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A320Descripción completa
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Weights Limits 320 321 Max taxi wt 77400 kg 93900 kg Max T/O wt 77000 kg 93500 kg Max Lnd wt 66000 kg 77800 kg Max ZFW 62500 kg 73800 kg Min wt 37230 kg 47500 kg Over wt lndg is permitted provided pilot follows overweight landing procedure.QRH 80.06 Flt Maneuver Load (All) Clean config -1 g to + 2.5 g Slats & Flaps ext 0 g to + 2 g Slats ext & Flaps ret 0 to +2 g Airport Operations (All) Runway slope ± 2% Runway Alt -2000 > 9200 ft Nominal Rwy width 45 m Wind for T/O & LNDG: Max X wind 38 kt Max T wind 10 kt Wind for Doors: Max Pax Door ops 65 kt Max Cargo Door ops 40 kt or 50 kts with nose into wind door must be closed before 65 kt. Speed Limits VMO up to 24600 ft 350 kts MMO above = 0.82 M Max Flaps/Slats speeds: 320 321 1 230 kts 235 kts 1+ F 215 kts 225 kts 2 200 kts 215 kts 3 185 kts 195 kts Full 177 kts 190 kts Max Alt to extend slat/flap 20000ft Taxi Speed: When taxi wt higher than 76000 kg Max speed 20 kt during turns. Gear Down speeds: Max Gr Exuded(VLE) 280 kt/M.67 Max to Ext Gr (VLO)ext 250 kt Max to Ret Gr(VLO)ret 220 kt Max Alt to Ext Gr 25000 ft -------------Max Tire Speed 195 kt Max Wiper Speed 230 kt Max window Speed 200 kt Max Taxi speed above (76.000) 20kt Cabin Pressure Max pos ∆ press 8.6 psi Max neg ∆ press - 1 psi Max ops FL 39800 ft Cabin Alt Warn 9550 ft (±350) Ram air inlet: Only open when ∆p lower than 1 psi Air condition with LP ground unit:
-Do not use both together. -Airflow supplied by the ground cart shall not exceed 1.2 kg/s (2.60 lb/s).
Air condition with HP ground unit: Do not use HP air when APU bleed is used. Avionics Ventilation OAT = 49 °C no limitation OAT = 55 °C time limit 2 h OAT = 60 °C time limit 1 h OAT = 64 °C time limit 1/2 h
Auto Flight Minimum height for AP use: T/O with SRS mode 100 ft OR 5 s After Liftoff Straight-in non-precision MDA Circle app MDA-100 ft ILS (no CAT II or III displayed) 160 ft G/A 100 ft all other phases 500 ft (321 900 ft) Non Precision app with Eng out: 321> is not permitted to use AP for NPA’s in: Final APP,NAV V/S, NAV/FPA. Only FD allowed. CAT II: Max wind limits: (321 without Auto LND) H/ wind 30 kt 40 kts T/ wind 10 kt 10 kts X/ wind 20 kt 25 kts CAT II Auto land approved in CONF 3 & CONF Full. At least one AP engaged in APPR mode with CAT 2, 3 single or dual displayed in the FMA. For manual landing disengage AP before 80 ft. Engine out: CAT II only approved in CONF Full (321 also in CONF 3) provided engine-out procedure completed before reaching 1000 ft in approach. Electrical Max continu load 100% (90 KVA) Max TR load ea 200 A Electric outlets: Forbidden to use on T/O & LNDG. Fuel Min Temp Jet A1 - 43̊ C Min Temp Jet A - 36 C Max = = + 54̊ C Max allowed wing fuel imbalance: 320 Inner tanks (outer tanks balanced) Full 1500 kg 4300 kg 1600 kg 2250 kg 2250 kg -The variation is linear between these values (No limitation below 2 250 kg)
Outer tanks
690 kg
Fuel content of one side (outer + inner) is equal to the fuel content of the other side (outer + inner), or On the side of the lighter outer tank, the inner tank fuel quantity is higher than the opposite inner tank quantity, up to a maximum of 3 000 kg.
321 Wing tanks Full 4000 kg 2350 kg
1320 kg 1450 kg Empty
-Apply linear interpolation between these values (No limitation below 2 350 kg).
Minimum fuel for T/O 1500 kg & Wing Tk LO LVL not displayed. Fuel management: (320) Feeding CTR tank then wing tanks. T/O on CTR tank is prohibited. Hydraulic Norm pressure 3000 psi ± 200 Landing Gear Max brk temp T/O (fan off) 300̊ C Taxi with deflated tires: Allowed with deflated tires but not allowed with damaged tires. 1- One tire on ea. gear Max speed 7 kt when turning. 2- Two tires on the same gear Max taxi speed 3 kt & steering limit 30̊ . Nose Wheel -Steering hand wheel 75 deg -tow bar less vehicle 85 deg -tow bar 95 deg NWS Must be displayed prior Push Back. APU APU maybe started with LOW OIL LEVEL maintenance action within next 10 hrs of APU ops required. Starter: 3 cycles then WAIT 60 min before attempting 3 more cycles.
Max N speed
107%
The APU automatically shuts down at 107 % N speed.
Max EGT START: Below 25000ft Above 25000ft
900̊ C 982̊ C
Maximum EGT, with APU running: 682 °C, with 5 s confirmation time for shutdown, or From 700 °C to 742 °C for Immediate shutdown, depending on the ambient temperature.
APU CONT. MAX Alt for bleed: - 20 000 ft ENG Start OR One Pack. - 15 000 ft Two packs, air bleed for anti-ice is not permitted.
MAX Alt to start: -41000 ft and APU will supply electrical up to 39000 ft.
Power Plant T/O & GA 5 min 950̊ C Eng out 10 min 950 C MCT unlimited 915̊ C Starting 725̊ C Oil: Max continu temp 140̊ C Max transient temp 15 min 155̊ C Min starting temp - 40̊ C Min temp for T/O - 10̊ C Min oil quantity: 9.5 qt + .5 qt/hr of flight time. RPM: N1 max 104% N2 max 105% Starter: 15 min cooling required after 4 consecutive cycles Each lasts a max of 2 min Pause 20 sec between attempts. >> No starter running engagement above 20% N2. Reverse Thrust: It is not permitted to select reverse thrust in flight. It is not permitted to back up the aircraft with reverse thrust. Maximum reverse should not be used below 70 kt (or when the airspeed indication starts to fluctuate). Idle reverse Is permitted down to aircraft stop.
Reduced Thrust T/O Can Not Be Used: -Contaminated Runway. -Deicing/anti-icing fluids are applied to the aircraft. -Gear down dispatch operation. -One brake inop. -30 day. -One or more N1 gauges inop. -Anti-skid sys. Inop on wet runway. -Ground spoiler control sys. Inop on wet runway. -One or two thrust reversers inop. On wet runway.
CONT,
320 Max reduction 25%. Limited to ISA + 53̊ C (T Max Flex). 321 Never lower than MCT at ISA + 35̊ C. Limited to ISA + 43̊ C ( T Max Flex). NAVIGATION In NAV mode, the IRS will not provide a valid magnetic heading: • For latitude greater than 73 ° North, • For latitude greater than 60 ° South.
944 PSI Less then this Refer To OXY The Table. LIM-35 P 1-2.
-Protection in case of smoke, with 100 % oxygen : For all cockpit members for 15 min at a cabin altitude of 8 000 ft. -----------------------------(OTHER INFORMATION) TASKSHARING The general task sharing shown below applies to all procedures. -The pilot's flying remains the pilot flying throughout the procedure. The Pilot Flying (PF), is responsible for the: Thrust levers Control of flight path and airspeed Aircraft configuration (request configuration change) Navigation Communications. -The Pilot Not Flying (PNF), is responsible for: Monitoring and reading aloud the ECAM and checklists Performing required actions, or actions requested by the PF, if applicable Using the engine master switches, cockpit C/Bs, IR and guarded switches, with PF's confirmation.
Rejecting the takeoff: -Below 100 kt: -if any ECAM warning/caution is activated. Above 100 kt and below V1: 1. Fire warning or severe damage. 2. Sudden loss of engine thrust. 3. Malfunctions or conditions that give unambiguous indications that the aircraft will not fly safely. 4. Any red ECAM warning. 5. Any amber ECAM caution listed below: F/CTL SIDESTICK FAULT ENG FAIL ENG REVERSER FAULT ENG REVERSE UNLOCKED ENG 1(2) THR LEVER FAULT
SPECIAL OPERATIONS - PRO-SPO-20 Flight Without Cabin Pressurization. -PRO-SPO-25 Flight with Gear Down. -PRO-SPO-35 Flight Over Mountainous Area. -PRO-SPO-40 Extended Range. Operations. -PRO-SPO-45 Engine Intermix. Operations. -PRO-SPO-50 Reduced Vertical Separation Minimum (RVSM). -PRO-SPO-51 Required Navigation Performance (RNP). -PRO-SPO-60 Operations on Narrow Runways. -PRO-SPO-65 Operations at QNH Above 1050 hPa. -PRO-SPO-85 ILS PRM Approach. --------------------------------
Regards; Fadi Ashour Sibie. PNR: 11008848 11 NOV 12. FCOM REV. 17 Aug 12 For study purpose only plz refer to
MEMORY ITEMS
your updated Manual for the
The following procedures are to be applied without referring to paper: CREW INCAPACITATION. EGPWS . EMER DESCENT UNRELIABLE SPEED INDICATION/ADR CHECK PROC. LOSS OF BRAKING. STALL RECOVERY. STALL WARNING AT LIFT-OFF. TCAS. WINDSHEAR. WINDSHEAR AHEAD.
