777-200 to 777-200ER/-200LR/ -300/-300ER/Freighter Differences Training TBC-777-D1 Revision Number: 5 Revision Date: May 5, 2008
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777-200 to 777-200ER-/200LR/-300/-300ER/Freighter Differences Differences
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Range The 777-200 is designed for routes up to 5,235 nm (9,695 km). The 777-200ER is designed for routes up to 7,700 nm (14,260 km). The 777-200LR is designed for routes up to 9,380 nm (17,370 km). The 777-300 is designed for routes up to 6,015 nm (11,135 km). The 777-300ER is designed for routes up to 7,930 nm (14,685 km). The 777 Freighter is designed for routes up to 4,885 nm (9,045 km) with a full payload.
Range Capability From London 777-200
(305 three-class passengers)
777-200ER
(301 three-class passengers)
777-200LR*
(301 three-class passengers)
777-300 (368 three-class passengers)
777-300ER (365 three-class passengers)
777 Freighter (226,700lb/102,830kg payload)
Typical mission rules Airways and traffic allowances included 85% annual winds * Three optional auxiliary fuel tanks included
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Range Capability From New York 777-200
(305 three-class passengers)
777-200ER
(301 three-class passengers)
777-200LR*
(301 three-class passengers)
777-300 (368 three-class passengers)
777-300ER (365 three-class passengers)
777 Freighter (226,700lb/102,830kg payload)
Typical mission rules Airways and traffic allowances included 85% annual winds * Three optional auxiliary fuel tanks included
Range Capability From Tokyo 777-200
(305 three-class passengers)
777-200ER
(301 three-class passengers)
777-200LR* (301 three-class passengers)
777-300 (368 three-class passengers)
777-300ER (365 three-class passengers)
777 Freighter (226,700lb/102,830kg payload)
Typical mission rules Airways and traffic allowances included 85% annual winds * Three optional auxiliary fuel tanks included
May 5, 2008
TBC-777-D1
3
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Weight Limitations The weight limitations for the 777-200ER/-200LR/-300/-300ER/Freighter vary depending on engine thrust and customer options. See “Engine Configurations” which follows for specifications. Here are typical airplane weight limitations for the 777-200ER/-200LR/-300/-300ER/Freighter airplanes:
777-200 Weights
Pounds
Kilograms
Maximum Taxi Weight
547,000
248,115
Maximum Takeoff Weight
545,000
247,208
Maximum Landing Weight
445,000
201,849
Maximum Zero Fuel Weight
420,000
190,509
Pounds
Kilograms
Maximum Taxi Weight
652,000
295,742
Maximum Takeoff Weight
650,000
294,835
Maximum Landing Weight
470,000
213,188
Maximum Zero Fuel Weight
440,000
199,581
Pounds
Kilograms
Maximum Taxi Weight
768,000
348,358
Maximum Takeoff Weight
766,000
347,451
Maximum Landing Weight
492,000
223,167
Maximum Zero Fuel Weight
461,000
209,106
777-200ER Weights
777-200LR Weights
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777-300 Weights
Pounds
Kilograms
Maximum Taxi Weight
662,000
300,278
Maximum Takeoff Weight
660,000
299,371
Maximum Landing Weight
524,000
237,682
Maximum Zero Fuel Weight
495,000
224,528
Pounds
Kilograms
Maximum Taxi Weight
777,000
352,441
Maximum Takeoff Weight
775,000
351,534
Maximum Landing Weight
554,000
251,290
Maximum Zero Fuel Weight
524,000
237,682
Pounds
Kilograms
Maximum Taxi Weight
768,000
348,358
Maximum Takeoff Weight
766,000
347,451
Maximum Landing Weight
575,000
260,815
Maximum Zero Fuel Weight
547,000
248,115
777-300ER Weights
777 Freighter Weights
May 5, 2008
TBC-777-D1
5
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
VREF Limitation (777-200LR/Freighter) At lighter weights, FMC approach VREF speeds are limited to a minimum value to ensure controllability in the event of an engine failure. These minimum speeds vary with engine maximum thrust rating and destination airport elevation.
Minimum Takeoff Weight and FMC Message (777-200LR/Freighter) Takeoff at the (GE90-110B1L or GE90-115BL) thrust rating requires observance of a minimum takeoff weight in order to maintain airplane controllability in the event of an engine failure during takeoff. FMC gross weight entries less than the minimum takeoff weight will cause the message 'V SPEEDS UNAVAILABLE' to appear in the FMC scratchpad and the takeoff speed entries will be blank. For takeoff at weights below the minimum takeoff weight, use of a lower thrust rating (certified derate) is required. Note that the assumed temperature method of reducing thrust may not be used as a means to comply with this restriction.
May 5, 2008
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Dimensions 777-200 and 777-200ER Dimensions The 777-200 and 777-200ER have the same dimensions.
199 Feet 11 Inches (60.9 Meters) 70 Feet 7.5 Inches (21.53 Meters)
36 Feet (11 Meters)
60 Feet 6 Inches (18.4 Meters)
84 Feet 11 Inches (25.9 Meters) 206 Feet 6 Inches (63 Meters) 209 Feet 1 Inch (63.7 Meters)
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777-200LR Dimensions The 777-200LR fuselage is the same as the 777-200. The wing span has an added 12 feet 8 inches (3.9 meters). It is also 10 inches (25.5 centimeters) taller.
212 Feet 7 Inches (64.8 Meters) 70 Feet 7.5 Inches (21.53 Meters)
36 Feet (11 Meters)
61 Feet 4 Inches (18.7 Meters)
84 Feet 11 Inches (25.9 Meters) 206 Feet 6 Inches (63 Meters) 209 Feet 1 Inch (63.7 Meters)
May 5, 2008
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777-300 Dimensions 777-300 fuselage extensions have added 33 feet (10 meters) to the total length of the airplane compared to the 777-200/-200ER/-200LR/-200F.
199 Feet 11 Inches (60.9 Meters) 70 Feet 7.5 Inches (21.53 Meters)
36 Feet (11 Meters)
60 Feet 8 Inches (18.5 Meters)
102 Feet 5 Inches (31.2 Meters) 239 Feet 9 Inches (73.1 Meters) 242 Feet 4 Inches (73.9 Meters)
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777-300ER Dimensions The 777-300ER is similar in size to the 777-300 except for the wingspan which has an added 12 feet 8 inches (3.9 meters). It is also 2 inches (5.1 centimeters) taller.
212 Feet 7 Inches (64.80 Meters) 70 Feet 7.5 Inches (21.53 Meters)
36 Feet (11 Meters)
60 Feet 10 Inches (18.54 Meters)
102 Feet 5 Inches (31.2 Meters) 239 Feet 9 Inches (73.1 Meters) 242 Feet 4 Inches (73.9 Meters)
May 5, 2008
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777 Freighter Dimensions The 777 Freighter fuselage is the same as the 777-200/-200LR. The wing span is the same as the 777-200LR, it has an added 12 feet 8 inches (3.9 meters). It is also 10 inches (25.5 centimeters) taller than the 777-200.
212 Feet 7 Inches (64.8 Meters) 70 Feet 7.5 Inches (21.53 Meters)
36 Feet (11 Meters)
61 Feet 4 Inches (18.7 Meters)
84 Feet 11 Inches (25.9 Meters) 206 Feet 6 Inches (63 Meters) 209 Feet 1 Inch (63.7 Meters)
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Turning Radius The wing tip swings the largest arc while turning and determines the minimum obstruction clearance path. All other portions of the airplane structure remain within this arc.
777-200 and 777-200ER Turning Radius
Nose radius 110 Feet (33.5 Meters)
Tail radius 131 Feet (39.9 Meters)
s u i d r a l i a T
Steering angle 70 o
Nose Radius
Minimum width of pavement for 180o turn
u s i d a R p T i g n W i
Wing tip radius 144.9 Feet (44.2 Meters)
Center of turn for minimum turning radius. (Slow continuous turning with minimum thrust on all engines. No differential braking.)
Note: Minimum width of pavement for 180 o turn: 155.8 Feet (47.5 Meters)
CAUTION: Do not attempt to make a turn away from an obstacle within 15 feet (4.6 m) of the wing tip, or within 50 feet (15.2 m) of the nose. May 5, 2008
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777-200LR and 777 Freighter Turning Radius
Nose radius 112 Feet (34.1 Meters)
Tail radius 130 Feet (39.4 Meters)
s u i d r a l i a T
Steering angle 70 o
Nose Radius
Minimum width of pavement for 180o turn
u s i d a R i p T n g i W
Wing tip radius 152 Feet (46.3 Meters)
Center of turn for minimum turning radius. (Slow continuous turning with minimum thrust on all engines. No differential braking.)
Note: Minimum width of pavement for 180 o turn: 155.8 Feet (47.5 Meters)
CAUTION: Do not attempt to make a turn away from an obstacle within 15 feet (4.6 m) of the wing tip, or within 55 feet (16.8 m) of the nose.
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777-300 Turning Radius
Nose radius 129.4 Feet (39.4 Meters)
Tail radius 148.8 Feet (45.3 Meters)
s u i d r a l i a T
Steering angle 70o
Nose Radius
Minimum width of pavement for 180o turn
u s i d a R p T i g n W i
Wing tip radius 153.2 Feet (46.7 Meters)
Center of turn for minimum turning radius. (Slow continuous turning with minimum thrust on all engines. No differential braking.)
Note: Minimum width of pavement for 180 ° turn: 183.8 Feet (56.0 Meters)
CAUTION: Do not attempt to make a turn away from an obstacle within 15 feet (4.6 m) of the wing tip, or within 39 feet (11.9 m) of the nose.
May 5, 2008
TBC-777-D1
15
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777-300ER Turning Radius
Nose radius 129.4 Feet (39.4 Meters)
Tail radius 148.8 Feet (45.3 Meters)
s u i d r a l i a T
Steering angle 70o
Nose Radius
Minimum width of pavement for 180o turn
u s i d a R i p T n g i W
Wing tip radius 160.7 Feet (49.0 Meters)
Center of turn for minimum turning radius. (Slow continuous turning with minimum thrust on all engines. No differential braking.)
Note: Minimum width of pavement for 180 o turn: 183.9 Feet (56.1 Meters)
CAUTION: Do not attempt to make a turn away from an obstacle within 15 feet (4.6 m) of the wing tip, or within 45 feet (13.9 m) of the nose.
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Supernumerary Signs and Lighting (777 Freighter) The Passenger Signs and Lighting Panel (now called the Supernumerary Signs and Lighting Panel) is unchanged from 777 Passenger airplanes except for the 'SUPRNMRY SIGNS' legend. The switch functions are identical to 777 Passenger airplanes. Also, to provide a “return to seat” function for any supernumeraries in the Main Deck Cargo Compartment, the sidewall lights will flash for 30 seconds when the SEAT BELTS switch is rotated to the ON posistion.
SUPRNMRY SIGNS NO SMOKING AUTO OFF ON
OVHD/ CB
SEAT BELTS AUTO OFF ON
DOME
STORM
MASTER BRIGHT
ON
OFF
MIN
PNL/FLOOD
PUSH ON/OFF
LANDING LEFT OFF
NOSE OFF
ON
RIGHT OFF
ON ON
May 5, 2008
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Oxygen System (777 Freighter) Oxygen Pressure Display (777 Freighter) Displays crew and supernumerary oxygen cylinder pressure (PSI) Note: Access is through the display select panel STATUS switch.
OXYGEN CREW PRESS
1950
SUPRNMRY PRESS
1950
Supernumerary Oxygen (777 Freighter) The supernumerary oxygen system is supplied by bottled gaseous oxygen. The supernumerary oxygen masks are located above the supernumerary seats in passenger service units (PSUs). The masks automatically drop from the PSUs if cabin altitude exceeds approximately 13,500 feet. The supernumerary masks can be manually deployed from the flight deck by pushing the overhead panel SUPRNMRY OXYGEN switch to the ON position. Oxygen flow can be reset by selecting the SUPRNMRY OXYGEN switch to the RESET position. Supernumerary oxygen pressure is displayed on the MFD STATUS display.
Supernumerary Oxygen switch (777 Freighter) The panel is identical to 777 Passenger airplanes with optional gaseous oxygen except for the 'SUPRNMRY OXYGEN' nomenclature on light plate. The switch functions are identical to 777 Passenger airplanes with optional gaseous oxygen.
SUPRNMRY OXYGEN RESET
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NORM
ON
TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Oxygen System EICAS Messages (777 Freighter) Message
Level
Aural
Condition
SUPRNMRY OXYGEN LOW
Advisory
Supernumerary Oxygen is low.
SUPRNMRY OXYGEN ON
Advisory
Supernumerary Oxygen is activated.
May 5, 2008
TBC-777-D1
19
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Doors and Windows (777 Freighter) Door Synoptic Display (777 Freighter) The 777 Freighter Doors Synoptic is identical to 777 Passenger airplanes except passenger doors 2 through 5 are removed and there is an additional main deck cargo door located aft of the wing. The 777 Freighter has two crew entry doors (1R and 1L and four cargo doors.
FWD ACCESS E/E ACCESS A
ENTRY 1L
ENTRY 1R FWD CARGO
MAIN DECK CARGO
AFT CARGO BULK CARGO
A (green) – Door mode is armed M (white) – Door mode is manual. (blank) - Door mode is not available
(amber) – passenger door open (blank) – passenger door closed (white) – door status is not available (amber) – cargo/access door open (blank) – cargo/access door closed (white) – door status is not available
MULTIFUNCTION DISPLAY
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Crew Entry Doors (777 Freighter) Door 1R and L design and operation is identical to those on the 777 Passenger airplanes. Door arming status indication remains an option. Emergency slides/rafts are provided at door 1L and 1R. Exterior emergency lighting at door 1L and 1R consists of escape slide lights. The lights are located aft of each door and illuminate the areas at the base of the escape slides.
Flight Deck Door (777 Freighter) There is no Flight Deck Door for the 777 Freighter. A curtain is installed in lieu of the flight deck door to partition the flight deck from the supernumerary area.
Doors and Windows EICAS Messages (777 Freighter) Message
DOOR MAIN DECK CARGO
May 5, 2008
Level
Aural
Caution
Beeper
Condition
Main deck cargo door is not closed, latched, and locked.
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Emergency Exits (777-300/-300ER/Freighter) Overwing Exits (777-300/-300ER) The biggest difference in the passenger cabin from the 777-200/-200ER/ -200LR is the additional evacuation doors located over each wing. There are now a total of 10 emergency exit doors in the cabin. The door numbers have been resequenced so that doors 3L and 3R are over the wing and doors 5L and 5R are near the tail.
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
The overwing exits are for emergency use only. An overwing exit slide is contained in the wing-body fairing on the fuselage and not in the door bustle, as on the passenger entry doors. However, doors 3L or 3R may contain a separate life raft to be used for ditching, depending on airline configuration. Do not use the overwing exits during ditching operations unless the door is equipped with a raft. The overwing slide is used for emergency evacuation of the airplane during land operations only. Opening the door with the door mode select lever in the AUTOMATIC or ARMED position will automatically deploy the slide. Evacuation Path
May 5, 2008
Barber Pole
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
When evacuating the airplane, passengers must step down on to the wing from the door sill. The evacuation path on the wing has a non-skid surface with directional arrows pointing aft to the slide ramp. When doors 3L or 3R are opened, the inboard spoilers on the associated wing automatically stow in the down position for the escape slide extension. The lower portion of the slide cannot be seen from the overwin g exit door. A red and white striped barber pole extends above the slide when th e lower portion inflates. This provides a visual indication that the entire slide has inflated correctly. Barber Pole
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
For land evacuations, if the slide does not deploy automatically, a manual inflation handle is located in the upper aft portion of the door frame.
FWD
Pull to manually inflate slide.
May 5, 2008
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
The escape slides for the overwing doors are located in the wing body fairing near the trailing edge of each wing. The EICAS message DOOR WING SLIDE L, R displays if the escape slide door is not closed and locked.
Wing Slide Compartment
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Slide/Raft Operation (777 Freighter) Emergency evacuation side/raft and pneumatic door opening systems are contained in each crew entry door. Each door system has enough po wer to open the door unassisted, even if the airplane is not level because of any landing gear collapse condition. A slide/raft cover in the lower face of the door contains the side/raft.
May 5, 2008
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Seating (777-300/-300ER) The extended 777-300/-300ER fuselage allows for additional seating and cargo space. 328 passengers can be accommodated in a 3 class configuration and up to 550 seats are available with an all economy configuration seating 10 abreast.
Air Systems (777 Freighter)
The Air Systems and Air Conditioning Panel on the 777 Freighter have been modified to meet specific requirements of the cargo airplane. AIR CONDITIONING EQUIP COOLING
RECIRC FANS
AUTO
ON
M/D FLOW NORM HIGH
ALTN VENT
AIR COND RESET
ON
OVRD
- MAIN DECK CARGO TEMP FWD AFT
FLT DECK TEMP AUTO
C
MAN
W
C
W
L PACK
AUTO OFF
C
W R PACK
L-TRIM AIR-R
ON
ON
FAULT
FAULT
AUTO OFF
Main Deck Cargo Temperature Control (777 Freighter) The Main Deck is divided into two zones, forward and aft, for temperature control. One FWD and one AFT MAIN DECK CARGO TEMP selector replace the CABIN TEMP selector. Target and actual zone temperatures are shown on the Air Synoptic page.
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Electrical System (777 Freighter) The 777 Freighter Electrical Panel is the same as the 777 Passenger airplanes except the IFE/PASS SEATS switch is removed.
ELECTRICAL
APU ON
BATTERY
OFF
START
ON
CABIN/ UTILITY
OFF
ON
APU GEN
OFF
FAULT
ON OFF
L BUS TIE
R BUS TIE
AUTO ISLN
AUTO
SECONDARY EXT PWR
PRIMARY EXT PWR
ON
ON
AVAIL
AVAIL
L MAIN
L XFR
CTRL CTRL
R XFR
R MAIN
BACKUP GEN L R
ON OFF
ON
ON
OFF
OFF
R GEN CTRL
ON OFF
DRIVE
DRIVE
L
32
ISLN
DRIVE DISC
TBC-777-D1
R
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Cargo Fire Panel (777 Freighter) Main Deck Cargo Compartment Smoke Detection (777 Freighter) CARGO FIRE
APU BTL
ARM
DISCH
MAIN DECK ARMED LWR FWD
MAIN
LWR AFT
ARMED
ARMED
FWD
AFT
DISCH FIRE/ OVHT TEST
DEPR/DISCH DEPR DISCH
The main deck cargo compartment has smoke detectors divided into 8 zones. If smoke is detected in any zone, a fire warning occurs. Whenever main deck cargo compartment smoke detection is inoperative, the EICAS advisory message DET FIRE MAIN DECK is displayed.
Main Deck Cargo Compartment Fire Extinguishing (777 Freighter) The main deck cargo compartment is a Class E compartment. With the Main Deck Cargo Fire Arm switch pressed and subsequently push the DEPR/DISCH switch, the combination of these two switches will command the Cabin Pressure Control System (CPCS) to initiate depressurization to a cabin altitude of 25,000 feet.
Fire Protection EICAS Messages (777 Freighter) Message
Level
Aural
FIRE CARGO MAIN DECK
Warning
Fire Bell
DET FIRE CARGO MAIN
Advisory
34
Condition
Fire is detected in the Main Deck Cargo Compartment. Loss of smoke detection capability in the main deck compartment.
TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Wingtip Configuration (777-200LR/-300ER/Freighter) The 777-200LR/-300ER/Freighter have a distinctive "rake" wingtip that makes it easily identifiable.
May 5, 2008
TBC-777-D1
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777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Flap Limit Speeds The 777-200ER/-200LR/-300/-300ER/Freighter flap limit speeds are different from the 777-200 airplane. 777-200
777-200ER
FLAP LIMIT
FLAP LIMIT
1 - 240K
1 - 255K
5 15 20 25 30
-
220K 200K 190K 180K 170K
5 15 20 25 30
-
235K 215K 195K 185K 170K
777-300
777-200LR/-300ER/Freighter
FLAP LIMIT
FLAP LIMIT
1 - 255K
1 - 265K 5 - 245K
5 - 235K 15 - 215K 20 - 200K 25 - 190K 30 - 180K
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15 20 25 30
TBC-777-D1
-
230K 225K 200K 180K
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Note the stripes painted on the top of the wing. These stripes are placed directly over the outside edge of the main gear wheels to assist the pilot in locating the main gear wheels in adverse lighting conditions.
L
Camera Display Switch
R
INBD
LWR
INBD
CTR ENG
ELEC
STAT
HYD
FUEL
CAMERA LTS
AIR
OFF DOOR
GEAR
FCTL
CAM
CANC/RCL CHKL
COMM
ON
NAV
Display Select Panel
Overhead Panel
Multifunction Display
May 5, 2008
TBC-777-D1
39
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777-200ER/-300/-300ER/Freighter 777-200LR (w/o aux tank)
Main Tank
Center Tank
Surge Tank
777-200LR (one aux tank) 777-200LR contains a total of 333,200 lbs (151,100 kgs) with one auxiliary tank.
Main Tank
Center Tank
Auxiliary Tank Surge Tank
May 5, 2008
TBC-777-D1
43
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Fuel Tank Capacities 777-200 Fuel Quantity
Gallons
Liters
Pounds
Kilograms
Left Main Tank
9,300
35,200
62,300
28,300
Right Main Tank
9,300
35,200
62,300
28,300
Center Tank
12,400
46,900
83,100
37,700
TOTAL
31,000
117,300
207,700
94,300
Gallons
Liters
Pounds
Kilograms
Left Main Tank
9,560
36,200
64,100
29,100
Right Main Tank
9,560
36,200
64,100
29,100
Center Tank
26,100
98,790
174,900
79,300
TOTAL
45,220
171,190
303,100
137,500
777-200ER/-300 Fuel Quantity
777-200LR (w/o aux tank)/-300ER/Freighter Fuel Quantity
Gallons
Liters
Pounds
Kilograms
Left Main Tank
10,300
38,990
69,000
31,300
Right Main Tank
10,300
38,990
69,000
31,300
Center Tank
27,290
103,290
182,800
82,900
TOTAL
47,890
181,270
320,800
145,500
Gallons
Liters
Pounds
Kilograms
Left Main Tank
10,300
38,990
69,000
31,300
Right Main Tank
10,300
38,990
69,000
31,300
Center Tank
27,290
103,290
182,800
82,900
Auxiliary Tank
1,850
7,000
12,400
5,600
TOTAL
49,740
188,270
333,200
151,100
777-200LR (one aux tank) Fuel Quantity
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Fuel Panels 777-200/-200ER/-300/-300ER/Freighter 777-200LR (w/o aux tank) FUEL CROSSFEED FWD
L PUMPS FWD
R PUMPS FWD
ON
ON
AFT
ON
ON
AFT
AFT
L
CENTER PUMPS
ON
R ON
TOTAL FUEL
203.7
LBS X 1000 L MAIN
R MAIN
FWD
FWD
62.3
CROSSFEED
62.3
AFT
AFT
L
R
79.1 CENTER
Fuel pump
May 5, 2008
Fuel valve closed
TBC-777-D1
Fuel valve open
45
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
777-200LR (one aux tank)
FWD CROSSFEED FWD
L PUMPS FWD
R PUMPS FWD
AFT
ON
ON
ON
L CENTER PUMPS R ON
ON
ON
AFT
AFT
A U X
ON
TOTAL FUEL
329.2
LBS X 1000 FUEL BALANCED L MAIN
R MAIN CROSSFEED
FWD
69.0
FWD
69.0
CENTER AFT
L
R
AFT
178.8
12.4 AUX
Fuel pump
46
Fuel valve closed
TBC-777-D1
Fuel valve open
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Fuel Jettison As with the 777-200 airplane, the fuel jettison system will jettison fuel from all tanks at the same time. However, on the 777-200ER/-200LR/ -300/-300ER/Freighter, the main tank jettison can be delayed under certain conditions. When the airplane is heavy and loaded near the forward CG, fuel is jettisoned from the center tank first. This is to keep the CG within limits. The computed jettison time is automatically adjusted to reflect the increased jettison time if main tank jettison is delayed. For a 777-200LR with auxiliary tank, fuel jettison does not occur directly from the auxiliary tank. Auxiliary fuel is transferred to the center tank where it may be jettisoned. Auxiliary tank transfer is inhibited during jettison if necessary to help avoid an undesirable forward CG shift.
May 5, 2008
TBC-777-D1
47
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Tail Skid (777-300/-300ER) The 777-300/-300ER is equipped with a tail skid. It helps protect the pressurized part of the airplane from contact with the runway. The tail skid retracts and extends along with the landing gear and is connected to the center hydraulic system. If the tail skid position disagrees with th e landing gear lever position, the EICAS advisory message TAIL SKID appears. Tail skid contact with the runway will not cause the TAIL STRIKE message to appear unless the tail strike sensor has also made contact.
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TBC-777-D1
May 5, 2008
777-200 to 777-200ER/-200LR/-300/-300ER/Freighter Differences
Tail Strike Protection (777-200LR/-300ER/Freighter) Tail Strike Protection (TSP) is added on the 777-200LR/-300ER/Freighter. lf the flight control system receives input that a tail strike is imminent, elevator deflection is decreased to reduce the potential for tail skid ground contact. It will not activate during a normal rotation and will not provide feedback to the control column. An additional hydraulic strut is installed on the 777-300ER forward of each main gear strut. During takeoff rotation this strut moves the axis of rotation aft providing increased takeoff performance capability by permitting lower rotation speeds. The picture below shows the large strut connected to the foreward side of the main gear st rut and the foreward axle.
May 5, 2008
TBC-777-D1
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