 2500 RPM RANGE...............................866 NM 20°C LEAN of PEAK EGT 162 152 160 148 140 129 150 154 169 170 25 IN HG / 2500 RPM TAS - kt ISA FIGURE 033-04 033 PICTURE SUPPLEMENTS 95 © 2008 AVIATIONEXAM.com Endurance FULL THROTTLE 2500 RPM FULL THROTTLE 2300 RPM FULL THROTTLE 2100 RPM 25 IN HG / 2100 RPM 21 IN HG / 2100 RPM 23 IN HG / 2300 RPM 25 IN HG / 2500 RPM SL 1000 2000 3000 4000 5000 6000 7000 8000 9000 10,000 11,000 12,000 13,000 14,000 PRESSURE ALTITUDE - FEET 3.0 3.5 4.0 4.5 5.0 5.5 6.0 6.5 7.0 7.5 8.0 ENDURANCE - HOURS NOTE: ENDURANCE INCLUDES CRUISE CLIMB & ALLOWS FOR TAXI, RUNUP, & 45 MINUTES RESERVE FUEL AT ECONOMY CRUISE POWER ASSOCIATED CONDITIONS: MASS............................... FUEL................................ FUEL DENSITY................ INITIAL FUEL LOAD........ TAKE-OFF ALTITUDE...... WIND................................ 3663 LB BEFORE ENGINE START AVIATION GASOLINE 6.0 LB/GAL
74 U.S. GAL (444 LB) SEA LEVEL ZERO EXAMPLE: CRUISE ALTITUDE....11,500 FT POWER SETTING......FULL THROTTLE 2500 RPM ENDURANCE.............5.4 HRS (5 HRS, 24 MINS) 20°C LEAN of PEAK EGT 150 129 140 148 154 170 169 160 162 152 TAS - kt ISA FIGURE 033-05 033 PICTURE SUPPLEMENTS 96 © 2008 AVIATIONEXAM.com Climb -40 -20 0 +20 +40 0 20 40 60 80 B M I L C O T E C N A T S I D & , E M I T , L E U F C ° E R U T A R E P M E T R I A E D I S T U O ASSOCIATED CONDITIONS: 4750 LB GEAR UP COWL FLAPS CLOSED 2600 RPM & 33 IN. HG. or FULL THROTTLE MIXTURE FULL RICH EXAMPLE: DEPARTURE AIRPORT ALTITUDE.............2000 ft DEAPARTURE AIRPORT OAT.....................21°C CRUISE ALTITUDE......................................16,500 ft CRUISE OAT................................................-13°C FUEL TO CLIMB...........................................15 - 2 = 13 gal TIME TO CLIMB...........................................27 - 3 = 24 min DISTANCE TO CLIMB..................................50 - 5 = 45 NM 18,000 8,000 16,000 14,000 12,000 10,000 6,000 4,000 2,000 SEA LEVEL PRESSURE ALTITUDE - FT ISA TEMP DEPARTURE FUEL gal TIME min DISTANCE NM CRUISE CLIMB SPEED 120 kt IAS FIGURE 033-06 033 PICTURE SUPPLEMENTS 97
© 2008 AVIATIONEXAM.com Range ASSOCIATED CONDITIONS: USABLE FUEL 123 gal 4750 lb AIRCRAFT CLEAN COWL FLAPS CLOSED CLIMB AT MAX. CONTINUOUS POWER DESCENT AT 1000 fpm & 145 kt IAS, NO WIND 4.2 gal FUEL FOR START, TAXI & TAKE-OFF EXAMPLE: CRUISE ALTITUDE.....................16,500 ft POWER.......................................45% RANGE WITH RESERVE............942 NM RANGE WITH NO RESERVE.....1060 NM NOTE: RANGE INCLUDES CLIMB & DESCENT DISTANCES RANGE INCREASES APPROX 1 NM FOR EACH °C ABOVE ISA & DECREASES 1 NM FOR EACH °C BELOW ISA 75% % POWER, MIXTURE LEANED 75% 65% 45% HIGH SPEED ECONOMY LONG RANGE 65% 55% 45% 75% 65% 55% 45% 500 600 700 800 900 1000 700 800 900 1000 1100 RANGE - NM WITH 45 MIN. RESERVE AT 45% POWER RANGE - NM WITH NO RESERVE 5000 10,000 15,000 20,000 25,000 ALTITUDE ft FIGURE 033-07 033 PICTURE SUPPLEMENTS 98 © 2008 AVIATIONEXAM.com Enter the Power Setting table (Figure 3.3) at the cruise Pressure Altitude and t ravel horizontally right to the block appropriate to the power setting. At the top of the block read the fuel ow in US gallons per hour. In the same block select the column appropriate to the RPM and at the cruise Pressure Altitude read the manifold pressure. These tables are for ISA deviation 0°C. To maintain constant power at temperature
deviations other than 0° the manifold pressure must be corrected by adding 1% for each 6°C above the standard temperature or by subtracting 1% for each 6°C below the standard temperature. The Cruise Manifold Pressure must not exceed 34 inches. Power Setting Table % 5 4 % 5 5 % 5 6 % 5 7 R E W O P FUEL FLOW H P G 0 . 6 1 H P G 7 . 8 1 H P G 3 . 3 2 H P G 0 . 9 2 RPM 2,500 2,600 2,400 2,500 2,600 2,100 2,200 2,300 2,400 2,500 2,600 2,100 2,20 0 2,300 2,400 2,500 2,600 PRESS ALT (ft) ISA 0oC MANIFOLD ABSOLUTE PRESSURE (Hg in) (MAP) 0 15 34.0 33.0 33.8 32.0 31.0 31.2 30.3 29.4 28.2 27.2 26.3 27.1 26.4 25.5 24.3 23.3 22.5 2,000 11 33.8 32.7 33.2 31.7 30.7 30.5 29.7 28.8 27.8 26.8 26.0 26.4 25.8 24.6 2 3.7 22.8 22.1 4,000 7 33.6 32.4 32.8 31.5 30.5 30.0 29.2 28.3 27.4 26.4 25.6 25.8 25.0 24.0 23 .2 22.3 21.8 6,000 3 33.4 32.2 32.5 31.2 30.3 29.7 28.8 28.0 27.0 26.2 25.3 25.3 24.5 23.5 22 .8 21.9 21.5 8,000 -1 33.1 32.0 32.3 31.0 30.1 29.4 28.4 27.7 26.8 25.7 25.0 24.8 24.0 23.0 2 2.4 21.6 21.2 10,000 -5 33.0 31.9 32.0 30.9 30.0 - 28.3 27.5 26.5 25.5 24.7 24.4 23.7 22.8 22. 0 21.4 21.0 12,000 -9 32.5 31.8 31.8 30.7 29.8 - 28.3 27.2 26.3 25.3 24.6 24.0 23.3 22.5 21. 7 21.2 20.9 14,000 -13 - 31.7 - 30.5 29.7 - - 27.1 26.1 25.2 24.4 - 23.0 22.3 21.4 21.1 20.8 16,000 -17 - 31.6 - 30.4 29.5 - - - 25.9 25.0 24.3 - - 22.0 21.3 21.0 20.6 18,000 -21 - - - - 29.4 - - - - 25.0 24.2 - - - 21.2 20.9 20.5 20,000 -25 - - - - 29.3 - - - - - 24.2 - - - 21.2 20.8 20.4 22,000 -28 - - - - - - - - - - 24.1 - - - - - 20.4 F ° 0 5 6 , 1 F ° 5 2 5 , 1 T G E X A M 24,000 -33 - - - - - - - - - - - - - - - - 20.4 25,000 -34 - - - - - - - - - - - - - - - - 20.4 FIGURE 033-08 033 PICTURE SUPPLEMENTS 99 © 2008 AVIATIONEXAM.com Speed v Power 8,000 OUTSIDE AIR TEMPERATURE °C TRUE AIRSPEED - kt -20 -40 0 +20 +40 120 140 160 180 200 14,000 16,000 12,000 10,000 6,000 4,000 2,000 SEA LEVEL 18,000
20,000 22,000 24,000 PRESS. ALT - ft 75% 65% 45% HIGH SPEED ECONOMY LONG RANGE EXAMPLE: OAT...................................13 °C PRESSURE ALTITUDE....16,500 ft POWER.............................55% TRUE AIRSPEED..............172 kt ASSOCIATED CONDITIONS: MIXTURE FULL RICH ABOVE 75% POWER MIXTURE LEANED IN ACCORDANCE WITH SECTION 4.37 COWL FLAPS CLOSED AIRCRAFT CLEAN MID CRUISE MASS (4450 lb) 75% 65% 55% 45% 100% ISA TEMP FIGURE 033-09 033 PICTURE SUPPLEMENTS 100 © 2008 AVIATIONEXAM.com Endurance FIGURE 033-10 033 PICTURE SUPPLEMENTS 101 © 2008 AVIATIONEXAM.com Fuel, Time and Distance to Descend -40 -30 -20 -10 0 +10 +20 +30 +40 0 10 20 30 40 50 60 70 80 OUTSIDE AIR TEMPERATURE °C FUEL, TIME & DISTANCE TO DESCEND DESTINATION CRUISE SEA LEVEL ISA TEMP FUEL gal TIME min DISTANCE NM 18,000 8,000 16,000 14,000 12,000 10,000 6,000 4,000 000,2 PRESSURE ALTITUDE - ft 22,000
20,000 ASSOCIATED CONDITIONS: 145 kt IAS 1000 FPM DESCENT AIRCRAFT CLEAN NO WIND EXAMPLE: CRUISE ALTITUDE..................16,500 ft CRUISE OAT............................-13°C DESTINATION ALT...................3000 ft DESTINATION OAT..................22°C FUEL TO DESCEND................6 - 1 = 5 gal TIME TO DESCEND................16 - 3 = 13 min DISTANCE TO DESCEND.......45 - 8 = 37 NM SOLUTION: FIGURE 033-11 033 PICTURE SUPPLEMENTS 102 © 2008 AVIATIONEXAM.com Optimum Altitude Off-Optimum Condition Fuel Mileage Penalty % LRC or Mach 0.74 Mach 0.78 2,000 ft above -1 -1 Optimum 0 0 2,000 ft below -1 -2 4,000 ft below -4 -4 8,000 ft below -10 -11 12,000 ft below -15 -20 Off-Optimum Fuel Penalty FIGURE 033-12 033 PICTURE SUPPLEMENTS 103 © 2008 AVIATIONEXAM.com Short Distance Cruise Altitude PRESSURE ALTITUDE 1000 ft 10 20 30 40 45 50 55 60 65 70 40 BRAKE RELEASE WEIGHT 1000 kg 35 TRIP DISTANCE NM 100 200 300 REF LINE ISA + 20°C ISA + 10°C & BELOW FIGURE 033-13
033 PICTURE SUPPLEMENTS 104 © 2008 AVIATIONEXAM.com Simplied Flight Planning Trip Distances 200 NM to 1,200 NM 37 BASED ON: 280 / 0.74 CLIMB 0.74 / 250 DESCENT 30 40 50 60 10 2 3 4 5 6 7 8 9 FUEL REQUIRED 1000 kg 0 TRIP TIME hr 1 2 3 4 20 10 0 -10 ISA DEV °C 100 0 100 HEAD TAIL WIND kt 200 400 600 800 1000 1200 TRIP DISTANCE NM LANDING WEIGHT 1000 kg PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft 37 33 29 2522 18 14 10 29 & ABOVE 10 REF LINE 22 REF LINE REF LINE LONG RANGE CRUISE 50 50 FIGURE 033-14
033 PICTURE SUPPLEMENTS 105 © 2008 AVIATIONEXAM.com Simplied Flight Planning Trip Distances 1,000 NM to 3,000 NM TRIP DISTANCE NM 30 40 50 60 LANDING WEIGHT 1000 kg 100 100 HEAD TAIL WIND kt 50 50 0 1000 1500 2000 2500 3000 TRIP TIME hr 20 10 0 -10 ISA DEV °C 2 3 4 5 6 7 BASED ON: 280 / 0.74 CLIMB 0.74 / 250 DESCENT FUEL REQUIRED 1000 kg 6 10 14 18 22 26 PRESSURE ALTITUDE 1000 ft REF LINE REF LINE REF LINE PRESSURE ALTITUDE 1000 FT 29 & ABOVE 10 22 373329 2522 18 14 10 PRESSURE ALTITUDE 1000 ft 37 10 LONG RANGE CRUISE FIGURE 033-15 033 PICTURE SUPPLEMENTS
106 © 2008 AVIATIONEXAM.com Simplied Flight Planning Trip Distances 100 NM to 600 NM 100 0 TRIP DISTANCE NAUTICAL NM 30 40 50 60 LANDING WEIGHT 1000 kg 100 100 HEAD TAIL WIND kt 50 50 200 300 400 500 600 BASED ON: 280 / 0.74 CLIMB 0.74 / 250 DESCENT TRIP TIME hr 20 10 0 -10 ISA DEV °C 1 2 0 PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft 35 & ABOVE 33 312927 25 23 21 REF LINE REF LINE 37 35 & ABOVE 21 1500 2000 2500 3000 3500 4000 4500 FUEL REQUIRED kg REF LINE 21 0.74 MACH CRUISE FIGURE 033-16 033 PICTURE SUPPLEMENTS 107 © 2008 AVIATIONEXAM.com
Simplied Flight Planning Trip Distances 100 NM to 600 NM 100 0 TRIP DISTANCE NM 30 40 50 60 LANDING WEIGHT 1000 kg 100 100 HEAD TAIL WIND kt 50 50 200 300 400 500 600 BASED ON: 280 / 0.74 CLIMB 0.74 / 250 DESCENT TRIP TIME hr 20 10 0 -10 ISA DEV °C 1 2 0 PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft 35 & ABOVE 3331 2927 25 REF LINE REF LINE 37 35 & ABOVE 25 1500 2000 2500 3000 3500 4000 4500 FUEL REQUIRED kg REF LINE 25 0.78 MACH CRUISE FIGURE 033-17 033 PICTURE SUPPLEMENTS 108 © 2008 AVIATIONEXAM.com Simplied Flight Planning REF LINE PRESSURE ALTITUDE 1000 ft
Trip Distances 1,000 NM to 3,000 NM
33 & ABOVE BASED ON: 280 / 0.74 CLIMB 0.74 / 250 DESCENT 30 40 50 60 TRIP TIME hr 2 3 4 20 10 0 -10 ISA DEV °C 100 0 100 HEAD TAIL WIND kt 1000 1500 2000 2500 3000 TRIP DISTANCE NM LANDING WEIGHT 1000 kg 50 50 5 6 7 31 33 & ABOVE 25 6 8 10 12 14 16 18 20 FUEL REQUIRED 1000 kg 22 0.78 MACH CRUISE REF LINE REF LINE PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft 25 2729 31 25 37 FIGURE 033-18 033 PICTURE SUPPLEMENTS 109 © 2008 AVIATIONEXAM.com Step Climb Simplied Fuel Planning This chart allows the planner to optimise aeroplane performance by increasing th e cruise altitude in 4000 ft steps in order to allow for the increase in optimum altitude
as aeroplane weight decreases. The graph is valid for altitudes with Step Climb of 4,000 ft to 2,000 ft above opt imum altitude. The graph provides trip fuel and time, at LRC or 0.74 M, from brake re lease to touchdown. The method of use is the same as that for the constant altitude chart s except that the argument of Brake Release Weight is used in place of Cruise Pressure Altit ude - see example on chart. Simplied Flight Planning Trip Distances 1,000 NM to 4,000 NM REF LINE TRIP TIME hr 3 4 20 10 0 -10 ISA DEV °C 100 0 HEAD WIND kt 1000 1500 2000 2500 3000 TRIP DISTANCE NM 50 50 5 6 7 10 15 20 25 FUEL REQUIRED 1000 kg 2 8 9 10 100 TAIL 3500 4000 5 VALID FOR ALL PRESSURE ALTITUDES WITH 4000 ft STEP CLIMB TO 2000 ft ABOVE OPTIMUM ALTITUDE STEPPED CLIMB CRUISE 70 65 60 55 45 50 BRAKE RELEASE WEIGHT 1000 kg ALL BRAKE RELEASE WEIGHTS REF LINE FIGURE 033-19 033 PICTURE SUPPLEMENTS 110 © 2008 AVIATIONEXAM.com Simplied Flight Planning
Alternate Distances to 500 NM
0 1 2 3 4 5 ALTERNATE FUEL 1000 kg TIME TO ALTERNATE hr 1.4 1.2 1.0 0.8 0.6 0.4 0.2 0 100 0 HEAD WIND kt 50 50 100 TAIL 0 100 200 300 400 500 DISTANCE TO ALTERNATE NM REF LINE ALTERNATE PLANNING LONG RANGE CRUISE LANDING WEIGHT AT ALTERNATE 1000 kg ALL LANDING WEIGHTS 70 65 6055 4550 4035 FIGURE 033-20 033 PICTURE SUPPLEMENTS 111 © 2008 AVIATIONEXAM.com Holding Fuel Planning The table below provides fuel ow values for various hold entry weights and holdin g pressure altitudes to facilitate the calculation of the holding reserve fuel req uirements for ight planning. Calculation Procedure a) Enter Figure 4.4 with the Pressure Altitude at which the hold is planned and the weight at the start of the hold, interpolating as required. b) Extract the holding fuel ow in kg per hour. c) The fuel ow is based on a racetrack pattern at the minimum drag KIAS. The minimum speed that is permitted to be own is 210 KIAS. d) If the hold is to be conducted in straight and level ight, reduce the fuel ow b y 5%. Press Alt. ft
Weight x 1,000 kg 66 64 62 60 58 56 54 52 50 48 46 44 42 40 38 FUEL FLOW in kg per hour 0 8 6 , 1 0 4 7 , 1 0 0 8 , 1 0 0 9 , 1 0 8 9 , 1 0 8 0 , 2 0 6 1 , 2 0 6 2 , 2 0 0 4 , 2 0 4 5 , 2 0 4 7 , 2 0 0 0 , 7 3 35,000 3,020 2,820 2,660 2,520 2,420 2,320 2,220 2,140 2,060 1,960 1,880 1,800 1 ,720 1,660 30,000 2,840 2,740 2,660 2,560 2,480 2,400 2,300 2,220 2,140 2,060 1,960 1,880 1 ,800 1,740 1,680 25,000 2,840 2,760 2,660 2,580 2,500 2,420 2,320 2,240 2,160 2,080 2,000 1,920 1 ,840 1,780 1,720 20,000 2,840 2,760 2,680 2,580 2,500 2,420 2,340 2,260 2,180 2,100 2,020 1,940 1 ,860 1,800 1,760 15,000 2,880 2,800 2,700 2,620 2,540 2,460 2,380 2,300 2,220 2,140 2,060 1,980 1 ,920 1,860 1,800 10,000 2,920 2,820 2,740 2,660 2,580 2,500 2,420 2,340 2,260 2,180 2,100 2,020 1 ,980 1,920 1,880 5,000 2,960 2,860 2,780 2,700 2,620 2,540 2,460 2,380 2,300 2,220 2,140 2,080 2, 020 1,960 1,920 1,500 3,000 2,900 2,820 2,740 2,660 2,580 2,520 2,440 2,360 2,280 2,220 2,140 2, 080 2,020 1,980 Holding Fuel Flow Flaps Retracted FIGURE 033-21 033 PICTURE SUPPLEMENTS 112 © 2008 AVIATIONEXAM.com ISA -6°C TO -15°C Press. Alt. ft Units Min/kg. NAM/Kt BRAKE RELEASE WEIGHT KG 68000 66000 64000 62000 60000 58000 56000 52000 48000 44000 40000 0 5 9 / 2 1 0 5 0 1 / 3 1 0 0 2 1 / 5 1 0 5 3 1 / 7 1 0 5 5 1 / 0 2 0 5 6 1 / 2 2 0 0 8 1 / 5 2 0 0 1 2 / 0 3 l e u F / e mi T 0 0 0 7 3 7 7 3 / 4 6 8 7 3 / 3 7 9 7 3 / 5 8 1 8 3 / 8 9 3 8 3 / 7 1 1 5 8 3 / 0 3 1 7 8 3 / 8 4 1 1 9 3 / 4 8 1 S A T / t s i D 0 0 9 / 1 1 0 0 1 1 / 3 1 0 5 1 1 / 4 1 0 0 3 1 / 6 1 0 5 4 1 / 9 1 0 5 5 1 / 0 2 0 5 6 1 / 2 2 0 0 8 1 / 4 2 0 5 0 2 / 8 2 l e u F / e mi T 0 0 0 6 3 5 7 3 / 0 6 6 7 3 / 9 6 7 7 3 / 9 7 8 7 3 / 1 9 0 8 3 / 6 0 1 1 8 3 / 5 1 1 3 8 3 / 7 2 1 5 8 3 / 2 4 1 8 8 3 / 6 6 1 S A T / t s i D 35000 Time/Fuel 32/2350 27/2000 24/1850 22/1700 20/1600 19/1500 17/1400 15/1250 13/1100 12/1000 11/900 Dist/TAS 195/390 156/385 139/383 125/381 114/380 105/378 97/377 85/376 74/375 65 /374 57/373 34000 Time/Fuel 26/2000 23/1850 21/1700 20/1600 19/1500 17/1400 16/1350 14/1200 13/1100 11/950 10/850 Dist/TAS 152/383 136/381 123/379 113/378 105/376 97/375 90/375 79/373 70/372 61/ 371 54/371 33000 Time/Fuel 23/1850 21/1750 20/1650 19/1550 17/1450 16/1350 15/1300 14/1150 12/1050 11/950 10/850 Dist/TAS 133/378 121/376 112/375 104/374 97/373 90/372 84/372 74/371 66/370 58/3 69 51/368 32000 Time/Fuel 21/1750 20/1650 19/1550 17/1500 16/1400 16/1300 15/1250 13/1150 12/1000 11/900 9/800 Dist/TAS 120/374 111/373 103/372 96/371 90/370 84/369 79/369 70/368 62/367 55/36
6 48/366 31000 Time/Fuel 20/1700 19/1600 18/1500 17/1400 16/1350 15/1300 14/1200 13/1100 11/1000 10/900 9/800 Dist/TAS 110/370 102/369 95/368 89/367 84/367 79/366 74/366 66/365 58/364 52/364 46/363 30000 Time/Fuel 19/1600 18/1550 17/1450 16/1350 15/1300 14/1250 13/1200 12/1050 11/950 10/850 9/800 Dist/TAS 101/366 95/365 89/1364 83/364 78/363 74/363 70/362 62/362 55/361 49/361 43/360 29000 Time/Fuel 17/1550 16/1450 16/1400 15/1300 14/1250 13/1200 13/1150 11/1050 10/950 9/850 8/750 Dist/TAS 92/361 87/360 81/360 77/359 72/359 68/358 64/358 57/357 51/357 46/357 4 1/356 28000 Time/Fuel 16/1450 15/1400 15/1300 14/1250 13/1200 13/1150 12/1100 11/1000 10/900 9/800 8/750 Dist/TAS 84/356 79/356 75/355 70/355 67/355 63/354 59/354 53/353 48/353 42/353 3 8/352 27000 Time/Fuel 15/1400 14/1350 14/1250 13/1200 12/1150 12/1100 11/1050 10/950 9 /850 8/800 8/700 Dist/TAS 77/352 73/351 69/351 65/351 61/350 58/350 55/1350 49/349 44/349 39/349 35/348 26000 Time/Fuel 14/1350 14/1250 13/1200 12/1150 12/1100 11/1050 11/1000 10/900 9 /850 8/750 7/700 Dist/TAS 71/348 67/347 63/347 60/347 57/347 54/346 51/346 46/346 41/345 37/345 3 3/345 25000 Time/Fuel 13/1300 13/1200 12/1150 12/1100 11/1050 11/1000 10/950 9/900 8/8 00 8/750 7/650 Dist/TAS 65/344 61/343 58/343 55/343 52/343 50/343 47/342 42/342 38/342 34/342 3 0/341 24000 Time/Fuel 13/1200 12/1150 11/1100 11/1050 10/1000 10/950 10/950 9/850 8 / 750 7/700 6/650 Dist/TAS 60/340 56/340 54/340 51/339 48/339 46/339 43/339 39/339 35/338 32/338 2 8/338 23000 Time/Fuel 12/1150 11/1100 11/1050 10/1000 10/1000 9 / 950 9/900 8/800 7/75 0 7/700 6/600 Dist/TAS 55/336 52/336 49/336 47/336 44/336 42/335 40/335 36/335 33/335 29/335 2 6/335 22000 Time/Fuel 11/1100 11/1050 10/1000 10/1000 9/950 9/900 9/850 8/800 7/700 6/ 650 6/600 Dist/TAS 50/333 48/333 45/333 43/332 41/332 39/332 37/332 33/332 30/332 27/332 2 4/331 21000 Time/Fuel 10/1050 10/1000 10/1000 9/950 9/900 8/850 8/800 7/750 7/700 6/65 0 6/550 Dist/TAS 46/330 44/329 42/329 40/329 38/329 36/329 34/329 31/329 28/328 25/328 2 2/328 20000 Time/Fuel 10/1000 9/950 9/950 9/900 8/850 8/800 8/800 7/700 6/650 6/600 5/ 550 Dist/TAS 42/326 40/326 38/326 36/326 35/326 33/326 31/326 28/326 26/325 23/325 2 1/325 19000 Time/fuel 9/950 9/950 8/900 8/850 8/800 7/800 7/750 7/700 6/650 6/600 5/50 0 Dist/TAS 39/323 37/323 35/323 33/323 32/323 30/323 29/323 26/323 24/322 21/322 1 9/322 18000 Time/Fuel 9/900 8/900 8/850 8/800 7/800 7/750 7/700 6/650 6/600 5/550 5/50 0 Dist/TAS 35/320 34/320 32/320 31/320 29/320 28/320 26/320 24/320 22/320 19/319 1 7/319 17000 Time/Fuel 8/900 8/850 8/800 7/800 7/750 7/700 6/700 6/650 5/600 5/550 5/50 0 Dist/TAS 32/317 31/317 29/317 28/317 27/317 25/317 24/317 22/317 20/317 18/317 1
6/317 16000 Time/Fuel 8/850 7/800 7/750 7/750 7/700 6/700 6/650 6/600 5/550 5/500 4/45 0 Dist/TAS 29/314 28/314 27/314 25/314 24/314 23/314 22/314 20/314 18/314 16/314 1 5/314 15000 Time/Fuel 7/800 7/750 7/750 6/700 6/700 6/650 6/650 5/600 5/550 4/500 4/45 0 Dist/TAS 26/312 25/312 24/312 23/311 22/311 21/311 20/311 18/311 16/311 15/311 1 3/311 14000 Time/Fuel 7/750 6/700 6/700 6/650 6/650 6/600 5/600 5/550 5/500 4/450 4/40 0 Dist/TAS 24/309 23/309 22/309 21/309 20/309 19/309 18/309 16/309 15/309 13/309 1 2/309 13000 Time/Fuel 6/700 6/700 6/650 6/650 5/600 5/600 5/550 5/500 4/500 4/450 4/40 0 Dist/TAS 21/306 20/306 19/306 19/306 18/306 17/306 16/306 15/306 13/306 12/306 1 1/306 12000 Time/Fuel 6/650 6/650 5/600 5/600 5/600 5/550 5/550 4/500 4/450 4/400 3/40 0 Dist/TAS 19/304 18/304 17/304 17/304 16/304 15/304 14/304 13/304 12/304 11/304 1 0/304 11000 Time/Fuel 5/650 5/600 5/600 5/550 5/550 5/500 4/500 4/450 4/450 3/400 3/35 0 Dist/TAS 17/301 16/301 15/301 15/301 14/301 13/301 13/301 12/301 11/301 10/301 9 /301 10000 Time/Fuel 5/600 5/550 5/550 5/550 4/500 4/500 4/500 4/450 4/400 3/350 3/35 0 Dist/TAS 15/299 14/299 13/299 13/299 12/299 12/299 11/299 10/299 9/299 8/299 7/2 99 8000 Time/Fuel 4/500 4/500 4/500 4/450 4/450 4/450 3/400 3/400 3/350 3/350 3/300 Dist/TAS 11/294 10/294 10/294 9/294 9/294 9/294 8/294 7/294 7/294 6/294 6/294 6000 Time/Fuel 4/450 3/400 3/400 3/400 3/400 3/350 3/350 3/350 3/300 2/300 2/250 Dist/TAS 7/290 7/290 6/290 6/290 6/290 6/290 5/290 5/290 5/290 4/290 4/290 1500 Time/Fuel 2/250 2/250 2/250 2/250 2/250 2/250 2/250 2/200 2/200 2/200 1/150 Fuel Adjustment for high elevation airports Effect on time and distance is negligible Fuel Adjustment -50 -100 -150 En-route Climb 280/.74 2000 4000 6000 8000 10000 12000 -250 -300 -350 Airport Elevation FIGURE 033-22 033 PICTURE SUPPLEMENTS 113 © 2008 AVIATIONEXAM.com ISA +6°C TO +15°C Press. Alt. ft Units Min/kg. NAM/Kt BRAKE RELEASE WEIGHT KG 68000 66000 64000 62000 60000 58000 56000 52000 48000 44000 40000 0 0 0 1 / 2 1 0 5 1 1 / 4 1 0 0 3 1 / 6 1 0 0 5 1 / 8 1 0 0 7 1 / 2 2 0 5 8 1 / 4 2 0 0 0 2 / 7 2 0 5 3 2 / 3 3 l e u F / e mi T 0 0 0 7 3
3 9 3 / 2 7 4 9 3 / 2 8 6 9 3 / 5 9 7 9 3 / 1 1 1 0 0 4 / 2 3 1 2 0 4 / 7 4 1 4 0 4 / 9 6 1 9 0 4 / 2 1 2 S A T / t s i D 0 0 0 1 / 2 1 0 0 1 1 / 3 1 0 5 2 1 / 5 1 0 0 4 1 / 7 1 0 0 6 1 / 0 2 0 0 7 1 / 1 2 0 5 6 1 / 3 2 0 0 0 2 / 6 2 0 5 2 2 / 0 3 l e u F / e mi T 0 0 0 6 3 1 9 3 / 8 6 2 9 3 / 7 7 3 9 3 / 9 8 5 9 3 / 2 0 1 7 9 3 / 9 1 1 8 9 3 / 0 3 1 0 0 4 / 3 4 1 2 0 4 / 1 6 1 5 0 4 / 9 8 1 S A T / t s i D 35000 Time/Fuel 35/2600 29/2250 26/2050 23/1900 21/1750 20/1650 19/1550 16/1350 14/1200 13/1100 11/950 Dist/TAS 224/407 180/402 157/399 141/397 129/396 119/395 110/394 95/392 83/391 7 3/390 64/389 34000 Time/Fuel 28/2250 25/2050 23/1900 21/1800 20/1650 19/1550 18/1500 16/1300 14/1200 12/1050 11/950 Dist/TAS 173/400 154/397 140/395 128/394 118/393 110/392 102/391 89/389 78/388 6 9/387 61/386 33000 Time/Fuel 25/2100 23/1950 21/1800 20/1700 19/1600 18/1500 17/1450 15/1300 13/1150 12/1050 10/900 Dist/TAS 151/394 138/393 127/391 118/390 109/389 102/388 95/388 84/386 74/385 65 /385 58/384 32000 Time/Fuel 23/1950 21/1850 20/1750 19/1650 18/1550 17/1450 16/1400 14/1250 13/1100 11/1000 10/900 Dist/TAS 136/390 126/389 117/388 109/387 102/386 95/385 89/384 79/383 70/383 62/ 382 55/381 31000 Time/Fuel 22/1850 20/1750 19/1650 18/1550 17/1500 16/1400 15/1350 13/1200 12/1100 11/1000 10/900 Dist/TAS 125/386 116/385 108/384 101/383 95/382 89/382 84/381 74/380 66/380 59/3 79 52/378 30000 Time/Fuel 20/1800 19/1700 18/1600 17/1500 16/1450 15/1350 14/1300 13/1150 12/1050 10/950 9/850 Dist/TAS 115/382 108/381 101/380 .95/379 89/379 84/378 77/378 70/377 62/376 56/3 76 49/375 29000 Time/Fuel 19/1700 18/1600 17/1550 16/1450 15/1400 14/1300 14/1250 12/1150 11/1000 10/900 9/850 Dist/TAS 105/376 98/376 92/375 87/374 82/374 77/374 73/373 65/373 58/372 52/372 46/371 28000 Time/Fuel 17/1600 17/1550 16/1450 15/1400 14/1300 13/1250 13/1200 12/1100 10/1000 9/900 8/800 Dist/TAS 95/371 90/371 84/370 80/370 75/369 71/369 67/369 60/368 54/368 48/367 4 2/367 27000 Time/Fuel 16/1550 15/1450 15/1400 14/1350 13/1250 13/1200 12/1150 11/1050 10/950 9/850 8/750 Dist/TAS 87/366 82/366 77/366 73/365 69/365 66/365 62/364 56/364 50/363 44/363 3 9/363 26000 Time/Fuel 15/1450 15/1400 14/1350 13/1250 13/1200 12/1150 11/1100 10/1000 9/900 8/800 8/750 Dist/TAS 80/362 75/362 71/361 67/361 64/361 60/360 57/360 51/360 46/359 41/359 3 7/359 25000 Time/Fuel 14/1400 14/1350 13/1250 12/1200 12/1150 11/1100 11/1050 10/950 9 /850 8/800 7/700 Dist/TAS 73/356 69/357 65/357 62/'357 59/367 56/356 53/356 47/356 43/356 38/355 34/355 24000 Time/Fuel 13/1350 13/1250 12/1200 12/1150 11/1100 11/1050 10/1000 9/900 8/ 850 8/750 7/700 Dist/TAS 67/354 63/353 60/353 57/353 54/353 51/353 49/352 44/352 39/352 35/352 3 2/351 23000 Time/Fuel 13/1250 12/1200 11/1150 11/1100 10/1050 10/1000 10/950 9/900 8/8 00 7/750 7/650 Dist/TAS 61/350 58/350 55/349 53/349 50/349 47/349 45/349 41/348 37/348 33/348 2 9/348 22000 Time/Fuel 12/1200 11/1150 11/1100 10/1050 10/1000 9/950 9/950 8/850 8/750 7/700 6/650
Dist/TAS 56/346 54/346 51/346 48/346 46/345 44/345 42/345 37/345 34/345 30/345 2 7/344 21000 Time/Fuel 11/1150 11/1100 10/1050 10/1000 9/950 9/950 9/900 8/800 7/750 6/ 700 6/600 Dist/TAS 52/343 49/342 47/342 44/342 42/342 40/342 38/342 35/342 31/341 28/341 2 5/341 20000 Time/Fuel 10/1100 10/1050 10/1000 9/950 9/950 8/900 8/850 7/800 7/700 6/65 0 6/600 Dist/TAS 47/339 45/339 43/339 41/339 39/339 37/338 35/338 32/338 29/338 26/338 2 3/338 19000 Time/Fuel 10/1050 9/1000 9/950 9/950 8/900 8/850 8/800 7/750 6/700 6/600 5 /550 Dist/TAS 43/336 41/336 39/335 37/335 36/335 34/335 32/335 29/335 26/335 24/335 2 1/335 18000 Time/Fuel 9/1000 9/950 8/900 8/900 8/850 7/800 7/800 7/700 6/650 6/600 5/5 50 Dist/TAS 39/332 38/332 36/332 34/332 33/332 31/332 30/332 27/332 24/332 22/332 1 9/332 17000 Time/Fuel 9/950 8/900 8/900 8/850 7/800 7/750 7/750 6/700 6/600 5/550 5/50 0 Dist/TAS 36/329 34/329 33/329 31/329 30/329 28/329 27/329 24/329 22/329 20/329 1 8/329 16000 Time/Fuel 8/900 8/850 7/850 7/800 7/750 7/750 6/700 6/650 5/600 5/550 4/50 0 Dist/TAS 33/326 31/326 30/326 28/326 27/326 26/326 25/326 22/326 20/326 18/326 1 6/326 15000 Time/Fuel 8/850 7/800 7/800 7/750 6/750 6/700 6/650 5/600 5/550 5/500 4/45 0 Dist/TAS 29/323 28/323 27/323 26/323 24/323 23/323 22/323 20/323 18/323 16/323 1 5/323 14000 Time/Fuel 7/800 7/800 7/750 6/700 6/700 6/650 6/650 5/600 5/550 4/500 4/45 0 Dist/TAS 26/321 25/321 24/321 23/320 22/320 21/320 20/320 18/320 17/320 15/320 1 3/320 13000 Time/Fuel 7/750 6/750 6/700 6/700 6/650 5/650 5/600 5/550 4/500 4/450 4/45 0 Dist/TAS 24/318 23/318 22/318 21/318 20/318 19/318 18/318 16/318 15/318 13/318 1 2/318 12000 Time/Fuel 6/700 6/700 6/650 5/650 5/600 5/600 5/550 5/500 4/500 4/450 4/40 0 Dist/TAS 21/315 20/315 19/315 18/315 18/315 17/315 16/315 15/315 13/315 12/315 1 1/315 11000 Time/Fuel 6/650 5/650 5/600 5/600 5/600 5/550 5/550 4/500 4/450 4/400 3/40 0 Dist/TAS 19/313 18/313 17/313 16/313 16/313 15/312 14/312 13/312 12/312 11/312 9 /312 10000 Time/Fuel 5/600 5/600 5/600 5/550 5/550 4/500 4/500 4/450 4/450 3/400 3/35 0 Dist/TAS 16/310 16/310 15/310 14/310 14/310 13/310 12/310 11/310 10/310 9/310 8/ 310 8000 Time/Fuel 4/550 4/500 4/500 4/500 4/450 4/450 4/450 3/400 3/350 3/350 3/300 Dist/TAS 12/305 11/305 11/305 10/305 10/305 10/305 9/305 8/305 8/305 7/305 6/305 6000 Time/Fuel 4/450 4/450 3/400 3/400 3/400 3/400 3/350 3/350 3/300 2/300 2/250 Dist/TAS 8/301 8/301 7/301 7/301 7/301 6/301 6/301 6/301 5/301 5/301 4/301 1500 Time/Fuel 2/250 2/250 2/250 2/250 2/250 2/250 2/250 2/200 2/200 2/200 1/150 Fuel Adjustment for high elevation airports
Effect on time and distance is negligible Fuel Adjustment -50 -100 -200 En-route Climb 280/.74 6000 8000 10000 12000 2000 4000 -250 -300 -400 Airport Elevation FIGURE 033-23 033 PICTURE SUPPLEMENTS 114 © 2008 AVIATIONEXAM.com ISA +16°C TO +25°C Press. Alt. ft Units Min/kg. NAM/Kt BRAKE RELEASE WEIGHT KG 68000 66000 64000 62000 60000 58000 56000 52000 48000 44000 40000 0 5 1 1 / 5 1 0 0 3 1 / 7 1 0 5 4 1 / 9 1 0 5 6 1 / 2 2 0 5 9 1 / 7 2 0 5 1 2 / 1 3 0 5 5 2 / 7 3 l e u F / e mi T 0 0 0 7 3 2 0 4 / 8 8 3 0 4 / 1 0 1 5 0 4 / 8 1 1 7 0 4 / 0 4 1 0 1 4 / 2 7 1 3 1 4 / 8 9 1 7 1 4 / 6 4 2 S A T / t s i D 0 0 1 1 / 4 1 0 5 2 1 / 6 1 0 0 4 1 / 8 1 0 0 6 1 / 1 2 0 5 8 1 / 4 2 0 0 0 2 / 7 2 0 0 2 2 / 0 3 0 5 4 2 / 5 3 l e u F / e mi T 0 0 0 6 3 9 9 3 / 2 8 0 0 4 / 5 9 2 0 4 / 0 1 1 4 0 4 / 8 2 1 6 0 4 / 3 5 1 8 0 4 / 0 7 1 1 1 4 / 2 9 1 4 1 4 / 7 2 2 S A T / t s i D 35000 Time/Fuel 42/2950 34/2500 30/2200 27/2050 25/1900 23/1750 20/1550 17/1350 15/1200 13/1050 Dist/TAS 281/418 220/412 190/409 169/406 153/405 140/403 119/401 103/399 90/398 78/397 34000 Time/Fuel 40/2850 34/2500 30/2250 27/2100 25/1950 23/1800 21/1700 19/1500 16/1300 14/1150 13/1050 Dist/TAS 260/414 215/409 188/406 169/404 153/403 141/401 130/400 112/398 97/397 85/396 74/395 33000 Time/Fuel 33/2500 30/2300 27/2100 25/1950 23/1850 21/1700 20/1600 18/1450 16/1300 14/1150 12/1000 Dist/TAS 210/407 186/404 168/402 153/400 141/399 130/398 121/397 105/395 92/394 80/393 70/392 32000 Time/Fuel 30/2350 27/2150 25/2000 23/1900 22/1750 20/1650 19/1550 17/1400 15/1250 13/1100 12/1000 Dist/TAS 185/401 167/399 153/398 141/396 130/395 121/394 113/394 98/392 86/391 7 6/390 67/389 31000 Time/Fuel 27/2200 25/2050 23/1900 22/1800 20/1700 19/1600 18/1500 16/1350 14/1200 13/1100 11/950 Dist/TAS 166/396 152/395 141/394 130/393 121/392 113/391 106/390 93/389 82/388 7 2/387 63/387 30000 Time/Fuel 25/2100 24/1950 22/1850 21/1750 19/1650 18/1550 17/1450 15/1300 14/1150 12/1050 11/950 Dist/TAS 152/392 140/391 130/389 121/389 113/388 106/387 99/387 87/385 77/385 68 /384 60/383 29000 Time/Fuel 23/1950 22/1850 20/1750 19/1650 18/1550 17/1450 16/1400 14/1250 13/1100 12/1000 10/900 Dist/TAS 136/386 126/385 118/384 110/383 106/383 97/382 91/382 80/381 71/380 63/ 379 56/379 28000 Time/Fuel 21/1850 20/1750 19/1650 18/1550 17/1500 16/1400 15/1350 14/1200 12/1100 11/950 10/850 Dist/TAS 123/380 114/379 107/379 100/378 94/378 89/377 83/377 74/376 66/375 58/3 75 52/375
27000 Time/Fuel 20/1750 19/1650 18/1550 17/1500 16/1400 15/1350 14/1250 13/1150 11/1050 10/950 9/850 Dist/TAS 111/375 104/374 98/374 92/373 86/373 81/372 77/372 68/371 61/371 54/371 48/370 26000 Time/Fuel 18/1650 17/1550 16/1500 16/1400 15/1350 14/1300 13/1200 12/1100 11/1000 10/900 9/800 Dist/TAS 101/370 95/370 89/369 84/369 79/368 75/368 70/368 63/367 56/367 50/366 44/366 25000 Time/Fuel 17/1550 16/1500 15/1400 15/1350 14/1300 13/1200 13/1150 11/1050 10/950 9/850 8/750 Dist/TAS 92/365 86/365 81/365 77/364 73/364 69/364 65/363 58/363 52/363 46/362 4 1/362 24000 Time/Fuel 16/1500 15/1400 14/1350 14/1300 13/1200 12/1150 12/1100 11/1000 10/900 9/850 8/750 Dist/TAS 84/361 79/361 75/360 70/360 67/360 63/360 60/359 53/359 48/359 43/358 3 8/358 23000 Time/Fuel 15/1400 14/1350 13/1300 13/1250 12/1150 12/1100 11/1050 10/950 9 /900 8/800 7/700 Dist/TAS 77/357 72/357 68/356 65/356 61/356 58/356 55/356 49/355 44/355 39/355 3 5/355 22000 Time/Fuel 14/1350 13/1300 13/1250 12/1150 11/1100 11/1050 10/1000 9/900 9/ 850 8/750 7/700 Dist/TAS 70/353 66/353 63/352 59/352 56/352 53/352 50/352 45/351 41/351 36/351 3 2/351 21000 Time/Fuel 13/1300 12/1200 12/1150 11/1100 11/1050 10/1000 10/950 9/900 8/8 00 7/750 7/650 Dist/TAS 64/349 60/349 57/349 54/349 52/348 49/348 46/348 42/348 37/348 34/348 3 0/347 20000 Time/Fuel 12/1200 12/1150 11/1100 11/1050 10/1000 10/950 9/950 8/850 8/750 7/700 6/650 Dist/TAS 58/345 55/345 52/345 50/345 47/345 45/345 43/345 38/344 34/344 31/344 2 8/344 19000 Time/Fuel 11/1150 11/1100 10/1050 10/1000 9/950 9/900 9/900 8/800 7/750 7/ 650 6/600 Dist/TAS 53/342 50/342 48/342 45/342 43/342 41/341 39/341 35/341 32/341 28/341 2 5/341 18000 Time/Fuel 11/1100 10/1050 10/1000 9/950 9/900 9/900 8/850 7/750 7/700 6/65 0 6/600 Dist/TAS 48/339 46/339 44/338 42/338 39/338 38/338 36/338 32/338 29/338 26/338 2 3/338 17000 Time/Fuel 10/1050 10/1000 9/950 9/900 8/850 8/850 8/800 7/750 6/650 6/600 5/550 Dist/TAS 44/335 42/335 40/335 38/335 36/335 34/335 33/335 29/335 27/335 24/335 2 1/335 16000 Time/Fuel 9/1000 9/950 9/900 8/850 8/850 7/800 7/750 7/700 6/650 5/600 5/5 50 Dist/TAS 40/332 38/332 36/332 34/332 33/332 31/332 30/332 27/332 24/332 22/332 1 9/332 15000 Time/Fuel 9/950 8/900 8/850 8/800 7/800 7/750 7/700 6/650 6/600 5/550 5/50 0 Dist/TAS 36/329 34/329 33/329 31/329 30/329 28/329 27/329 24/329 22/329 20/329 1 8/329 14000 Time/Fuel 8/850 8/650 7/800 7/750 7/750 7/700 6/700 6/650 5/550 5/500 4/50 0 Dist/TAS 32/326 31/326 29/326 28/326 27/326 25/326 24/326 22/326 20/326 18/326 1 6/326 13000 Time/Fuel 7/800 7/800 7/750 7/750 6/700 6/650 6/650 5/600 5/550 5/500 4/45 0 Dist/TAS 29/323 28/323 26/323 25/323 24/323 23/323 22/323 20/323 18/323 16/323 1 4/323
12000 Time/Fuel 7/750 7/750 6/700 6/700 6/650 6/650 5/600 5/550 5/500 4/450 4/45 0 Dist/TAS 26/321 25/321 23/321 22/321 21/321 20/321 19/321 18/321 16/320 14/320 1 3/320 11000 Time/Fuel 6/700 6/700 6/650 6/650 5/600 5/600 5/550 5/500 4/500 4/450 4/40 0 Dist/TAS 23/318 22/318 21/318 20/318 19/318 18/318 17/318 16/318 14/318 13/318 1 1/318 10000 Time/Fuel 6/650 6/650 5/600 5/600 5/550 5/550 5/550 4/500 4/450 4/400 3/40 0 Dist/TAS 20/315 19/315 18/315 17/315 16/315 16/315 15/315 14/315 12/315 11/315 1 0/315 8000 Time/Fuel 5/550 5/550 5/550 4/500 4/500 4/500 4/450 4/400 3/400 3/350 3/350 Dist/TAS 14/310 14/310 13/310 13/310 12/310 11/310 11/310 10/310 9/310 8/310 7/3 10 6000 Time/Fuel 4/450 4/450 4/450 4/450 3/400 3/400 3/400 3/350 3/350 3/300 2/300 Dist/TAS 10/306 9/306 9/306 8/306 8/306 8/306 7/306 7/306 6/306 5/306 5/306 1500 Time/Fuel 2/250 2/250 2/250 2/250 2/250 2/250 2/250 2/200 2/200 2/200 1/150 Fuel Adjustment for high elevation airports Effect on time and distance is negligible Fuel Adjustment -50 -150 -200 -300 En-route Climb 280/.74 -350 -400 Airport Elevation 2000 4000 6000 8000 10000 12000 FIGURE 033-24 033 PICTURE SUPPLEMENTS 115 © 2008 AVIATIONEXAM.com Wind Range Correction Graph 300 400 500 600 0 100 200 300 400 500 600 700 800 HEADWIND TAILWIND GROUND DISTANCE NM 700 800 600 500 450 400 350 300 250 200 150 100
50 150 200 100 50 0 50 100 150 200 WIND VELOCITY kt M A N E C N A T S I D R I A t k S A T E S I U R C E G A R E V A FIGURE 033-25 033 PICTURE SUPPLEMENTS 116 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 28,000 ft LONG RANGE CRUISE GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg TAS CRUISE DISTANCE NAUTICAL AIR MILES 35000 376 0 20 41 62 83 104 125 145 166 187 36000 380 208 229 249 270 290 311 332 352 373 393 37000 384 414 434 455 475 495 516 536 557 577 597 38000 388 618 638 658 678 698 718 738 759 779 799 39000 392 819 839 859 879 898 918 938 958 978 998 40000 396 1018 1037 1057 1077 1096 1116 1136 1155 1175 1195 41000 399 1214 1234 1253 1273 1292 1312 1331 1350 1370 1389 42000 403 1409 1428 1447 1466 1486 1505 1524 1543 1563 1582 43000 406 1601 1620 1639 1658 1677 1696 1715 1734 1753 1772 44000 409 1791 1810 1829 1848 1866 1885 1904 1923 1942 1960 45000 413 1979 1998 2016 2035 2054 2072 2091 2109 2128 2147 46000 416 2165 2184 2202 2220 2239 2257 2275 2294 2312 2331 47000 419 2349 2367 2385 2404 2422 2440 2458 2476 2495 2513 48000 422 2531 2549 2567 2585 2603 2621 2639 2657 2675 2693 49000 425 2711 2729 2747 2764 2782 2800 2818 2836 2853 2871 50000 427 2889 2907 2924 2942 2960 2977 2995 3013 3030 3048 51000 429 3065 3083 3100 3118 3135 3153 3170 3188 3205 3222 52000 432 3240 3257 3274 3292 3309 3326 3344 3361 3378 3395 53000 434 3413 3430 3447 3464 3481 3498 3515 3532 3549 3567 54000 436 3584 3601 3617 3634 3651 3668 3685 3702 3719 3736 55000 437 3753 3770 3786 3803 3820 3837 3853 3870 3887 3904 56000 439 3920 3937 3953 3970 3987 4003 4020 4036 4053 4069 57000 440 4086 4102 4119 4135 4152 4168 4184 4201 4217 4234 58000 441 4250 4266 4282 4299 4315 4331 4347 4364 4380 4396 59000 442 4412 4428 4444 4460 4476 4492 4509 4525 4541 4557 60000 442 4573 4589 4605 4620 4636 4652 4668 4684 4700 4716 61000 442 4732 4747 4763 4779 4795 4810 4826 4842 4858 4873 62000 442 4889 4905 4920 4936 4951 4967 4983 4998 5014 5029 63000 443 5045 5060 5076 5091 5106 5122 5137 5153 5168 5184 64000 443 5199 5214 5229 5245 5260 5275 5290 5306 5321 5336 65000 443 5351 5367 5382 5397 5412 5427 5442 5457 5472 5487 66000 443 5502 5517 5532 5547 5562 5577 5592 5607 5622 5637 67000 443 5652 5666 5681 5696 5711 5725 5740 5755 5770 5784 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMIT A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMIT B) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMIT
C) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMIT NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Long Range Cruise Pressure Altitude 28,000 ft FIGURE 033-26 033 PICTURE SUPPLEMENTS 117 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 33,000 ft LONG RANGE CRUISE GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg TAS CRUISE DISTANCE NAUTICAL AIR MILES 35000 400 0 23 46 69 92 115 138 161 184 207 36000 405 230 252 275 298 320 343 366 389 411 434 37000 408 457 479 502 524 547 569 591 614 636 659 38000 412 681 703 725 747 770 792 814 836 858 880 39000 415 902 924 946 968 990 1012 1034 1055 1077 1099 40000 419 1121 1143 1164 1186 1207 1229 1251 1272 1294 1315 41000 421 1337 1358 1380 1401 1422 1444 1465 1486 1508 1529 42000 424 1550 1571 1593 1614 1635 1656 1677 1698 1719 1740 43000 426 1761 1782 1803 1823 1844 1865 1886 1907 1928 1948 44000 428 1969 1990 2010 2031 2051 2072 2092 2113 2134 2154 45000 430 2175 2195 2215 2235 2256 2276 2296 2317 2337 2357 46000 432 2377 2397 2417 2437 2458 2478 2498 2518 2538 2558 47000 433 2578 2597 2617 2637 2657 2677 2696 2716 2736 2756 48000 433 2775 2795 2814 2834 2854 2873 2893 2912 2932 2951 49000 433 2971 2990 3009 3029 3048 3067 3087 3106 3125 3144 50000 433 3164 3183 3202 3221 3240 3259 3278 3297 3316 3335 51000 433 3354 3373 3392 3411 3429 3448 3467 3486 3505 3523 52000 433 3542 3561 3579 3598 3617 3635 3654 3672 3691 3709 53000 433 3728 3746 3765 3783 3801 3819 3838 3856 3874 3893 54000 433 3911 3929 3947 3965 3983 4001 4019 4038 4056 4074 55000 433 4092 4110 4127 4145 4163 4181 4199 4216 4234 4252 56000 433 4270 4287 4305 4323 4340 4358 4375 4393 4410 4428 57000 433 4445 4463 4480 4497 4515 4532 4549 4567 4584 4601 58000 433 4619 4636 4653 4670 4687 4704 4721 4738 4755 4772 59000 433 4789 4806 4823 4840 4856 4873 4890 4907 4924 4940 60000 433 4957 4974 4990 5007 5024 5040 5057 5073 5090 5106 61000 433 5123 5139 5155 5172 5188 5204 5221 5237 5253 5270 62000 433 5286 5302 5318 5334 5350 5366 5382 5398 5414 5430 63000 433 5446 5462 5478 5493 5509 5525 5541 5557 5572 5588 64000 433 5604 5619 5635 5650 5666 5681 5697 5712 57,28 5743 65000 433 5759 5774 5789 5804 5820 5835 5850 5865 5880 5896 66000 433 5911 5926 5941 5956 5970 5985 6000 6015 6030 6045 67000 433 6060 6075 6089 6104 6118 6133 6148 6162 6177 6191 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 58,200 kg A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMIT B) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMIT C) THRUST LIMITED WEIGHT FOR ISA +20 IS 66,400 kg NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Long Range Cruise Pressure Altitude 33,000 ft
FIGURE 033-27 033 PICTURE SUPPLEMENTS 118 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 34,000 ft LONG RANGE CRUISE GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg TAS CRUISE DISTANCE NAUTICAL AIR MILES 35000 405 0 23 46 70 93 117 140 164 187 210 36000 409 234 257 280 303 326 350 373 396 419 442 37000 413 465 488 511 534 557 579 602 625 648 671 38000 416 694 716 739 761 784 806 829 851 874 896 39000 419 919 941 963 986 1008 1030 1053 1075 1097 1119 40000 422 1142 1164 1186 1207 1229 1251 1273 1295 1317 1339 41000 424 1361 1383 1405 1426 1448 1470 1492 1513 1535 1557 42000 427 1578 1600 1621 1643 1664 1685 1707 1728 1750 1771 43000 428 1792 1814 1835 1856 1877 1898 1919 1940 1961 1983 44000 430 2004 2025 2045 2066 2087 2108 2129 2150 2171 2191 45000 431 2212 2233 2253 2274 2295 2315 2336 2356 2377 2398 46000 431 2418 2438 2459 2479 2499 2520 2540 2560 2581 2601 47000 431 2621 2641 2661 2682 2702 2722 2742 2762 2782 2802 48000 431 2822 2842 2862 2881 2901 2921 2941 2960 2980 3000 49000 431 3020 3039 3059 3078 3098 3118 3137 3157 3176 3196 50000 431 3215 3234 3254 3273 3292 3311 3331 3350 3369 3389 51000 431 3408 3427 3446 3465 3484 3503 3522 3541 3560 3579 52000 431 3598 3616 3635 3654 3673 3691 3710 3729 3747 3766 53000 431 3785 3803 3822 3840 3859 3877 3896 3914 3932 3951 54000 431 3969 3987 4006 4024 4042 4060 4078 4096 4115 4133 55000 431 4151 4169 4187 4205 4223 4240 4258 4276 4294 4312 56000 431 4330 4348 4365 4383 4400 4418 4436 4453 4471 4489 57000 431 4506 4524 4541 4558 4576 4593 4610 4628 4645 4662 58000 431 4680 4697 4714 4731 4748 4765 4782 4799 4816 4833 59000 431 4851 4867 4884 4901 4918 4934 4951 4968 4985 5002 60000 431 5018 5035 5051 5068 5084 5101 5117 5134 5150 5167 61000 431 5183 5200 5216 5232 5248 5264 5281 5297 5313 5329 62000 431 5345 5361 5377 5393 5409 5425 5441 5457 5472 5488 63000 431 5504 5520 5535 5551 5566 5582 5598 5613 5629 5644 64000 431 5660 5675 5690 5706 5721 5736 5751 5766 5782 5797 65000 430 5812 5827 5842 5857 5872 5886 5901 5916 5931 5946 66000 430 5961 5975 5990 6004 6019 6033 6048 6062 6077 6091 67000 430 6106 6120 6134 6148 6162 6176 6190 6204 6219 6233 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 55,500 kg A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER IS 67,100 kg B) THRUST LIMITED WEIGHT FOR ISA +15 IS 65,700 kg C) THRUST LIMITED WEIGHT FOR ISA +20 IS 64,000 kg NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Long Range Cruise Pressure Altitude 34,000 ft FIGURE 033-28 033 PICTURE SUPPLEMENTS 119 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto
PRESSURE ALTITUDE 35,000 ft LONG RANGE CRUISE GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg TAS CRUISE DISTANCE NAUTICAL AIR MILES 35000 410 0 23 47 71 95 119 143 167 191 214 36000 414 238 262 285 309 333 356 380 403 427 450 37000 417 474 497 521 544 567 590 614 637 660 683 38000 420 707 730 753 776 798 821 844 867 890 913 39000 422 936 959 982 1004 1027 1050 1072 1095 1117 1140 40000 425 1163 1185 1207 1230 1252 1275 1297 1319 1342 1364 41000 426 1386 1408 1430 1452 1474 1496 1519 1541 1563 1585 42000 428 1607 1628 1650 1672 1694 1715 1737 1759 1781 1802 43000 429 1824 1845 1867 1888 1910 1931 1953 1974 1996 2017 44000 429 2039 2060 2081 2102 2123 2144 2165 2187 2208 2229 45000 429 2250 2271 2292 2313 2334 2355 2375 2396 2417 2438 46000 429 2459 2480 2500 2521 2541 2562 2582 2603 2624 2644 47000 429 2665 2685 2705 2726 2746 2766 2787 2807 2827 2848 48000 429 2868 2888 2908 2928 2948 2968 2988 3008 3028 3048 49000 429 3068 3088 3107 3127 3147 3166 3186 3206 3226 3245 50000 429 3265 3284 3304 3323 3343 3362 3381 3401 3420 3440 51000 429 3459 3478 3497 3516 3536 3555 3574 3593 3612 3631 52000 429 3650 3669 3688 3707 3726 3744 3763 3782 3801 3820 53000 429 3838 3857 3875 3894 3913 3931 3950 3968 3987 4005 54000 429 4024 4042 4060 4078 4097 4115 4133 4151 4170 4188 55000 430 4206 4224 4242 4260 4278 4296 4314 4331 4349 4367 56000 430 4385 4403 4420 4438 4456 4473 4491 4509 4526 4544 57000 430 4561 4579 4596 4613 4631 4648 4665 4682 4700 4717 58000 429 4734 4751 4768 4785 4802 4819 4836 4853 4870 4887 59000 429 4904 4921 4937 4954 4971 4987 5004 5021 5037 5054 60000 429 5070 5087 5103 5119 5136 5152 5168 5184 5201 5217 61000 429 5233 5249 5265 5281 5297 5313 5329 5345 5361 5377 62000 429 5393 5408 5424 5439 5455 5470 5486 5501 5517 5532 63000 428 5548 5563 5578 5593 5608 5623 5638 5654 5669 5684 64000 428 5699 5714 5728 5743 5758 5772 5787 5802 5817 5831 65000 427 5846 5860 5874 5889 5903 5917 5932 5946 5960 5974 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 53,000 kg A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER IS 64,500 kg B) THRUST LIMITED WEIGHT FOR ISA +15 IS 63,100 kg C) THRUST LIMITED WEIGHT FOR ISA +20 IS 61,600 kg NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Long Range Cruise Pressure Altitude 35,000 ft FIGURE 033-29 033 PICTURE SUPPLEMENTS 120 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 24,000 ft MACH 0.74 CRUISE TAS 447 kt GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg CRUISE DISTANCE NAUTICAL AIR MILES 35000 0 16 33 49 66 83 99 116 133 149 36000 166 183 199 216 232 249 266 282 299 315 37000 332 349 365 382 398 415 431 448 465 481 38000 498 514 531 547 564 580 597 613 630 646 39000 663 679 696 712 729 745 762 778 795 811 40000 828 844 860 877 893 910 926 942 959 975
41000 992 1008 1024 1041 1057 1074 1090 1106 1123 1139 42000 1155 1172 1188 1204 1221 1237 1253 1269 1286 1302 43000 1318 1335 1351 1367 1383 1399 1416 1432 1448 1464 44000 1481 1497 1513 1529 1545 1561 1578 1594 1610 1626 45000 1642 1658 1675 1691 1707 1723 1739 1755 1771 1787 46000 1803 1819 1835 1851 1867 1883 1899 1915 1932 1948 47000 1964 1980 1995 2011 2027 2043 2059 2075 2091 2107 48000 2123 2139 2155 2171 2187 2202 2218 2234 2250 2266 49000 2282 2298 2313 2329 2345 2361 2377 2392 2408 2424 50000 2440 2455 2471 2487 2503 2518 2534 2550 2565 2581 51000 2597 2612 2628 2644 2659 2675 2691 2706 2722 2737 52000 2753 2769 2784 2800 2815 2831 2846 2862 2877 2893 53000 2908 2924 2939 2955 2970 2986 3001 3017 3032 3047 54000 3063 3078 3094 3109 3124 3140 3155 3170 3186 3201 55000 3216 3232 3247 3262 3277 3293 3308 3323 3338 3354 56000 3369 3384 3399 3414 3430 3445 3460 3475 3490 3506 57000 3521 3536 3551 3566 3581 3596 3611 3626 3641 3656 58000 3671 3686 3701 3716 3731 3746 3761 3776 3791 3806 59000 3821 3836 3851 3866 3881 3896 3910 3925 3940 3995 60000 3970 3985 4000 4014 4029 4044 4059 4073 4088 4103 61000 4118 4132 4147 4162 4176 4191 4206 4220 4235 4250 62000 4264 4279 4294 4308 4323 4337 4352 4366 4381 4396 63000 4410 4425 4439 4454 4468 4483 4497 4511 4526 4540 64000 4555 4569 4584 4598 4612 4627 4641 4655 4670 4684 65000 4698 4713 4727 4741 4756 4770 4784 4798 4813 4827 66000 4841 4855 4869 4884 4898 4912 4926 4940 4954 4968 67000 4983 4997 5011 5025 5039 5053 5067 5081 5095 5109 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMIT A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMIT B) THRUST LIMITED WEIGHT FOR IS A +15 EXCEEDS STRUCTURAL LIMIT C) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMIT NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Pressure Altitude 24,000 ft Mach 0.74 Cruise FIGURE 033-30 033 PICTURE SUPPLEMENTS 121 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 25,000 ft MACH 0.74 CRUISE TAS 445 kt GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg CRUISE DISTANCE NAUTICAL AIR MILES 35000 0 17 34 51 69 86 103 120 138 155 36000 172 189 206 224 241 258 275 293 310 327 37000 344 361 378 396 413 430 447 464 481 499 38000 516 533 550 567 584 601 618 635 652 670 39000 687 704 721 738 755 772 789 806 823 840 40000 857 874 891 908 925 942 959 976 993 1010 41000 1027 1044 1061 1076 1094 1111 1128 1145 1162 1179 42000 1196 1213 1230 1246 1263 1280 1297 1314 1331 1347 43000 1364 1381 1398 1414 1431 1448 1465 1482 1498 1515 44000 1532 1548 1565 1582 1599 1615 1632 1649 1665 1682 45000 1699 1715 1732 1748 1765 1782 1798 1815 1831 1848 46000 1865 1881 1898 1914 1931 1947 1964 1980 1997 2013 47000 2030 2046 2063 2079 2096 2112 2128 2145 2161 2178
48000 2194 2210 2227 2243 2259 2276 2292 2308 2325 2341 49000 2358 2374 2390 2406 2422 2439 2455 2471 2487 2504 50000 2520 2536 2552 2568 2585 2601 2617 2633 2649 2665 51000 2681 2698 2714 2730 2746 2762 2778 2794 2810 2826 52000 2842 2858 2874 2890 2906 2922 2938 2954 2970 2986 53000 3002 3017 3033 3049 3065 3081 3097 3113 3128 3144 54000 3160 3176 3192 3207 3223 3239 3255 3270 3286 3302 55000 3318 3333 3349 3365 3380 3396 3411 3427 3443 3458 56000 3474 3490 3505 3521 3536 3552 3567 3583 3598 3614 57000 3630 3645 3660 3676 3691 3707 3722 3738 3753 3768 58000 3784 3799 3815 3830 3845 3861 3876 3891 3906 3922 59000 3937 3952 3968 3983 3998 4013 4028 4044 4059 4074 60000 4089 4104 4119 4135 4150 4165 4180 4195 4210 4225 61000 4240 4255 4270 4285 4300 4315 4330 4345 4360 4375 62000 4390 4405 4420 4435 4450 4465 4479 4494 4509 4524 63000 4539 4554 4568 4583 4598 4613 4628 4642 4657 4672 64000 4687 4701 4716 4731 4745 4760 4774 4789 4804 4818 65000 4833 4848 4862 4877 4891 4906 4920 4935 4949 4964 66000 4978 4993 5007 5022 5036 5050 5065 5079 5094 5108 67000 5122 5137 5151 5165 5180 5194 5208 5222 5237 5251 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMIT A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMIT B) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMIT C) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMIT NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Pressure Altitude 25,000 ft Mach 0.74 Cruise FIGURE 033-31 033 PICTURE SUPPLEMENTS 122 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 28,000 ft MACH 0.74 CRUISE TAS 440 kt GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg CRUISE DISTANCE NAUTICAL AIR MILES 35000 0 19 38 57 76 95 114 134 153 172 36000 191 210 229 248 267 286 305 324 343 362 37000 382 401 419 438 457 476 495 514 533 552 38000 571 590 609 628 647 666 684 703 722 741 39000 760 779 797 816 835 854 873 891 910 929 40000 948 966 985 1004 1022 1041 1060 1078 1097 1116 41000 1134 1153 1171 1190 1209 1227 1246 1264 1283 1301 42000 1320 1338 1357 1375 1394 1412 1431 1449 1467 1486 43000 1504 1523 1541 1559 1578 1596 1614 1633 1651 1669 44000 1688 1706 1724 1742 1760 1779 1797 1815 1833 1851 45000 1870 1888 1906 1924 1942 1960 1978 1996 2014 2032 46000 2050 2068 2086 2104 2122 2140 2158 2176 2194 2212 47000 2230 2248 2265 2283 2301 2319 2337 2355 2372 2390 48000 2408 2426 2443 2461 2479 2497 2514 2532 2550 2567 49000 2585 2603 2620 2638 2655 2673 2690 2708 2726 2743 50000 2761 2778 2795 2813 2830 2848 2865 2883 2900 2917 51000 2935 2952 2969 2987 3004 3021 3039 3056 3073 3090 52000 3108 3125 3142 3159 3176 3193 3211 3228 3245 3262 53000 3279 3296 3313 3330 3347 3364 3381 3398 3415 3432 54000 3449 3466 3483 3500 3517 3533 3550 3567 3584 3601
55000 3618 3634 3651 3668 3685 3701 3718 3735 3751 3768 56000 3785 3801 3818 3835 3851 3868 3884 3901 3917 3934 57000 3951 3967 3983 4000 4016 4033 4049 4065 4082 4098 58000 4115 4131 4147 4164 4180 4196 4212 4229 4245 4261 59000 4277 4293 4310 4326 4324 4358 4374 4390 4406 4422 60000 4438 4454 4470 4486 4502 4518 4534 4550 4566 4582 61000 4598 4614 4630 4645 4661 4677 4693 4709 4724 4740 62000 4756 4772 4787 4803 4818 4834 4850 4865 4881 4897 63000 4912 4928 4943 4959 4974 4990 5005 5021 5036 5052 64000 5067 5082 5098 5113 5128 5144 5159 5174 5190 5205 65000 5220 5235 5250 5266 5281 5296 5311 5326 5341 5357 66000 5372 5387 5402 5417 5432 5447 5462 5477 5492 5507 67000 5522 5536 5551 5566 5581 5596 5611 5625 5640 5655 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMIT A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMIT B) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMIT C) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMIT NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Pressure Altitude 28,000 ft Mach 0.74 Cruise FIGURE 033-32 033 PICTURE SUPPLEMENTS 123 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 31,000 ft MACH 0.74 CRUISE TAS 434 kt GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg CRUISE DISTANCE NAUTICAL AIR MILES 35000 0 21 42 63 84 105 126 147 168 189 36000 210 231 252 273 294 315 336 357 378 399 37000 420 440 461 482 503 524 544 565 586 607 38000 628 648 669 689 710 731 751 772 793 813 39000 834 854 875 895 916 936 957 977 998 1018 40000 1039 1059 1079 1100 1120 1140 1161 1181 1201 1222 41000 1242 1262 1282 1303 1323 1343 1363 1383 1403 1423 42000 1444 1464 1484 1504 1524 1544 1564 1584 1604 1624 43000 1644 1663 1683 1703 1723 1743 1763 1782 1802 1822 44000 1842 1862 1881 1901 1921 1940 1960 1979 1999 2019 45000 2038 2058 2077 2097 2116 2136 2155 2175 2194 2214 46000 2233 2252 2272 2291 2310 2330 2349 2368 2388 2407 47000 2426 2445 2464 2483 2503 2522 2541 2560 2579 2598 48000 2617 2636 2655 2674 2693 2712 2731 2750 2769 2788 49000 2807 2825 2844 2863 2882 2900 2919 2938 2956 2975 50000 2994 3013 3031 3050 3068 3087 3105 3124 3142 3161 51000 3179 3198 3216 3235 3253 3271 3290 3308 3326 3345 52000 3363 3381 3399 3417 3436 3454 3472 3490 3508 3526 53000 3545 3563 3580 3598 3616 3634 3652 3670 3688 3706 54000 3724 3742 3760 3777 3795 3813 3831 3848 3866 3884 55000 3902 3919 3937 3954 3972 3989 4007 4024 4042 4060 56000 4077 4094 4112 4129 4146 4164 4181 4198 4216 4233 57000 4251 4268 4285 4302 4319 4336 4353 4370 4388 4405 58000 4422 4439 4456 4473 4490 4507 4523 4540 4557 4574 59000 4591 4608 4625 4641 4658 4675 4691 4708 4725 4742 60000 4758 4775 4791 4808 4824 4841 4857 4874 4890 4907 61000 4923 4940 4956 4972 4989 5005 5021 5038 5054 5070
62000 5086 5103 5119 5135 5151 5167 5183 5199 5215 5231 63000 5247 5263 5279 5295 5311 5327 5343 5358 5374 5390 64000 5406 5422 5437 5453 5469 5484 5500 5516 5531 5547 65000 5563 5578 5594 5609 5624 5640 5655 5671 5686 5702 66000 5717 5732 5748 5763 5778 5793 5809 5824 5839 5854 67000 5870 5885 5900 5915 5930 5945 5960 5975 5990 6005 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 63,500 kg A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMIT B) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMIT C) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMIT NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Mach 0.74 Cruise Pressure Altitude 31,000 ft FIGURE 033-33 033 PICTURE SUPPLEMENTS 124 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 34,000 ft MACH 0.74 CRUISE TAS 428 kt GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg CRUISE DISTANCE NAUTICAL AIR MILES 35000 0 22 45 68 91 114 137 160 183 206 36000 229 252 275 297 320 343 365 388 411 434 37000 456 479 502 524 547 569 592 614 637 659 38000 682 704 726 749 771 793 816 838 860 883 39000 905 927 949 971 993 1015 1037 1060 1082 1104 40000 1126 1148 1170 1191 1213 1235 1257 1279 1301 1323 41000 1344 1366 1388 1409 1431 1453 1474 1496 1517 1539 42000 1561 1582 1603 1625 1646 1668 1689 1710 1732 1753 43000 1775 1796 1817 1838 1859 1880 1902 1923 1944 1965 44000 1986 2007 2028 2049 2070 2091 2112 2132 2153 2174 45000 2195 2216 2236 2257 2278 2298 2319 2340 2360 2361 46000 2402 2422 2442 2463 2483 2504 2524 2544 2565 2585 47000 2606 2626 2646 2666 2686 2706 2726 2747 2767 2787 48000 2807 2827 2847 2867 2886 2906 2926 2946 2966 2986 49000 3006 3025 3045 3064 3084 3104 3123 3143 3163 3182 50000 3202 3221 3240 3260 3279 3298 3318 3337 3356 3376 51000 3395 3414 3433 3452 3471 3491 3510 3529 3548 3567 52000 3586 3605 3624 3642 3661 3680 3699 3718 3736 3755 53000 3774 3792 3811 3830 3848 3867 3885 3904 3922 3941 54000 3959 3978 3996 4014 4032 4051 4069 4087 4105 4124 55000 4142 4160 4178 4196 4214 4232 4250 4268 4286 4304 56000 4322 4339 4357 4375 4393 4410 4428 4446 4464 4481 57000 4499 4516 4534 4551 4569 4586 4604 4621 4639 4656 58000 4673 4691 4708 4725 4742 4759 4777 4794 4811 4828 59000 4845 4862 4879 4896 4913 4930 4947 4963 4980 4997 60000 5014 5031 5047 5064 5081 5097 5114 5130 5147 5164 61000 5180 5196 5213 5229 5245 5262 5278 5294 5311 5327 62000 5343 5359 5375 5391 5407 5423 5439 5455 5471 5487 63000 5503 5519 5534 5550 5566 5581 5597 5613 5828 5644 64000 5660 5675 5690 5705 5721 5736 5751 5767 5782 5797 65000 5812 5827 5842 5857 5872 5887 5902 5917 5932 5947 66000 5962 5976 5991 6005 6020 6034 6049 6063 6078 6093 67000 6107 6121 6135 6150 6164 6178 6192 6206 6220 6234 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 55,500 kg
A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER IS 67,100 kg B) THRUST LIMITED WEIGHT FOR ISA +15 IS 65,700 kg C) THRUST LIMITED WEIGHT FOR ISA +20 IS 64,000 kg NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Mach 0.74 Cruise Pressure Altitude 34,000 ft FIGURE 033-34 033 PICTURE SUPPLEMENTS 125 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 30,000 ft MACH 0.78 CRUISE TAS 460 kt GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg CRUISE DISTANCE NAUTICAL AIR MILES 35000 0 19 38 57 77 96 115 135 154 173 36000 193 212 231 250 269 289 308 327 346 366 37000 385 404 423 442 461 480 499 519 538 557 38000 576 595 614 633 652 671 690 709 728 747 39000 766 785 804 823 842 860 879 898 917 936 40000 955 974 993 1011 1030 1049 1068 1086 1105 1124 41000 1143 1161 1180 1199 1217 1236 1255 1273 1292 1311 42000 1329 1348 1366 1385 1403 1422 1440 1459 1477 1496 43000 1514 1533 1551 1569 1588 1606 1624 1643 1661 1679 44000 1698 1716 1734 1752 1771 1789 1807 1825 1844 1862 45000 1880 1898 1916 1934 1952 1970 1988 2006 2024 2042 46000 2061 2078 2096 2114 2132 2150 2168 2186 2204 2222 47000 2239 2257 2275 2293 2310 2328 2346 2363 2381 2399 48000 2417 2434 2452 2469 2487 2504 2522 2539 2557 2574 49000 2592 2609 2627 2644 2661 2679 2696 2713 2731 2748 50000 2765 2783 2800 2817 2834 2851 2868 2886 2903 2920 51000 2937 2954 2971 2988 3005 3022 3039 3056 3073 3090 52000 3107 3123 3140 3157 3174 3191 3207 3224 3241 3258 53000 3274 3291 3308 3324 3341 3357 3374 3390 3407 3423 54000 3440 3456 3473 3489 3506 3522 3538 3555 3571 3587 55000 3604 3626 3636 3652 3668 3684 3701 3717 3733 3749 56000 3765 3781 3797 3813 3829 3845 3861 3877 3893 3909 57000 3925 3940 3956 3972 3988 4003 4019 4035 4050 4066 58000 4082 4097 4113 4128 4144 4160 4175 4191 4206 4222 59000 4237 4252 4268 4283 4298 4314 4329 4344 4360 4375 60000 4390 4405 4421 4436 4451 4466 4481 4496 4511 4526 61000 4541 4556 4571 4586 4601 4616 4631 4646 4661 4676 62000 4691 4705 4720 4735 4749 4764 4779 4794 4808 4823 63000 4838 4852 4867 4881 4896 4910 4925 4939 4954 4968 64000 4983 4997 5011 5025 5040 5054 5068 5083 5097 5111 65000 5125 5140 5154 5168 5182 5196 5210 5224 5238 5252 66000 5266 5280 5294 5308 5322 5335 5349 5363 5377 5391 67000 5405 5418 5432 5446 5459 5473 5487 5500 5514 5528 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 64,200 kg A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMIT B) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMIT C) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMIT NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA
D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Mach 0.78 Cruise Pressure Altitude 30,000 ft FIGURE 033-35 033 PICTURE SUPPLEMENTS 126 © 2008 AVIATIONEXAM.com All Engines Maximum Cruise Thrust Limits A/C Auto PRESSURE ALTITUDE 21,000 ft LOW-LEVEL CRUISE TAS 406 kt GROSS 0 100 200 300 400 500 600 700 800 900 WT. kg CRUISE DISTANCE NAUTICAL AIR MILES 35000 0 16 33 49 66 82 99 115 132 148 36000 165 181 198 214 231 247 264 280 297 313 37000 330 346 363 379 396 412 429 445 461 478 38000 494 511 527 543 560 576 592 609 625 642 39000 658 674 691 707 723 739 756 772 788 805 40000 821 837 853 870 886 902 918 935 951 967 41000 983 999 1016 1032 1048 1064 1080 1096 1112 1129 42000 1145 1161 1177 1193 1209 1225 1241 1257 1273 1289 43000 1305 1321 1337 1353 1369 1385 1401 1417 1433 1449 44000 1465 1481 1497 1513 1529 1545 1561 1577 1593 1609 45000 1624 1640 1656 1672 1688 1704 1719 1735 1751 1767 46000 1783 1798 1814 1830 1846 1861 1877 1893 1909 1924 47000 1940 1956 1971 1987 2003 2018 2034 2050 2065 2081 48000 2096 2112 2128 2143 2159 2174 2190 2205 2221 2236 49000 2252 2267 2283 2298 2314 2329 2345 2360 2376 2391 50000 2407 2422 2437 2453 2468 2483 2499 2514 2530 2545 51000 2560 2576 2591 2606 2621 2637 2652 2667 2682 2698 52000 2713 2728 2743 2758 2774 2789 2804 2819 2834 2849 53000 2865 2880 2895 2910 2925 2940 2955 2970 2985 3000 54000 3015 3030 3045 3060 3075 3090 3105 3120 3135 3150 55000 3165 3180 3195 3209 3224 3239 3254 3269 3284 3299 56000 3313 3328 3343 3358 3373 3387 3402 3417 3432 3446 57000 3461 3476 3490 3505 3520 3534 3549 3564 3578 3593 58000 3608 3622 3637 3651 3666 3681 3695 3710 3724 3739 59000 3753 3768 3782 3797 3811 3826 3840 3854 3869 3883 60000 3898 3912 3926 3941 3955 3969 3984 3998 4012 4027 61000 4041 4055 4070 4084 4098 4112 4126 4141 4155 4169 62000 4183 4197 4212 4226 4240 4254 4268 4282 4296 4310 63000 4324 4338 4352 4366 4381 4395 4409 4423 4437 4451 64000 4465 4478 4492 4506 4520 4534 4548 4562 4576 4590 65000 4604 4617 4631 4645 4659 4672 4686 4700 4714 4728 66000 4741 4755 4769 4782 4796 4810 4823 4837 4851 4864 67000 4878 4892 4905 4919 4932 4946 4959 4973 4987 5000 NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMIT A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMIT B) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMIT C) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMIT NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES A) INCREASE FUEL REQUIRED BY 0.5 PERCENT PER 10 DEGREES C ABOVE ISA B) DECREASE FUEL REQUIRED BY 0.5 PERCENT PER 10 DEGREES C BELOW ISA C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISA Low-Level Cruise Pressure Altitude 21,000 ft FIGURE 033-36 033 PICTURE SUPPLEMENTS 127 © 2008
AVIATIONEXAM.com 0.74 M/250 KIAS (Economy) Descent Economy Descent PRESS. ALT. ft TIME min FUEL kg AIR DISTANCE TRAVELLED NM LANDING WEIGHT kg 35,000 45,000 55,000 65,000 75,000 37,000 23 295 98 109 114 114 110 35,000 22 290 94 105 110 110 106 33,000 21 285 89 99 103 103 101 31,000 20 280 83 93 97 98 95 29,000 19 275 78 87 91 91 89 27,000 19 270 73 81 85 85 83 25,000 18 260 68 75 79 79 77 23,000 16 255 63 69 72 73 71 21,000 15 245 58 64 66 67 66 19,000 14 235 53 58 60 61 60 17,000 13 225 48 52 54 55 54 15,000 12 215 43 46 48 49 48 10,000 9 185 30 32 33 34 33 5,000 6 140 18 18 18 18 18 3,700 5 130 14 14 14 14 14 0.70 M/280/250 KIAS (Turbulence Penetration) Descent Turbulence Penetration Descent PRESS. ALT. ft TIME min FUEL kg AIR DISTANCE TRAVELLED NM LANDING WEIGHT kg 35,000 45,000 55,000 65,000 75,000 37,000 21 280 88 100 107 110 109 35,000 20 275 84 96 102 105 105 33,000 20 275 80 91 98 101 101 31,000 19 270 76 86 93 96 96 29,000 18 265 72 82 88 91 92 27,000 17 260 69 78 84 87 87 25,000 17 255 64 73 78 80 81 23,000 16 250 60 67 72 74 74 21,000 15 240 55 62 66 68 68 19,000 14 230 51 57 60 62 62 17,000 13 225 46 52 55 56 56 15,000 12 215 42 46 49 50 50 10,000 9 185 30 32 33 34 33 5,000 6 140 18 18 18 18 18 3,700 5 130 14 14 14 14 14 FIGURE 033-37 033 PICTURE SUPPLEMENTS 128 © 2008
AVIATIONEXAM.com Non-Normal Operation Gear Down Ferry Flight REF LINE REF LINE PRESSURE ALTITUDE 1000 ft BASED ON: 220 KIAS CLIMB 220 KIAS DESCENT 30 40 50 60 TRIP TIME hr 0 1 2 3 4 20 10 0 -10 ISA DEV °C TRIP DISTANCE NM LANDING WEIGHT 1000 kg 0 3 4 5 6 7 8 9 FUEL REQUIRED 1000 kg 1 2 10 11 12 15 14 13 100 0 100 HEAD TAIL WIND kt 50 50 200 400 600 800 1000 0 2824 20 161412108 28242016141210 8 28 8 PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft REF LINE FIGURE 033-38
033 PICTURE SUPPLEMENTS 129 © 2008 AVIATIONEXAM.com Speed M/KIAS Div. Wt 1000 kg TIME MINUTES 60 70 80 90 100 110 120 130 140 150 160 170 180 190 200 35 406 472 539 605 672 738 805 871 938 1004 1071 1137 1204 1271 1337 40 402 467 533 598 663 729 794 860 925 990 1056 1121 1187 1252 1318 45 397 462 526 590 654 718 782 846 910 975 1039 1103 1167 1231 1295 .70/280 50 392 454 517 580 642 705 768 830 893 956 1018 1081 1144 1207 55 385 446 507 568 630 691 752 813 875 936 997 1058 1119 1181 1242 60 377 437 497 557 616 676 736 796 855 915 975 1035 1094 1154 1214 65 369 427 486 544 602 660 718 776 835 893 951 1009 1067 1125 1183 70 363 419 476 532 589 645 702 758 815 871 928 985 1041 1098 1154 35 412 478 545 612 678 745 811 878 945 1011 1078 1145 1211 1278 1345 40 409 474 540 606 672 737 803 869 935 1000 1066 1132 1198 1263 1329 45 404 469 533 598 663 727 792 856 921 986 1050 1115 1180 1244 1309 .74/290 50 400 463 526 590 653 717 780 844 907 970 1034 1097 1161 1224 55 393 455 517 579 641 704 766 828 890 952 1014 1077 1139 1201 1263 60 386 447 508 568 629 690 751 812 872 933 994 1055 1116 1176 1237 65 378 437 497 556 615 675 734 793 853 912 971 1031 1090 1149 1209 70 372 430 488 546 603 661 719 777 835 893 950 1008 1066 1124 1182 35 415 482 548 615 681 748 814 881 948 1014 1081 1147 1214 1280 1347 40 413 479 545 611 677 743 810 876 942 1008 1074 1140 1206 1272 1338 45 410 476 541 607 672 737 803 868 933 999 1064 1130 1195 1260 1326 .74/310 50 407 472 536 601 665 730 794 859 923 988 1052 1116 1181 1245 55 402 466 529 592 656 719 783 846 908 973 1036 1100 1163 1226 1290 60 397 459 521 583 646 708 770 833 895 957 1019 1082 1144 1206 1269 65 391 452 513 574 635 696 757 818 879 940 1002 1063 1124 1185 1246 70 385 445 505 565 625 685 744 804 864 924 984 1044 1103 1163 1223 35 416 482 548 614 680 746 811 877 943 1009 1075 1141 1207 1273 1339 40 415 481 547 613 678 744 810 875 941 1007 1072 1138 1204 1270 1335 45 414 480 545 610 676 741 806 871 937 1002 1067 1133 1198 1263 1328 .74/330 50 412 477 542 607 671 736 801 865 930 995 1059 1124 1189 1254 55 408 472 536 600 664 728 792 856 920 984 1048 1112 1176 1240 1304 60 404 467 530 593 656 719 783 846 909 972 1035 1098 1161 1224 1287 65 399 461 523 586 648 710 772 834 896 958 1020 1082 1144 1207 1269 70 395 457 518 579 640 701 762 823 884 945 1006 1067 1128 1190 1251 35 368 428 488 548 608 668 728 787 847 906 965 1024 1083 1141 1200 40 372 433 493 554 614 674 735 794 854 914 973 1032 1092 1151 1209 45 376 437 497 558 619 679 739 799 859 919 979 1038 1097 1157 1216 LRC 50 379 440 501 561 622 682 742 803 862 922 982 1041 1101 1160 1219 55 380 441 502 562 623 683 743 803 863 922 982 1041 1100 1159 1218 60 381 442 503 563 624 684 744 804 863 923 982 1041 1100 1159 1218 65 381 442 503 563 623 683 742 802 861 921 980 1038 1097 1156 1214 70 383 444 504 564 623 683 742 802 860 919 978 1036 1094 1152 1210 ISA BASED ON DRIFTDOWN STARTING AT OR NEAR OPTIMUM ALTITUDE Area of Operation Diversion Distance One Engine Inoperative FIGURE 033-39 033 PICTURE SUPPLEMENTS 130 © 2008 AVIATIONEXAM.com In-Flight Diversion (LRC) One Engine Inoperative
1269
1288
1310
1318
20 10 0 -10 ISA DEV °C 100 0 100 HEAD TAIL WIND kt 50 50 DISTANCE FROM POINT OF DIVERSION TO ALTERNATE NM 0 400 800 1200 1600 30 40 50 60 70 WEIGHT AT POINT OF DIVERSION 1000 kg INCLUDES APU FUEL BURN BASED ON 0.74 / 250 DESCENT 2 4 6 8 10 12 14 FUEL REQUIRED 1000 kg REF LINE REF LINE 0 1 2 3 4 5 DIVERSION TIME hr 2622181410 6 26 22 18 14 10 6 26 6 PRESSURE ALTITUDE 1000 ft ONE ENGINE INOPERATIVE REF LINE PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft FIGURE 033-40 033 PICTURE SUPPLEMENTS 131 © 2008 AVIATIONEXAM.com
Fuel Tankering (LRC and 0.74 M) 29 33 35 37 SURPLUS FUEL BURN % 5 10 15 20 25 0 0 1000 2000 TRIP DISTANCE NM 3000 LANDING WEIGHT (WITHOUT TANKERED FUEL) 75 85 95 105 115 35 40 45 50 lb kg 1000 LONG RANGE CRUISE REF LINE PRESSURE ALTITUDE 1000 ft 5 10 15 20 25 0 0 1000 2000 TRIP DISTANCE NM 3000 LANDING WEIGHT (WITHOUT TANKERED FUEL) 75 85 95 105 115 35 40 45 50 lb kg 1000 REF LINE 29 33 3537 PRESSURE ALTITUDE 1000 ft 0.74 MACH SURPLUS FUEL BURN % FIGURE 033-41 033 PICTURE SUPPLEMENTS 132 © 2008 AVIATIONEXAM.com
Fuel Price Differential 0 5 10 15 20 25 30 SURPLUS FUEL BURNOFF % 50 75 100 125 150 175 200 BREAK-EVEN FUEL PRICE DESTINATION AIRPORT CENTS / GALLON 175 150 125 100 75 50 FUEL PRICE AT DEPARTURE AIRPORT CENTS/GALLON FIGURE 033-42 033 PICTURE SUPPLEMENTS 133 © 2008 AVIATIONEXAM.com Optimum Aircraft Weight Air Distance Fuel Price Ratio 500 NM 1000 NM 1500 NM 2000 NM 2500 NM 3000 NM 3500 NM 4000 NM 4500 NM 5000 NM 160 170 180 190 200 210 360 380 400 420 440 460 (1000 lbs) (1000 kg) 0.98 0.97 0.96 0.95 0.94 0.93 0.92 0.91 0.90 0.89 0.88 0.87 0.86 0.85 0.84
0.83 FL350 FIGURE 033-43 033 PICTURE SUPPLEMENTS 134 © 2008 AVIATIONEXAM.com Optimum Aircraft Weight Air Distance Fuel Price Ratio 500 NM 1000 NM 1500 NM 2000 NM 2500 NM 3000 NM 3500 NM 4000 NM 4500 NM 5000 NM 160 170 180 190 200 210 360 380 400 420 440 460 (1000 lbs) (1000 kg) 0.99 0.98 0.97 0.95 0.94 0.93 0.92 0.91 0.90 0.89 0.88 0.87 0.86 0.96 FL310 FIGURE 033-44 033 PICTURE SUPPLEMENTS 135 © 2008 AVIATIONEXAM.com 410 390 370 350 330 160 170 180 190 200 210 220 230 240 360 380 400 420 440 460 480 500 520 FL WEIGHT (x 1000 kg) M.80 (x 1000 lbs) 410 390 370 350 330
160 170 180 190 200 210 220 230 240 360 380 400 420 440 460 500 520 FL WEIGHT (x 1000 kg) (x 1000 lb) 310 MAX ALT (ISA+10) MAX ALT (ISA+20) OPT ALT ALL TEMP. MAX ALT (ISA+15) n = 1.4g n = 1.3g MAX AND OPT ALT (ISA+20) OPT ALT (. ISA+15) MAX ALT (ISA+15) MAX ALT (. ISA+10) n = 1.4g n = 1.3g 480 M.80 FIGURE 033-45 033 PICTURE SUPPLEMENTS 136 © 2008 AVIATIONEXAM.com 410 390 370 350 330 160 170 180 190 200 210 220 FL WEIGHT (x 1000 kg) (x 1000 lb) 310 LONG RANGE 410 390 370 350 330 160 170 180 190 200 210 220 FL WEIGHT (x 1000 kg) (x 1000 lb) 310 M.84 MAX AND OPT ALT (ISA+20) MAX ALT (ISA+15) OPT ALT ALL TEMP. n=1.3g n=1.4g MAX ALT (.ISA+10) OPT ALT(ISA+10) (ISA+15) MAX ALT (.ISA+10) MAX ALT (ISA+15) MAX ALT (ISA+20) 360 380 400 420 440 460 480 360 380 400 420 440 460 480 FIGURE 033-46
230 240
230 240
500 520 500 520
033 PICTURE SUPPLEMENTS 137 © 2008 AVIATIONEXAM.com GROUND DIST (NM) +150 +100 +50 0 ..50 ..100 ..150 10 8 8 9 10 11 13 15 20 15 17 18 20 22 25 29 30 23 25 27 30 34 38 44 40 30 33 36 40 45 51 59 50 38 41 45 50 56 63 73 100 76 83 90 100 112 127 146 200 152 165 181 200 224 254 293 300 228 248 271 300 335 381 439 400 304 330 362 400 447 507 586 500 380 413 452 500 559 634 732 1000 759 825 904 1000 1118 1268 1465 1500 1139 1238 1357 1500 1677 1903 2197 2000 1518 1651 1809 2000 2237 2537 2930 2500 1898 2063 2261 2500 2796 3171 3662 3000 2277 2476 2713 3000 3355 3805 4395 3500 2657 2889 3165 3500 3914 4439 5127 4000 3036 3302 3617 4000 4473 5073 5860 4500 3416 3714 4070 4500 5032 5708 6592 5000 3795 4127 4522 5000 5591 6342 7324 5500 4175 4540 4974 5500 6151 6976 8057 6000 4555 4952 5426 6000 6710 7610 8789 6500 4934 5365 5878 6500 7269 8244 9522 7000 5314 5778 6330 7000 7828 8878 10254 7500 5693 6190 6783 7500 8387 9513 10987 8000 6073 6603 7235 8000 8946 10147 11719 8500 6452 7016 7687 8500 9506 10781 12451 9000 6832 7428 8139 9000 10065 11415 13184 9500 7211 7841 8591 9500 10624 12049 13916 10000 7591 8254 9043 10000 11183 12683 14649 M.82 AIR..DISTANCE..(NM) TAIL..WIND HEAD..WIND WIND..COMPONENT..(KTS) FIGURE 033-47 033 PICTURE SUPPLEMENTS 138 © 2008 AVIATIONEXAM.com GROUND DIST (NM) +150 +100 +50 0 ..50 ..100 ..150 10 8 8 9 10 11 13 15 20 15 16 18 20 22 25 29 30 23 25 27 30 34 38 44 40 30 33 36 40 45 51 59 50 38 41 45 50 56 64 74 100 76 82 90 100 112 127 147 200 151 165 181 200 224 254 295 300 227 247 271 300 336 382 442 400 303 330 361 400 448 509 589 500 379 412 452 500 560 636 736 1000 757 824 903 1000 1120 1272 1473
1500 1136 1236 1355 1500 1680 1908 2209 2000 1514 1648 1807 2000 2240 2544 2945 2500 1893 2059 2258 2500 2799 3180 3681 3000 2271 2471 2710 3000 3359 3817 4418 3500 2650 2883 3162 3500 3919 4453 5154 4000 3028 3295 3613 4000 4479 5089 5890 4500 3407 3707 4065 4500 5039 5725 6627 5000 3785 4119 4517 5000 5599 6361 7363 5500 4164 4531 4968 5500 6159 6997 8099 6000 4542 4943 5420 6000 6719 7633 8836 6500 4921 5354 5872 6500 7279 8269 9572 7000 5299 5766 6324 7000 7839 8905 10308 7500 5678 6178 6775 7500 8398 9541 11044 8000 6056 6590 7227 8000 8958 10177 11781 8500 6435 7002 7679 8500 9518 10814 12517 9000 6813 7414 8130 9000 10078 11450 13253 9500 7192 7826 8582 9500 10638 12086 13990 10000 7570 8238 9043 10000 11198 12722 14726 LONG..RANGE..CRUISE..ABOVE..FL250 AIR..DISTANCE..(NM) TAIL..WIND WIND..COMPONENT..(KTS) HEAD..WIND FIGURE 033-48 033 PICTURE SUPPLEMENTS 139 © 2008 AVIATIONEXAM.com DIS. FL310 FL350 FL390 FL330 FL370 FL410 3537 3531 11 0.39 0.39 4764 4684 4622 4579 4555 4548 13 16 0.51 0.52 0.52 0.52 0.52 0.52 5993 5840 5711 5609 5536 5489 16 18 1.04 1.04 1.04 1.05 1.05 1.05 7225 6998 6803 6642 6519 6434 18 21 1.16 1.17 1.17 1.17 1.17 1.17 8460 8160 7898 7679 7506 7383 20 24 1.29 1.29 1.30 1.30 1.30 1.30 9698 9323 8996 8718 8496 8335 22 27 1.41 1.42 1.43 1.43 1.43 1.43 10938 10490 10096 9759 9490 9291 25 1.54 1.55 1.55 1.56 1.56 1.56 12180 11659 11199 10804 10486 10251 2.06 2.07 2.08 2.08 2.09 2.09 13425 12831 12305 11851 11485 11213 2.19 2.20 2.21 2.21 2.21 2.21 14673 14005 13413 12901 12487 12180 2.31 2.32 2.33 2.34 2.34 2.34 15924 15182 14525 13954 13492 13149 2.44 2.45 2.46 2.47 2.47 2.47 17178 16363 15640 15010 14501 14123 2.56 2.58 2.59 3.00 3.00 3.00 18434 17546 16758 16070 15514 15101 3.09 3.10 3.12 3.12 3.12 3.12 19693 18732 17879 17132 16530 16083 3.21 3.23 3.24 3.25 3.25 3.25 20955 19921 19003 18197 17550 17069 3.34 3.36 3.37 3.38 3.38 3.38
18 22 25 29 32 29 36 27 32 40 29 35 44 32 38 48 34 41 51 37 44 55 39 47 59 42 50 64 45 53 68
22221 21114 20129 19266 18574 18060 47 56 72 3.46 3.48 3.50 3.51 3.51 3.51 23489 22310 21260 20337 19601 19054 50 59 77 3.59 4.01 4.03 4.04 4.04 4.04 24761 23508 22394 21412 20632 20052 53 63 82 4.11 4.13 4.15 4.16 4.16 4.16 26035 24710 23531 22491 21667 21067 56 66 87 4.24 4.26 4.28 4.29 4.29 4.29 27311 25914 24671 23573 22707 22078 58 69 92 4.37 4.39 4.41 4.42 4.42 4.42 28591 27122 25814 24658 23750 23093 61 73 97 4.49 4.51 4.53 4.55 4.55 4.55 29875 28333 26960 25746 24796 24113 64 76 102 5.02 5.04 5.06 5.07 5.08 5.08 31161 29546 28110 26837 25846 25136 67 79 107 5.14 5.16 5.19 5.20 5.20 5.20 32450 30764 29263 27932 26920 26165 70 82 113 5.27 5.29 5.32 5.33 5.33 5.33 33742 31985 30419 29030 27982 27198 73 86 118 5.39 5.42 5.44 5.46 5.46 5.46 35038 33209 31577 30131 29047 28237 75 90 122 5.52 5.54 5.57 5.59 5.59 5.59 AIR CORRECTION ON FLIGHT LEVEL ANTI ICING OFF CG = 37,0 % TIME (H.MIN) NORMAL AIR CONDITIONING FLIGHT PLANNING FROM BREAKE RELEASE TO LANDING CLIMB: 250KTS/300KTS/M.80 - CRUISE: M.82 - DESCENT: M.82/300KTS/250KTS IMC PROCEDURE: 240 KG (6 MIN) REF. LANDING WEIGHT = 140.000 KG ISA FUEL CONSUMED (KG) FUEL CONSUMPTION (KG/1.000 KG) (NM) 1400 1500 200 300 400 500 600 310 330 350 370 390 410 1600 1700 1800 700 800 900 1000 1100 1200 1300 1900 2000 2100 2200 2300 ..FUEL..=..+1,5..% ..FUEL = +7 % TOTAL ANTI ICE ON ICE..ON 2400
2500 CARGO COOL ON ..FUEL = -0,4 % ..FUEL = +1 % 2600 2700 PACK FLOW LO PACK FLOW HI OR/AND ENGINE..ANTI FIGURE 033-49 033 PICTURE SUPPLEMENTS 140 © 2008 AVIATIONEXAM.com DIS. FL310 FL350 FL390 FL330 FL370 FL410 36336 34437 32738 31237 30117 29281 78 94 127 6.04 6.07 6.10 6.11 6.11 6.12 37638 35668 33903 32372 31191 30330 82 97 132 6.17 6.20 6.23 6.24 6.24 6.24 38942 36902 35072 33487 32269 31386 85 103 137 6.29 6.32 6.35 6.37 6.37 6.37 40249 38139 36243 34607 33351 32446 88 105 143 6.42 6.45 6.48 6.50 6.50 6.50 41560 39379 37453 35730 34439 33511 93 109 149 6.54 6.57 7.01 7.03 7.03 7.03 42874 40622 38634 36857 35532 34584 96 114 155 7.07 7.10 7.13 7.15 7.15 7.15 44192 41911 39819 37988 36628 35663 100 116 161 7.19 7.23 7.26 7.28 7.28 7.28 45514 43166 41008 39122 37729 36746 106 120 168 7.32 7.35 7.39 7.41 7.41 7.41 46839 44426 42201 40260 38835 37835 107 124 174 7.44 7.48 7.52 7.54 7.54 7.54 48219 45690 43398 41403 39944 38929 111 128 183 7.57 8.01 8.04 8.07 8.07 8.07 49556 46958 44600 42549 41060 40029 112 133 191 8.09 8.13 8.17 8.19 8.19 8.19 50897 48230 45805 43702 42181 41137 115 137 199 8.22 8.26 8.30 8.32 8.32 8.32 52241 49505 47014 44863 43306 42250 119 142 207 8.34 8.38 8.43 8.45 8.45 8.45 53588 50785 48228 46028 44438 43370 122 146 215 8.47 8.51 8.55 8.58 8.58 8.58 54940 52068 49446 47198 45577 44524 126 151 223 8.59 9.04 9.08 9.11 9.11 9.10* 56296 53355 50667 48374 46721 45690 130 156 230 9.12 9.16 9.21 9.23 9.23 9.23* 57657 54647 51892 49555 47872 46862 133 161 239 9.24 9.29 9.34 9.36 9.36 9.36* 59022 55943 53121 50739 49028 48040 137 166 247 9.37 9.41 9.46 9.49 9.49 9.49* 60391 57242 54355 51929 50190 49223 140 171 255 9.49 9.54 9.59 10.02 10.02 10.02* 61766 58545 55593 53123 51357 50411 144 176 262 10.02 10.07 10.12 10.15 10.15 10.14* 63144 59851 56836 54322 52530 51604 148 181 270 10.14 10.19 10.24 10.27 10.27 10.27* 64525 61162 58083 55527 53707 52803 152 186 277 10.27 10.32 10.37 10.40 10.40 10.40* 65911 62478 59335 56737 54917 54006 156 191 283
10.39 10.45 10.50 10.53 10.53 10.53* 67301 63798 60592 57952 56112 55217 160 196 291 10.52 10.57 11.03 11.06 11.06 11.06* 68696 65121 61854 59173 57312 56433 164 201 300 11.04 11.10 11.15 11.19 11.19 11.18* 70095 66449 63121 60400 58519 57654 167 207 309 11.17 11.23 11.28 11.31 11.31 11.31* AIR CORRECTION..ON FLIGHT..LEVEL ANTI..ICING..OFF CG..=..37,0..% TIME..(H.MIN) NORMAL..AIR..CONDITIONING FLIGHT..PLANNING..FROM..BREAKE..RELEASE..TO..LANDING CLIMB:..250KTS/300KTS/M.80......CRUISE:..M.82......DESCENT:..M.82/300KTS/250KTS IMC..PROCEDURE:..240..KG..(6..MIN) REF...LANDING..WEIGHT..=..140.000..KG ISA FUEL..CONSUMED..(KG) FUEL..CONSUMPTION (KG/1.000..KG) (NM) 4000 4100 2800 2900 3000 3100 3200 310 330 350 370 390 410 4200 4300 4400 3300 3400 3500 3600 3700 3800 3900 4500 4600 4700 4800 4900 ..FUEL..=..+1,5..% ..FUEL..=..+7..% TOTAL..ANTI..ICE..ON ICE..ON 5000 5100 CARGO..COOL..ON ..FUEL..=....0,4..% ..FUEL..=..+1..% 5200 5300 PACK..FLOW..LO PACK..FLOW..HI..OR/AND ENGINE..ANTI FIGURE 033-50 033 PICTURE SUPPLEMENTS 141 © 2008 AVIATIONEXAM.com WEIGHT TAS (1000 KG) (KTS)
0 18 35 53 70 88 105 123 140 157 356 0 3 6 9 12 15 18 21 23 26 175 192 210 227 245 262 279 297 314 331 359 29 32 35 38 41 44 47 50 53 55 349 366 383 400 418 435 452 469 487 504 361 58 61 64 67 70 73 75 78 81 84 521 538 556 573 590 607 624 641 658 676 362 87 90 93 95 98 101 104 107 110 113 693 710 727 744 761 778 795 812 829 846 362 115 118 121 124 127 129 132 135 138 141 863 880 897 914 931 948 965 982 999 1016 363 144 146 149 152 155 158 160 163 166 169 1033 1050 1067 1084 1100 1117 1134 1151 1168 172 174 177 180 183 185 188 191 194 197 1202 1218 1235 1252 1269 1269 1302 1319 1336 199 202 205 208 210 213 216 219 221 224 1369 1386 1403 1419 1436 1453 1469 1486 1503 227 230 232 235 238 241 243 246 249 251 1536 1553 1569 1586 1602 1619 1636 1652 1669 254 257 260 262 265 268 271 273 276 279 1702 1718 1735 1751 1768 1784 1801 1817 1834 281 284 287 289 292 295 298 300 303 306 1867 1883 1899 1916 1932 1949 1965 1981 1998 308 311 314 316 319 322 324 327 330 332 2031 2047 2063 2080 2096 2112 2128 2145 2161 335 338 340 343 346 348 351 354 356 359 2194 2210 2226 2242 2258 2275 2291 2307 2323 361 364 367 369 372 375 377 380 383 385 2356 2372 2388 2404 2420 2436 2452 2469 2485 388 390 393 396 398 401 403 406 409 411 3517 2533 2549 2565 2581 2597 2613 2629 2645 414 416 419 422 424 427 429 432 435 437 2677 2693 2709 2725 2741 2757 2773 2789 2805 440 442 445 448 450 453 455 458 460 463 3837 2853 2868 2884 2900 2916 2932 2948 2964 466 468 471 473 476 478 481 483 486 489 2995 3011 3027 3043 3058 3074 3090 3106 3121 491 494 496 499 501 504 506 509 511 514 3153 3169 3184 3200 3216 3231 3247 3263 3278 516 519 521 524 527 529 532 534 537 539 3310 3325 3341 3357 3372 3388 3403 3419 3434 542 544 547 549 552 554 557 559 562 564 3466 3481 3497 3512 3528 3543 3559 3574 3590 567 569 572 574 577 579 582 584 586 589 3621 3636 3652 3667 3682 3698 3713 3729 3744 591 594 596 599 601 604 606 609 611 614 3775 3790 3806 3821 3836 3852 3867 3882 3898 616 618 621 623 626 628 631 633 636 638 ..FUEL..=..+6..% ..FUEL..=....0,4..% PACK..FLOW..HI..OR/ AND..CARGO..COOL..ON ..FUEL..=..+1..% ENGINE..ANTI..ICE..ON ..FUEL..=..+1,5..% INTEGRATED CRUISE LR FL 250 PACK..FLOW..LO TOTAL..ANTI..ICE..ON DISTANCE ISA CG = 30,0 % ANTI-ICING OFF
1185 364 1352 365 1519 366 1685 366 1850 367 2014 368 2177 369 2339 369 2501 370 2661 371 2821 371 2979 372 3137 373 3294 373 3450 374 3605 375 3760 375 3913 376
MAX. CRUISE THRUST LIMITS NORMAL AIR CONDITIONING 1.2 1.4 1.6 1.8 TIME (MIN) (NM) 0 .2 .4 .6 .8 1.0 136 126 128 130 132 134 158 138 140 142 144 146 148 150 152 154 156 172 160 162 164 166 168 170 FIGURE 033-51 033 PICTURE SUPPLEMENTS 142 © 2008 AVIATIONEXAM.com WEIGHT TAS (1000 KG) (KTS) 0 22 43 65 87 108 130 151 173 194 377 0 3 7 10 14 17 21 24 27 31 216 237 259 280 302 323 344 366 387 408 385 34 37 41 44 47 51 54 57 60 64 430 451 472 493 514 536 557 578 599 620 392 67 70 73 77 80 83 86 89 93 96 641 662 683 704 725 746 767 788 809 829 400 99 102 105 108 112 115 118 121 124 127 850 871 892 913 933 954 975 995 1016 1037 411 130 133 136 139 142 145 148 151 154 157 1057 1078 1099 1119 1140 1160 1181 1201 1222 1242 160 163 166 169 172 175 178 180 183 186 1263 1283 1304 1324 1345 1365 1385 1406 1426 1446 189 192 195 198 201 204 207 210 213 215 1467 1487 1507 1528 1548 1568 1589 1609 1629 1649 218 221 224 227 230 233 236 239 241 244 1669 1690 1710 1730 1750 1770 1790 1810 1830 1850 247 250 253 256 259 261 264 267 270 273 1870 1890 1910 1930 1950 1970 1990 2010 2030 2050 276 278 281 284 287 290 292 295 298 301 2070 2090 2109 2129 2149 2169 2189 2208 2228 2248 304 306 309 312 315 318 320 323 326 329
418 420 421 423 425 427
2268 2287 2307 2327 2346 2366 2385 2405 2425 2444 429 331 334 337 340 342 345 348 351 353 356 2464 2483 2503 2522 2542 2561 2581 2600 2619 2639 431 359 361 364 367 370 372 375 378 380 383 2658 2678 2697 2716 2736 2755 2774 2793 2813 2832 434 386 388 391 394 396 399 402 404 407 410 2851 2870 2889 2909 2928 2947 2966 2985 3004 3023 437 412 415 418 420 423 425 428 431 433 436 3042 3062 3081 3100 3119 3138 3157 3175 3194 3213 439 439 441 444 446 449 452 454 457 459 462 3232 3251 3270 3289 3308 3327 3345 3364 3383 3402 441 464 467 470 472 475 477 480 482 485 487 3421 3439 3458 3477 3495 3514 3533 3551 3570 3589 442 490 493 495 498 500 503 505 508 510 513 3607 3626 3645 3663 3682 3700 3719 3737 3756 3774 444 515 518 520 523 525 528 530 533 535 538 3793 3811 3830 3848 3866 3885 3903 3922 3940 3958 446 540 543 545 548 550 553 555 558 560 563 3977 3995 4013 4031 4050 4068 4086 4104 4123 4141 448 565 567 570 572 575 577 580 582 585 587 4159 4177 4195 4213 4232 4250 4268 4286 4304 4322 450 589 592 594 597 599 601 604 606 609 611 4340 4358 4376 4394 4412 4430 4448 4466 4484 4502 451 614 616 618 621 623 625 628 630 633 635 4520 4538 4555 4573 4591 4609 4627 4645 4662 4680 453 637 640 642 644 647 649 652 654 656 659 ..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+6..% 168 170 172 PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON TOTAL..ANTI..ICE..ON AND..CARGO..COOL..ON 166 144 146 148 150 152 154 156 158 160 162 164 1.8 126 128 130 132 1.0 1.2 142 1.4 1.6 134 136 138 140 0 .2 .4 .6 .8 INTEGRATED CRUISE MAX. CRUISE THRUST LIMITS DISTANCE LR FL 350 NORMAL AIR CONDITIONING ISA (NM)
ANTI-ICING OFF CG = 37,0 % TIME (MIN) FIGURE 033-52 033 PICTURE SUPPLEMENTS 143 © 2008 AVIATIONEXAM.com WEIGHT TAS (1000 KG) (KTS) 5088 5107 5126 5144 5163 5182 5200 5219 5238 5256 459 665 668 670 673 675 678 680 682 685 687 5275 5293 5312 5330 5349 5367 5385 5404 5422 5441 459 690 692 695 697 699 702 704 707 709 711 5459 5477 5496 5514 5532 5551 5569 5587 5605 5623 459 714 716 719 721 723 726 728 731 733 735 5642 5660 5678 5696 5714 5732 5750 5768 5786 5804 459 738 740 742 745 747 750 752 754 757 759 5822 5840 5858 5875 5893 5911 5929 5947 5964 5982 459 761 764 766 768 771 773 775 778 780 782 6000 6018 6035 6053 6071 6088 6105 6119 6133 6151 459 785 787 789 791 794 796 798 800 802 804 6168 6186 6203 6220 6238 6255 6273 6290 6307 6325 459 807 809 811 813 816 818 820 822 825 827 6342 6359 6377 6394 6411 6429 6446 6463 6480 6497 459 829 832 834 836 838 841 843 845 847 850 6515 6532 6549 6566 6583 6600 6617 6635 6652 6669 459 852 854 856 859 861 863 865 868 870 872 6686 6703 6720 6737 6754 6771 6788 6805 6821 6838 459 874 876 879 881 883 885 888 890 892 894 6855 6872 6889 6906 6923 6940 6956 6973 6990 7007 459 896 899 901 903 905 907 910 912 914 916 7023 7040 7057 7073 7090 7107 7123 7140 7157 7173 459 918 921 923 925 927 929 931 934 936 938 7190 7206 7223 7239 7256 7272 7289 7305 7322 7338 459 940 942 944 947 949 951 953 955 957 960 7354 7371 7387 7403 7420 7436 7452 7468 7485 7501 459 962 964 966 968 970 972 974 977 979 981 7517 7533 7549 7566 7582 7598 7614 7630 7646 7662 459 983 985 987 989 991 993 996 998 1000 1002 7678 7694 7708 7720 7735 7751 7766 7782 7798 7814 459 1004 1006 1008 1010 1011 1013 1016 1018 1020 1022 7830 7846 7861 7877 7893 7909 7925 7940 7956 7972 461 1024 1026 1028 1030 1032 1034 1036 1038 1040 1042 7988 8003 8019 8035 8050 8066 8081 8097 8113 8128 461 1044 1046 1048 1050 1052 1054 1057 1059 1061 1063 8144 8159 8175 8191 8206 8222 8237 8253 8268 8284 461 1065 1067 1069 1071 1073 1075 1077 1079 1081 1083 8299 8315 8330 8345 8361 8376 8392 8407 8422 8438 461 1085 1087 1089 1091 1093 1095 1097 1099 1101 1103 8453 8468 8484 8499 8514 8529 8545 8560 8575 8590 461 1105 1107 1109 1111 1113 1115 1117 1119 1121 1123 8606 8621 8636 8651 8666 8681 8696 8712 8727 8742 461 1125 1127 1129 1131 1133 1135 1137 1138 1140 1142 8757 8772 8787 8802 8817 8832 8847 8862 8877 8892 461 1144 1146 1148 1150 1152 1154 1156 1158 1160 1162 ..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+7..% 216 218 PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON TOTAL..ANTI..ICE..ON AND..CARGO..COOL..ON
214 192 194 196 198 200 202 204 206 208 210 212 1.8 174 176 178 180 1.0 1.2 190 1.4 1.6 182 184 186 188 0 .2 .4 .6 .8 INTEGRATED CRUISE MAX. CRUISE THRUST LIMITS DISTANCE M.80 OPT FL NORMAL AIR CONDITIONING ISA (NM) ANTI-ICING OFF CG = 37,0 % TIME (MIN) FIGURE 033-53 033 PICTURE SUPPLEMENTS 144 © 2008 AVIATIONEXAM.com WEIGHT TAS (1000 KG) (KTS) 4710 4724 4738 4755 4772 4789 4806 4823 587 588 590 592 594 596 599 601 603 605 4874 4891 4908 4925 4942 4959 4975 4992 607 609 611 613 615 618 620 622 624 626 5043 5059 5076 5093 5109 5126 5143 5159 628 630 632 634 636 638 640 643 645 647 5209 5226 5242 5259 5276 5292 5309 5325 649 651 653 655 657 659 661 663 665 667 5375 5391 5407 5424 5440 5457 5473 5489 669 671 673 675 677 680 682 684 686 688 5538 5554 5571 5587 5603 5619 5635 5652 690 692 694 696 698 700 702 704 706 708 5700 5716 5732 5748 5764 5780 5796 5812 710 712 714 716 718 720 722 724 726 770 5860 5876 5892 5907 5923 5939 5955 5971 730 732 734 736 738 740 742 744 746 747 6018 6034 6049 6065 6081 6096 6112 6127 749 751 753 755 757 759 761 763 765 767 6174 6189 6202 6215 6230 6245 6261 6276 769 771 772 774 776 778 780 782 783 785 6322 6338 6353 6368 6384 6399 6414 6430 787 789 791 793 795 797 799 801 802 804 6476 6491 6506 6521 6536 6552 6567 6582
4840 4857 482 5009 5026 482 5176 5193 482 5342 5358 482 5505 5522 482 5668 5684 482 5828 5844 482 5986 6002 482 6143 6159 482 6292 6307 482 6445 6460 484 6597 6612 484
806 808 810 812 814 816 818 819 821 823 6627 6642 6657 6673 6688 6703 6718 6733 6748 6763 484 825 827 829 831 833 834 836 838 840 842 6778 6793 6808 6823 6838 6852 6867 6882 6897 6912 484 844 846 847 849 851 853 855 857 858 860 6927 6942 6956 6971 6986 7001 7016 7030 7045 7060 484 862 864 866 868 870 871 873 875 877 879 7074 7089 7104 7118 7133 7148 7162 7177 7191 7206 484 880 882 884 886 888 890 891 893 895 897 7221 7235 7249 7264 7278 7293 7307 7322 7336 7351 484 899 900 902 904 906 908 909 911 913 915 7365 7379 7394 7408 7422 7437 7451 7465 7479 7494 484 916 918 920 922 924 925 927 929 931 932 7508 7522 7536 7550 7565 7577 7589 7601 7615 7629 484 934 936 938 939 941 943 944 946 947 949 7643 7657 7671 7685 7699 7713 7727 7741 7755 7769 489 951 953 954 956 958 960 961 963 965 966 7783 7797 7811 7825 7839 7853 7867 7881 7895 7908 489 968 970 972 973 975 977 978 980 982 983 7922 7936 7950 7964 7978 7991 8005 8019 8033 8046 489 985 987 989 990 992 994 995 997 999 1000 8060 8074 8088 8101 8115 8129 8142 8156 8170 8183 489 1002 1004 1005 1007 1009 1011 1012 1014 1016 1017 AND..CARGO..COOL..ON ..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+7..% TOTAL..ANTI..ICE..ON 204 206 208 210 212 214 216 218 PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON 202 180 182 184 186 188 190 192 194 196 198 200 1.4 1.6 1.8 174 176 178 CG = 37,0 % TIME (MIN) 0 .2 .4 .6 .8 1.0 1.2 INTEGRATED CRUISE MAX. CRUISE THRUST LIMITS DISTANCE M.84 OPT FL NORMAL AIR CONDITIONING ISA (NM) ANTI-ICING OFF FIGURE 033-54 033 PICTURE SUPPLEMENTS
145 © 2008 AVIATIONEXAM.com WEIGHT TAS (1000 KG) (KTS) 0 22 45 67 89 112 134 156 178 200 418 0 3 6 10 13 16 19 22 26 29 223 245 267 289 311 333 355 377 399 42 419 32 35 38 41 45 48 51 54 57 60 443 465 487 509 531 553 575 597 619 640 421 63 67 70 73 76 79 82 85 88 91 662 684 706 727 749 771 793 814 836 857 424 95 98 101 104 107 110 113 116 119 122 879 901 922 944 965 987 1008 1030 1051 1073 426 125 128 131 134 137 140 143 146 149 152 1094 1115 1137 1158 1180 1201 1222 1243 1265 1286 428 155 158 161 164 167 170 173 176 179 182 1307 1328 1349 1371 1392 1413 1434 1455 1476 1497 431 185 188 191 194 197 200 203 206 209 211 1518 1539 1560 1581 1602 1623 1644 1665 1686 1707 434 214 217 220 223 226 229 232 235 238 240 1728 1748 1769 1790 1811 1831 1852 1873 1894 1914 436 243 246 249 252 255 258 260 263 266 269 1935 1956 1976 1997 2017 2038 2059 2079 2100 2120 439 272 275 277 280 283 286 289 291 294 297 2141 2161 2181 2202 2222 2243 2263 2283 2304 2324 441 300 303 305 308 311 314 316 319 322 325 2344 2365 2385 2405 2425 2446 2466 2486 2506 2526 443 327 330 333 336 338 341 344 347 349 352 2547 2567 2587 2607 2627 2647 2667 2687 2707 2727 445 355 357 360 363 366 368 371 374 376 379 2747 2767 2787 2807 2827 2846 2866 2886 2906 2926 447 382 384 387 390 392 395 398 400 403 406 2946 2965 2985 3005 3025 3044 3064 3084 3103 3123 449 408 411 414 416 419 422 424 427 429 432 3143 3162 3182 3201 3221 3240 3260 3279 3299 3318 451 435 437 440 442 445 448 450 453 455 458 3338 3357 3377 3396 3416 3435 3454 3474 3493 3512 452 461 463 466 468 471 473 476 479 481 484 3532 3551 3570 3590 3609 3628 3647 3666 3686 3705 454 486 489 491 494 496 499 501 504 507 509 3724 3743 3762 3781 3800 3820 3839 3858 3877 3896 456 512 514 517 519 522 524 527 529 532 534 3915 3934 3953 3972 3991 4009 4028 4047 4066 4085 458 537 539 542 544 547 549 551 554 556 559 4104 4123 4141 4160 4179 4198 4217 4235 4254 4273 459 561 564 566 569 571 574 576 579 581 583 4291 4310 4329 4347 4366 4385 4403 4422 4440 4459 460 586 588 591 593 596 598 600 603 605 608 4477 4496 4514 4533 4551 4570 4588 4607 4625 4643 461 610 612 615 617 620 622 625 627 629 632 4662 4680 4699 4717 4735 4753 4772 4790 4808 4826 462 634 636 639 641 644 646 648 651 653 655 ..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+8..% 168 170 172 PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON TOTAL..ANTI..ICE..ON AND..CARGO..COOL..ON 166
144 146 148 150 152 154 156 158 160 162 164 1.8 126 128 130 132 1.0 1.2 142 1.4 1.6 134 136 138 140 0 .2 .4 .6 .8 INTEGRATED CRUISE MAX. CRUISE THRUST LIMITS DISTANCE LR FL 370 NORMAL AIR CONDITIONING ISA (NM) ANTI-ICING OFF CG = 37,0 % TIME (MIN) FIGURE 033-55 033 PICTURE SUPPLEMENTS 146 © 2008 AVIATIONEXAM.com WEIGHT TAS (1000 KG) (KTS) 4845 4863 4881 4899 4917 4936 4954 4972 658 660 662 665 667 670 672 674 677 879 5026 5044 5062 5080 5098 5116 5134 5152 881 684 686 688 691 693 695 698 700 702 5206 5224 5241 5259 5277 5295 5313 5331 705 707 709 711 714 716 718 721 723 725 5384 5402 5419 5437 5455 5473 5490 5508 728 730 732 734 737 739 741 743 746 748 5561 5578 5596 5613 5631 5649 5666 5684 750 753 755 757 759 762 764 766 768 774 5756 5753 5771 5788 5806 5823 5840 5858 773 775 777 780 782 784 786 789 791 793 6010 5927 5944 5962 5879 5996 6013 6031 795 797 800 802 804 806 809 811 813 815 6082 6099 6116 6133 6151 6168 6185 6202 817 820 822 824 826 828 831 833 835 837 6253 6270 6287 6304 6321 6338 6355 6372 839 842 844 846 848 850 852 855 857 859 6422 6439 6456 6473 6490 6506 6523 6540 861 863 865 869 870 872 874 876 878 881 6590 6607 6623 6640 6857 6673 6690 6707 883 885 887 889 891 893 895 898 900 902 6757 6773 6790 6806 6823 6839 6856 6872 904 906 908 910 912 915 917 919 921 923
4990 5008 463 5170 5188 464 5348 5366 465 5525 5543 465 5701 5719 466 5875 5892 466 6048 6065 466 6219 6236 467 6388 6405 467 6557 6573 467 6723 6740 468 6888 6905 468
6921 6930 6954 6070 6987 7003 1011 7035 7052 7068 468 925 927 929 931 933 936 938 940 942 944 7084 7100 7117 7133 7149 7165 7181 7197 7213 7219 469 946 948 950 952 954 956 958 960 962 964 7245 7261 7277 7293 7309 7325 7341 7357 7373 7389 470 967 969 971 973 975 977 979 981 983 985 7405 7420 7436 7452 7468 7484 7490 7515 7531 7546 471 987 989 991 993 995 997 999 1001 1003 1005 7562 7578 7593 7609 7624 7640 7656 7671 7687 7702 471 1007 1009 1011 1013 1015 1017 1019 1021 1023 1025 7718 7733 7749 7764 7779 7795 7810 7825 7841 7856 471 1027 1029 1031 1033 1035 1037 1039 1041 1042 1044 7871 7887 7902 7917 7932 7948 7963 7978 7993 8008 471 1046 1048 1050 1052 1054 1056 1058 1060 1062 1064 8023 8038 8053 8068 8083 8098 8113 8128 8143 8158 471 1066 1068 1070 1071 1073 1075 1077 1079 1081 1083 8173 8188 8203 8217 8232 8747 8262 8271 8291 8306 471 1085 1087 1089 1090 1092 1094 1096 1098 1100 1102 8321 8335 8350 8365 8379 471 1104 1105 1107 1109 1111 AND..CARGO..COOL..ON ..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+6..% TOTAL..ANTI..ICE..ON 204 206 208 210 212 214 216 218 PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON 202 180 182 184 186 188 190 192 194 196 198 200 1.4 1.6 1.8 174 176 178 CG = 37,0 % TIME (MIN) 0 .2 .4 .6 .8 1.0 1.2 INTEGRATED CRUISE MAX. CRUISE THRUST LIMITS DISTANCE LR FL 370 NORMAL AIR CONDITIONING ISA (NM) ANTI-ICING OFF FIGURE 033-56 033 PICTURE SUPPLEMENTS 147 © 2008 AVIATIONEXAM.com
WEIGHT TAS (1000 KG) (KTS) 4555 4572 4589 4607 4624 4641 4658 4675 4692 4710 444 672 674 677 679 681 684 686 688 690 693 4727 4744 4761 4778 4795 4812 4829 4846 4863 4880 446 695 697 700 702 704 707 709 711 713 716 4897 4914 4931 4948 4965 4982 4999 5016 5033 5050 448 718 720 723 725 727 729 732 734 736 738 5067 5084 5101 5117 5134 5151 5168 5185 5201 5218 449 741 743 745 747 750 752 754 756 759 761 5235 5252 5268 5285 5302 5319 5335 5352 5369 5385 451 763 765 768 770 772 774 776 779 781 783 5402 5419 5435 8452 5468 5485 5501 5518 5535 5551 453 785 787 790 792 794 796 798 801 803 805 5568 5584 5601 5617 5634 5650 5666 5683 5699 5716 454 807 809 812 814 816 818 820 822 825 827 5732 5749 5765 5781 5798 5814 5830 5847 5863 5879 456 829 831 833 835 837 840 842 844 846 848 5895 5912 5928 5944 5960 5977 5993 6009 6025 6042 457 850 852 855 857 859 861 863 865 867 869 6058 6074 6090 6106 6122 6138 6154 6171 6187 6203 458 872 874 876 878 880 882 884 886 888 891 6219 6235 6251 6267 6283 6299 6315 6331 6347 6363 460 893 895 897 899 901 903 905 907 909 911 6379 6395 6411 6427 6442 6458 6474 6490 6506 6522 461 914 916 918 920 922 924 926 928 930 932 6538 6553 6569 6585 6601 6617 6632 6648 6664 6680 463 934 936 938 940 942 944 946 948 950 953 6695 6711 6727 6743 6758 6774 6790 6805 6821 6836 464 955 957 959 961 963 965 967 969 971 973 6852 6868 6883 6899 6914 6930 6946 6961 6977 6992 465 975 977 979 981 983 985 987 989 991 993 7008 7023 7039 7054 7070 7085 7100 7116 7131 7147 466 995 997 999 1001 1003 1005 1007 1009 1011 1013 7162 7177 7193 7208 7224 7239 7254 7269 7285 7300 467 1015 1017 1019 1021 1023 1025 1027 1029 1030 1032 7315 7331 7346 7361 7376 7392 7407 7422 7437 7452 468 1034 1036 1038 1040 1042 1044 1046 1048 1050 1052 7467 7483 7498 7513 7528 7543 7558 7573 7588 7603 468 1054 1056 1058 1060 1062 1064 1066 1067 1069 1071 7618 7633 7648 7664 7679 7694 7708 7723 7738 7753 469 1073 1075 1077 1079 1081 1083 1085 1087 1089 1091 7768 7783 7798 7813 7828 7843 7858 7873 7887 7902 470 1092 1094 1096 1098 1100 1102 1104 1106 1108 1110 7917 7932 7947 7962 7976 7991 8006 8021 8035 8050 470 1111 1113 1115 1117 1119 1121 1123 1125 1126 1128 8065 8080 8094 8109 8124 8138 8153 8168 8182 8197 471 1130 1132 1134 1136 1138 1140 1141 1143 1145 1147 AND CARGO COOL ON .FUEL = -0,4 % .FUEL = +1 % .FUEL = +1,5 % .FUEL = +6 % TOTAL ANTI ICE ON 204 206 208 210 212 214 216 218 PACK FLOW LO PACK FLOW HI OR/ ENGINE ANTI ICE ON
202 180 182 184 186 188 190 192 194 196 198 200 1.4 1.6 1.8 174 176 178 CG = 37,0 % TIME (MIN) 0 .2 .4 .6 .8 1.0 1.2 INTEGRATED CRUISE E C N A T S I D S T I M I L T S U R H T E S I U R C . X A M LR FL 330 NORMAL AIR CONDITIONING ISA ANTI-ICING OFF (NM) FIGURE 033-57 033 PICTURE SUPPLEMENTS 148 © 2008 AVIATIONEXAM.com time 140 150 160 170 180 190 200 210 220 230 240 correction 410 2.3 2.4 2.6 2.7 2.7 - - - - - - 5 min 390 2.2 2.3 2.5 2.6 2.8 2.9 - - - - - 5 min 370 2.1 2.2 2.4 2.5 2.7 2.8 2.9 - - - - 5 min 350 2.0 2.1 2.2 2.4 2.5 2.7 2.8 2.9 3.0 3.1 - 6 min 330 1.9 2.0 2.1 2.3 2.4 2.5 2.7 2.8 2.9 3.0 3.1 6 min 310 1.8 1.9 2.0 2.2 2.3 2.4 2.5 2.7 2.8 2.8 3.0 5 min 290 1.7 1.8 1.9 2.0 2.1 2.3 2.4 2.5 2.6 2.8 2.9 5 min 270 1.8 1.7 1.8 1.9 2.0 2.1 2.2 2.4 2.5 2.6 2.7 5 min 250 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.4 2.5 4 min 200 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 3 min 150 1.0 1.1 1.1 1.2 1.3 1.4 1.5 1.5 1.6 1.7 1.8 100 0.7 0.8 0.8 0.9 0.9 1.0 1.0 1.1 1.1 1.2 1.3 3 min time SPEED 140 150 160 170 180 190 200 210 220 230 240 correction LRC 2.3 2.4 2.6 2.7 2.8 2.8 2.8 3.0 3.0 3.0 3.0 6 min M.80 2.3 2.4 2.6 2.6 2.7 2.8 2.8 3.0 3.0 3.0 3.0 6 min M.82 2.2 2.4 2.6 2.6 2.6 2.8 2.8 2.9 3.0 3.0 3.0 6 min M.84 2.2 2.3 2.4 2.5 2.5 2.5 2.6 2.7 2.8 2.8 2.8 7 min FL WEIGHT AT BRAKE RELEASE (1000 kg) CORRECTION ON FUEL CONSUMPTION (1000 kg) WEIGHT AT BRAKE RELEASE (1000 kg) CORRECTION ON FUEL CONSUMPTION (1000 kg) CLIMB CORRECTION The planner must correct the values for the fuel and the time obtained from the integrated cruise tables with the numbers given in the following tables. The tables which are esta blished for M.80, M.82, M.84 and long range speed take into account climbing from the brake releas e point at 250KT/300KT/M.80.
CLIMB TO OPTIMUM FL STEP CLIMB CORRECTION When the flight includes one or more step climbs (2000 feet below FL290, 4000 fe et above), apply a correction of 160 kg per step climb to the fuel consumption. 3 min FIGURE 033-58 033 PICTURE SUPPLEMENTS 149 © 2008 AVIATIONEXAM.com time 130 140 150 160 170 180 190 correction 290 and 0.6 0.7 0.7 0.8 0.9 1.0 1.1 10 min above 270 0.6 0.7 0.7 0.8 0.9 0.9 1.0 250 0.6 0.6 0.7 0.7 0.8 0.8 0.9 200 0.5 0.6 0.6 0.7 0.7 0.8 0.8 8 min 150 0.5 0.5 0.6 0.6 0.6 0.7 0.7 100 0.4 0.4 0.4 0.5 0.5 0.5 0.5 FL WEIGHT OVERHEAD DESTINATION (1000 kg) CORRECTION ON FUEL CONSUMPTION (1000 kg) DESCENT CORRECTION Correct the fuel and the time values determined in the integrated cruise tables as follows to take into account the descent down to 1500 feet followed by 6 min IFR approach a nd landing. LONG RANGE CRUISE LRC, M.80, M.82, M.84 FROM OPTIMUM FL time 130 140 150 160 170 180 190 correction 0.6 0.7 0.8 0.9 1.0 1.0 1.1 11 min WEIGHT OVERHEAD DESTINATION (1000 kg) CORRECTION ON FUEL CONSUMPTION (1000 kg) FIGURE 033-59 033 PICTURE SUPPLEMENTS 150 © 2008 AVIATIONEXAM.com DIS. FL310 FL350 FL390 FL330 FL370 FL410 32826 31906 30946 30195 29491 7.37 6.47 6.38 6.27 6.18 6.14 34032 33058 32067 31285 30555 7.30 7.00 6.51 6.40 6.31 6.27 35244 34211 33245 32379 31624 7.44 7.14 7.04 6.53 6.44 5.40 36570 35370 34378 33478 32698 7.54 7.29 7.17 7.06 6.57 6.63 37607 36603 35517 34584 33778 8.07 7.47 7.30 7.16 7.10 7.05 39050 37728 36661 35694 34864 5.20 7.55 7.43 7.32 7.23 7.18 40300 38957 37810 36810 35956 8.33 8.09 7.67 7.45 7.35 7.31
28976 137 139 145 30024 141 142 151 31077 150 147 157 32135 155 149 154 33198 160 153 170 34269 159 158 177 35346 154 163 184
41559 40142 38965 37931 37054 36430 158 8.45 8.22 8.10 7.58 7.48 7.44 42921 41333 40125 39057 38157 37518 173 5.58 8.36 8.23 8.10 8.01 7.57 44069 42528 41291 40189 39265 38613 178 9.10 8.49 8.36 8.23 8.14 8.09 45322 43734 42464 41327 40380 39714 183 9.23 9.03 8.49 8.36 8.27 8.22 46580 44946 43640 42471 41502 40823 187 9.35 9.16 9.02 8.49 8.39 8.35 47844 46165 44820 43618 42629 41938 191 9.48 9.29 9.15 9.01 8.52 8.48 49114 47389 46006 44764 43763 43090 194 10.00 9.42 9.28 9.14 9.05 9.00* 50391 48620 47198 45915 44900 44238 198 10.12 9.55 9.41 9.27 9.17 9.13* 51673 49857 48396 47021 46042 45391 201 10.24 10.08 9.53 9.40 9.30 9.26* 52961 51100 49600 48233 47191 46550 205 10.36 10.22 10.06 9.53 9.43 9.39* 54256 52349 50810 49401 48348 47715 208 10.48 10.35 10.19 10.05 9.56 9.52* 55557 53604 52026 50574 49511 48886 213 11.00 10.47 10.32 10.18 10.08 10.05* 56860 54867 53248 51752 50680 50063 217 11.12 11.00 10.45 10.31 10.21 10.18* 58152 56135 54477 52936 51856 51245 222 11.26 11.13 10.57 10.43 10.34 10.31* 59449 57407 55713 54126 53037 52432 227 11.39 11.26 11.10 10.56 10.46 10.44* 60751 58682 56955 55323 54265 53626 232 11.52 11.39 11.23 11.09 10.59 10.56* 62059 59963 58196 56525 55467 54826 237 12.06 11.52 11.36 11.21 11.12 11.09* 63371 61250 59442 57736 56675 56033 242 12.19 12.05 11.48 11.34 11.24 11.22* 64689 62544 60694 58962 57890 57245 247 12.33 12.17 12.01 11.47 11.37 11.35* 330 350 370 390 410 3500 3600 3700 3800 310 .FUEL = -0,4 % 5100 4000 4100 4200 4300 4400 4500 4600 4700 5300 FLIGHT LEVEL CORRECTION ON FUEL CONSUMPTION (KG/1.000 KG) 5200
167 191 172 200 177 208 182 215 187 223 193 231 198 238 203 246 208 254 214 261 220 269 225 277 231 283 237 290 243 297 249 304 256 312 263 321 273 327
4800 4900 5000 3900 3300 2800 2900 3000 3100 3200 3400 FLIGHT PLANNING FROM BREAKE RELEASE TO LANDING CLIMB: 250KTS/300KTS/M.80 - LONG RANGE CRUISE - DESCENT: M.80/300KTS/250KTS IMC PROCEDURE: 240 KG (6 MIN) TOTAL ANTI ICE ON PACK FLOW LO AIR (NM) TIME (H.MIN) FUEL CONSUMED (KG) ISA CG = 37,0 % REF. LANDING WEIGHT = 140.000 KG NORMAL AIR CONDITIONING ANTI ICING OFF .FUEL = +5 % ENGINE ANTI .FUEL = +1,5 % PACK FLOW HI OR/AND .FUEL = +1 % CARGO COOL ON ICE ON FIGURE 033-60 033 PICTURE SUPPLEMENTS 151 © 2008 AVIATIONEXAM.com < < ) < < < < ) < < < < < < < < < < < < < < < < < < FLIGHT PLAN PLAN DE VOL PRIORITY Priorité ADDRESSEE(S) Destinataire(s) FLIGHT TIME Heure de dépôt ORIGINATOR Expéditeur SPECIFIC IDENTIFICATION OF ADDRESSEE(S) AND/OR ORIGINATOR Identification précise du(des) destinataire(s) et/ou de l'expéditeur 3 MESSAGE TYPE
Type de message 7 AIRCRAFT IDENTIFICATION Identification de l'aéronef TYPE OF AIRCRAFT Type de l'aéronef (FPL 4 FLIGHT RULES Regles de vol TYPE OF FLIGHT Type de vol 10 EQUIPMENT Équipment WAKE TURBULENCE CAT. Cat. de turbulence de sillage 9 NUMBER Nombre 13 DEPARTURE AERODROME Aérodrome de départ TIME Heure 15 CRUISING SPEED Vitesse croisiere LEVEL Niveau ROUTE Route 16 DESTINATION AERODROME Aérodrome de destination TOTAL FEET Durée totale estimée HR. MIN. ALTN AERODROME Aérodrome de dégagement 2ND ALTN AERODROME 2eme aérodrome de dégagement 18 OTHER INFORMATION Renseignements divers SUPPLEMENTARY INFORMATION (NOT TO BE TRANSMITTED IN FPL MESSAGES) Renseignements complémentaires (A NE PAS TRANSMETTRE DANS LES MESSAGES DE PLAN DE VOL DÉPOSÉ) 19 ENDURANCE Autonomie E HR. MIN. PERSONS ON BOARD Personnes a bord P R UHF VHF ELBA JACKETS / Gilets de sauvetage LIGHT Lampes FLUORES Fluores UHF VHF SURVIVAL EQUIPMENT / Équipement de survie POLAR Polaire DESERT Désert MARITIME Maritime
JUNGLE Jungle DINGHIES/Canots NUMBER Nombre CAPACITY Capacité COVER Couverture COLOUR Couleur AIRCRAFT COLOUR AND MARKINGS / Couleur et marques de l'aéronef REMARKS / Remarques PILOT IN COMMAND / Pilote commandant de bord FILED BY / Deposé par SPACE RESERVED FOR ADDITIONAL REQUIREMENTS Espace reserve a des tins supplémentaires S P D M J D C N C A J L F U U V E V FF < < FIGURE 033-61 033 PICTURE SUPPLEMENTS 152 © 2008 AVIATIONEXAM.com INTRODUCTION The following flight planning tables allow the planner to determine trip fuel co nsumption and trip time required to cover a given air distance. These tables are established for: - Takeoff - Climb profile: 250 kts/300 kts/M.80 - Cruise mach number: M.80, M.82, M.84, LR - Descent profile: Cruise Mach number/300 kts/250 kts - Approach and landing: 240 kg 6 minute IFR - ISA - CG = 37% - Normal air conditioning - Anti ice OFF Note: 1. In the tables, the asterisk (*) means that a step climb of 4.000 feet must be flown to
reach the corresponding FL. 2. To obtain a flight plan at optimum cruise level, the highest flight level des ired within the flight has to be selected in the table. 3. For each degree Celsius above ISA temperature apply fuel correction 0,010(kg/°C/NM) x . ISA(°C) x Air Distance (NM). CORRECTION FOR DEVIATION FROM REFERENCE LANDING WEIGHT The fuel consumption must be corrected when the actual landing weight is differe nt from the reference landing weight. If it is lower (or greater) than the reference landing weight, subtract (or add) the value given in the correction part of the table per 1000 kg below ( or above) the reference landing weight. EXAMPLE The following is an example of a complete flight plan based on the assumptions: - Zero fuel weight (OWE + PAYLOAD): 160.000 kg = landing weight at alternate air port - Cruise M.82 at FL390 - Ground distance from departure to destination: 2.500 NM - Average wind during flight: -50 kts (headwind) - ISA conditions - Enroute reserve: 5 % - Ground distance from destination to alternate: 200 NM, no wind at FL200 To calculate the flight plan, a reverse calculation is needed, i.e. start with t he landing weight at alternate. FIGURE 033-62 033 PICTURE SUPPLEMENTS 153 © 2008 AVIATIONEXAM.com FUEL TANKERING GENERAL Fuel tanking graphs allow to determine the Optimum fuel quantity to be tanked as a function of the fuel price ratio between departure and destination airports. The following pages pres ent for one flight level per page the Optimum aircraft takeoff weight depending on the fuel price ratio ( departure fuel price divided by destination fuel price) and on the air distance to fly. The computed optimum takeoff weight is based on the additional fuel consumption needed for the transport of the extra (tanked) fuel and it is the weight at which the maximum p rofit can be achieved. The quantity of extra fuel that can be loaded is calculated as the difference betwee n the Optimum takeoff weight (including extra fuel) and the planned takeoff weight (without fuel tanki ng). The graphs are established for: FL290, 310, 330, 350, 370, 390 Air distances from 500 to 5.000 NM Flight profile: Climb 250 kts/300kts/M.80 Cruise M.80 Descent M.80/300 kts/250 kts Note: 1. If necessary, step climbs are performed to reach the indicated flight levels.
2. The crew/operator has to verify that the found aircraft weight complies with basic aircraft limitations (e.g. max fuel capacity) as well as with mission dependent restricti ons (e.g. MLW at destinations). EXAMPLES 1.Fuel price ratio = 0.930 Cruising Altitude = FL310 Planned TOW = 200.000 kg (mission weight without fuel tanking) Air Distance = 2500 NM Enter graph For the given air distance, the optimum fuel tanking weight is 187.000 kg, which is lower than the planned takeoff weight, no fuel tanking recommended. 2. Fuel price ratio = 0.890 Cruising Altitude = FL350 Planned TOW = 190.000 kg (mission weight without fuel tanking) Air Distance = 3.250 NM Enter graph For the given air distance, the optimum fuel tanking weight is 198.000 kg, which is 8.000 kg higher than the planned takeoff weight, optimum quantity of extra fuel is 8.000 kg. Check: a) New TOW less or wqual MTOW from departure airport. b) Total fuel to be loaded less or equal maximum fuel capacity. c) MLW at destination. FIGURE 033-63 033 PICTURE SUPPLEMENTS 154 © 2008 AVIATIONEXAM.com NGM = NAM x (TAS +/- WIND) TAS DETAILED FUEL PLANNING En-route Climb Tables are provided for a range of temperature deviations from ISA -15°C to ISA +2 5°C Fuel and time given in these tables are from brake release and distance from 1.5 00 ft. With a climb airspeed schedule 280 KIAS / 0,74 Mach. The stated TAS is the average for the climb and should be used to correct the st ill air distance shown. Off-Optimum Condition Fuel Mileage Penalty % LRC or Mach 0.74 Mach 0.78 2,000 ft above -1 -1 Optimum 0 0 2,000 ft below -1 -2 4,000 ft below -4 -4 8,000 ft below -10 -11 12,000 ft below -15 -20 Off-Optimum Fuel Penalty Ascension Island Ghana Irish Republic *+ Morocco Sierra Leone Burkina-Faso Great Britain + Ivory Coast Portugal *+ Togo Republic Canary Islands * Guinea-Bissau Liberia Principe Tristan da Cunha Channel Islands + Guinea Republic Madeira * St. Helena
Faeroes *, The Iceland Mali Sao Tome Gambia, The Ireland, Northern + Mauritania Senegal + The European Union directive states that Summer Time, one hour in advance of U TC, is kept from 2001 March 25th 01h to October 28th 01h UTC. STANDARD TIMES (Corrected to November 1999) LIST II - PLACES NORMALLY KEEPING UTC * Summer time may be kept in these places. FIGURE 033-64 FIGURE 033-65 FIGURE 033-66 033 PICTURE SUPPLEMENTS 155 © 2008 AVIATIONEXAM.com STANDARD TIMES (Corrected to November 1999) LIST I PLACES FAST ON UTC (mainly those EAST OF GREENWICH) The times given below should be added to UTC to give Standard Time subtracted fr om Standard Time to give UTC. h m h m Admiralty Islands 10 Denmark *+ 01 Afghanistan 04 30 Djibouti 03 Albania * 01 Algeria 01 Egypt, Arab Republic of * 02 Amirante Islands 04 Equatorial Guinea, Republic of 01 Andaman Islands 05 30 Eritrea 03 Angola 01 Estonia * 02 Armenia * 04 Ethiopia 03 Australia Australian Capital Territory * 10 Fiji * 12 New South Wales 1 * 10 Finland *+ 02 Northern Territory 09 30 France *+ 01 Queensland 10 South Australia * 09 30 Gabon 01 Tasmania * 10 Georgia * 04 Victoria * 10 Germany *+ 01 Western Australia 08 Gibraltar * 01 Whitsunday Islands 10 Greece *+ 02 Austria *+ 01 Guam 10 Azerbaijan * 04 Hong Kong 08 Hungary * 01 Bahrain 03 Balearic Islands * 01 India 05 30 Bangladesh 06 Indonesia, Republic of Belarus * 02 Bangka, Billiton, Java, West and Belgium *+ 01 Central Kalimantan, Madura, Sumatra 07 Benin 01 Bali, Flores, South and East Bosnia and Herzegovina * 01 Kalimantan, Lombok, Sulawesi, Botswana, Republic of 02 Sumba, Sumbawa, Timor, 08 Brunei 08 Aru, Irian Jaya, Kai, Moluccas, Bulgaria * 02 Tanimbar 09 Burma (Myanmar) 06 30 Iran * 03 30 Burundi 02 Iraq * 03 Israel * 02 Italy *+ 01 Cambodia 07 Cameroon Republic 01 Jan Mayen Island 01 Japan 09
Jordan * 02 Caroline Islands 2 10 Kazakhstan * Central African Republic 01 Western, Aktau, Uralsk, Atyrau 04 Chad 01 Central, Aktyubinsk, Kzyl-Orda 05 Chagos Archipelago 05 Eastern 06 Chatham Islands * 12 45 Kenya 03 China, People s Republic of 08 Kiribati Republic Christmas Island, Indian Ocean 07 Gilbert Islands 12 Cocos (Keeling) Islands 06 30 Phoenix Islands 13 Comoro Islands (Comoros) 03 Line Islands 3 14 Congo, Democratic Republic Korea, North 09 Kinshasa, Mbandaka 01 Republic of (South) 09 Haut-Zaire, Kasai, Kivu, Shaba 02 Kuril Islands 11 Congo Republic 01 Kuwait 03 Corsica * 01 Kyrgyzstan * 05 Crete * 02 Croatia * 01 Laccadive Islands 05 30 Cyprus, Ercan *, Larnaca * 02 Laos 07 Czech Republic 01 Latvia * 02 * Summer time may be kept in these places. + For Summer time dates see List II 1 Except Broken Hill Area which keeps 09h 30m. 2 Except Pohnpei, Pingelap and Kosrae which keep 11h. 3 The Line Islands that are not part of the Kiribati Republic keep 10h slow on U TC. * FIGURE 033-67 033 PICTURE SUPPLEMENTS 156 © 2008 AVIATIONEXAM.com STANDARD TIMES (Corrected to November 1999) LIST I (continued) h m h m Lebanon * 02 Russia (continued) Lesotho 02 Zone 7 Bratsk, Irkutsk, Ulan-Ude 08 Libya 02 Zone 8 Yakutsk, Chita, Tiksi 09 Liechtenstein * 01 Zone 9 Vladivostok, Khabarovsk, Lithuania * 02 Okhotsk 10 Lord Howe Island * 10 30 Zone 10 Magadan, Yuzhno 11 Luxembourg *+ 01 Zone 11 Petropavlovsk, Pevek 12 Rwanda 02 Macau 08 Ryukyu Islands 09
Macedonia * former Yugoslav Republic 01 Macias Nguema (Fernando Póo) 01 Sakhalin Island * 10 Madagascar, Democratic Republic of 03 Santa Cruz Islands 11 Malawi 02 Sardinia * 01 Malaysia, Malaya, Sabah, Sarawak 08 Saudi Arabia 03 Maldives, Republic of The 05 Schouten Islands 10 Malta * 01 Serbia * 01 Mariana Islands 10 Seychelles 04 Marshall Islands 1 12 Sicily * 01 Mauritius 04 Singapore 08 Moldova * 02 Slovakia * 01 Monaco * 01 Slovenia * 01 Mongolia 08 Socotra 03 Mozambique 02 Solomon Islands 11 Somalia Republic 03 Namibia * 01 South Africa, Republic of 02 Nauru 12 Spain *+ 01 Nepal 05 45 Spanish Possessions in North Africa * 01 Netherlands, The *+ 01 Spitsbergen (Svalbard) * 01 New Caledonia 11 Sri Lanka 06 New Zealand * 12 Sudan, Republic of 02 Nicobar Islands 05 30 Swaziland 02 Niger 01 Sweden *+ 01 Nigeria, Republic of 01 Switzerland * 01 Norfolk Island 11 30 Syria (Syrian Arab Republic) * 02 Norway * 01 Novaya Zemlya 03 Taiwan 08 Tajikistan 05 Okinawa 09 Tanzania 03 Oman 04 Thailand 07 Tonga * 13 Pagalu (Annobon Islands) 01 Tunisia 01 Pakistan 05 Turkey * 02 Palau Islands 09 Turkmenistan 05 Papua New Guinea 10 Tuvalu 12 Pescadores Islands 08 Philippine Republic 08 Uganda 03 Poland * 01 Ukraine * 02 United Arab Emirates 04 Qatar 03 Uzbekistan 05 Reunion 04 Vanuatu, Republic of 11 Romania * 02 Vietnam, Socialist Republic of 07 Russia 2* Zone 1 Kaliningrad 02 Yemen 03 Zone 2 Moscow, St. Petersburg, Yugoslavia * , Federal Republic of 01 Arkhangelsk, Astrakhan 03 Zone 3 Samara, Izhevsk 04 Zambia, Republic of 02 Zone 4 Perm, Amderna, Novy Port 05 Zimbabwe 02 Zone 5 Omsk, Novosibirsk 06 Zone 6 Norilsk, Kyzyl, Dikson 07 * Summer time may be kept in these places. + For Summer time dates see List II 1 Except the Ebon Atol which keeps time 24h slow on that of the rest of the isla nds. 2 The boundaries between the zones are irregular, listed are chief towns in each zone. FIGURE 033-68 033 PICTURE SUPPLEMENTS
157 © 2008 AVIATIONEXAM.com METAR/TAF PARIS/CHARLES-DE-GAULLE LFPG/CDG SA1330 121330Z 27004KT 9999 SCT011 BKN050 09/08 Q1001 NOSIG= FC1100r 120800Z 1200918 30005KT 3500 BR BKN003 BECMG 0911 6000 SCT011 SCT050 BECMG 1113 9999 SCT020 BECMG TEMPO 1317 8000 SHRA SCT025TCU BKN030 T08/12Z T09/15Z= FT1000 121000Z 121812 27008KT 9999 BKN025 BECMG 1821 20005KT SCT030 BECMG 2124 6000 BECMG 0002 20008KT 2000 BR BKN005 TEMPO 0208 20004KT 0500 BCFG OVC001 BECMG 0810 18012KT 9999 SCT012 BECMG 1012 SCT020= BORDEAUX/MERIGNAC LFBD/BOD SA1330 121330Z 21005KT 9000 FEW030TCU FEW033CB SCT040 BKN100 09/08 Q1005 TEMPO 25015G25KT 3000 TSRA SCT005 BKN015CB= FC1100r 121100Z 121221 28010KT 9999 RA SCT020 FEW025CB SCT040 TEMPO 1218 25015G25KT 6000 SHRA SCT008 SCT020CB BKN033 PROB30 TEMPO 1218 28020G30KT 3000 TSRA SCT005 BKN015CB BKN030 BECMG 1821 22004KT 8000 NSW FEW006 BKN030= FT1000 122000Z 121812 30010KT 9999 SCT020 FEW025CB BKN040 BECMG 1822 22004KT 8000 FEW006 BKN030 BECMG 0306 24005KT 6000 SCT007 SCT015 BKN090 BECMG 1012 RA= LYON/SATOLAS LFLL/LYS SA1330 121330Z 14007KT 9000 TSRA FEW020CB SCT033TCU BKN046 09/07 Q1003 NOSIG= FC1100r 121100Z 121221 VRB03KT 9999 FEW010 SCT020 BKN040 BECMG 1821 33006KT TEMPO 1221 VRB15G20KT 4000 SHRA SCT008 BKN015= FT1000 121000Z 121812 33004KT 9999 SCT025 BKN060 BECMG 2224 VRB02KT 8000 SCT010 SCT020 BECMG 0204 1500 BR BKN003 TEMPO 0407 0800 FG OVC002 BECMG 0810 33006KT 9999 SCT015 BKN030= FIGURE 033-69 033 PICTURE SUPPLEMENTS 158 © 2008 AVIATIONEXAM.com METAR/TAF BALE/MULHOUSE LFSB/MLH SA1330 121330Z 23008KT 9999 RA FEW020 SCT030 BKN066 06/05 Q1001 NOSIG= FC1100r 121100Z 121221 18005KT 9000 RA FEW015 BKN030 BKN060 TEMPO 1216 NSW BECMG 1517 9999 FEW030 BKN040 BKN080 TEMPO 1621 SHRA= DUBAI OMDB/DXB FT1000 121212 33015KT 9999 SCT030 BKN090 TEMPO 1209 5000 SHRA PROB40 TEMPO 1424 VRB40KT 1000 TSSS SCT025CB BECMG 1618 05010KT BECMG 0608 33013G23KT= JOHANNESBURG/JAN SMUTS FAJS/JNB FT0900 120900Z 121212 36010KT 9999 FEW030CB FEW035 PROB40 TEMPO 1318 VRB15KT 3000 TSRA SCT030CB BKN080 FM2000 03005KT CAVOK BECMG 0204 SCT008 SCT100 PROB30 0305 3000 BCFG BKN004 FM0800 34012KT 9999 SCT025 T25/12Z T15/03Z T27/12Z= TUNIS/CARTHAGE DTTA/TUN
SA1330 121330Z 24008KT 6000 FU FEW023 BKN200 24/08 Q1007= LONDON/HEATHROW EGLL/LHR SA1330 121330Z 28008KT 7500 SCT021 BKN050 04/03 Q1008 NOSIG= FT1000 121000Z 121812 27008KT 9999 BKN025 BECMG 1821 20005KT SCT030 BECMG 2024 5000 BECMG 0002 VRB06KT 2200 BR BKN 005 TEMPO 0208 20003KT 1500 BR OVC002 BECMG 0810 VRB02KT 5500 BKN012 BECMG 1012 SCT020 9999= TRUE TRACK / FUEL POSITION DISTANCE CONSUMPTION (litres) 2 3 4 D R A 124°/112 3 3 6 J G T 123°/131 9 6 8 N E L U B FIGURE 033-70 FIGURE 033-71 033 PICTURE SUPPLEMENTS 159 © 2008 AVIATIONEXAM.com Endurance / Fuel Calculation Fuel (kg) Time (hh:mm) Trip Fuel 5.800 02:32 Contingency Fuel Alternate Fuel 1.800 00:42 Final Reserve Fuel 1.325 Minimum T/O Fuel Extra Fuel Actual T/O Fuel Taxi Fuel 200 Ramp Fuel 10.000 CH 000 045 090 135 ... Dev -2 -4 -3 -1 Flight Level 40 80 120 160 200 TAS (knots) 190 198 204 212 220 Hourly fuel flow (l/hrs) 210 202 182 170 156 FIGURE 033-72 FIGURE 033-73 FIGURE 033-74 033 PICTURE SUPPLEMENTS 160 © 2008 AVIATIONEXAM.com FIGURE 033-75 033 PICTURE SUPPLEMENTS 161 © 2008 AVIATIONEXAM.com FIGURE 033-76 033 PICTURE SUPPLEMENTS 162 © 2008 AVIATIONEXAM.com FIGURE 033-77
033 PICTURE SUPPLEMENTS 163 © 2008 AVIATIONEXAM.com FIGURE 033-78 033 PICTURE SUPPLEMENTS 164 © 2008 AVIATIONEXAM.com FIGURE 033-79 033 PICTURE SUPPLEMENTS 165 © 2008 AVIATIONEXAM.com FIGURE 033-80 033 PICTURE SUPPLEMENTS 166 © 2008 AVIATIONEXAM.com FIGURE 033-81 033 PICTURE SUPPLEMENTS 167 © 2008 AVIATIONEXAM.com FIGURE 033-82 033 PICTURE SUPPLEMENTS 168 © 2008 AVIATIONEXAM.com Simplied Flight Planning TRIP TIME hr 1 2 0 3 20 10 0 -10 ISA DEV °C REF LINE REF LINE 0 200 400 600 800 1000 TRIP DISTANCE NM 100 100 HEAD TAIL WIND kt 50 50 0 2 3 4 5
Trip Distances 0 NM to 1,000 NM
6 7 8 FUEL REQUIRED 1000 kg 30 40 50 60 LANDING WEIGHT 1000 kg 1 BASED ON: 280 / 0.74 CLIMB 0.74 / 250 DESCENT PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft PRESSURE ALTITUDE 1000 ft 12 24 20 8 1618 810121416 24 8 24 REF LINE 300 kt IAS CRUISE FIGURE 033-83 033 PICTURE SUPPLEMENTS 169 © 2008 AVIATIONEXAM.com Critical Fuel Reserve One Engine Inoperative 0 3 4 5 6 7 8 9 FUEL REQUIRED 1000 kg 1 2 10 11 12 15 14 13 100 0 100 HEAD TAIL WIND kt 50 50
200 400 600 800 1000 0 1200 1400 DISTANCE TO DIVERSION AIRPORT FROM CRITICAL POINT NM REF LINE Emergency descent to 10,000 ft Level cruise at 10,000 ft 250 KIAS descent to 1,500 ft 15 minutes hold at 1,500 ft One missed approach; approach & land 5% allowance for wind errors Includes APU fuel burn 70656055504540 ONE ENGINE INOPERATIVE WEIGHT AT CRITICAL POINT 1000 kg INCREASE FUEL REQUIRED BY 0.5% FOR EACH 10°C HOTTER THAN ISA CONDITIONS. IF ICING CONDITIONS EXIST, INCREASE FUEL REQUIRED BY 20% TO ACCOUNT FOR ENGINE & WING A.I. ON & ICE ACCUMULATION ON UNHEATED SURFACES. ALLOWANCE FOR PERFORMANCE DETERIORATION NOT INCLUDED. COMPARE THE FUEL REQUIRED FROM THIS CHART WITH CRITICAL FUEL RESERVES FOR TWO ENGINES OPERATIVE. USE THE HIGHER OF THE TWO. FIGURE 033-84 033 PICTURE SUPPLEMENTS 170 © 2008 AVIATIONEXAM.com Critical Fuel Reserve All Engines Operating 0 3 4 5 6 7 8 9 FUEL REQUIRED 1000 kg 1 2 10 11 12 15 14 13 100 0 100 HEAD TAIL WIND kt 50 50 200 400 600 800 1000 0 1200 1400 DISTANCE TO DIVERSION AIRPORT FROM CRITICAL POINT NM REF LINE Emergency descent to 10,000 ft Level cruise at 10,000 ft 250 KIAS descent to 1,500 ft 15 minutes hold at 1,500 ft One missed approach; approach & land
5% allowance for wind errors 706560555045 40 ALL ENGINES OPERATIVE WEIGHT AT CRITICAL POINT 1000 kg INCREASE FUEL REQUIRED BY 0.5% FOR EACH 10°C HOTTER THAN ISA CONDITIONS. IF ICING CONDITIONS EXIST, INCREASE FUEL REQUIRED BY 18% TO ACCOUNT FOR ENGINE & WING A.I. ON & ICE ACCUMULATION ON UNHEATED SURFACES. ALLOWANCE FOR PERFORMANCE DETERIORATION NOT INCLUDED. COMPARE THE FUEL REQUIRED FROM THIS CHART WITH CRITICAL FUEL RESERVES FOR ONE ENGINE INOPERATIVE. USE THE HIGHER OF THE TWO. FIGURE 033-85
