B777_200ER |
B777_200 (For Use on Domestic Routes) |
B777_200 (For Use on International Routes) |
B777_300 |
[ For reference ] B747_400 |
|
Width(m) |
60.9 |
<-- |
<-- |
<-- |
64.4 |
Length(m) |
63.7 |
<-- |
<-- |
73.9 |
70.7 |
Height(m) |
18.5 |
<-- |
<-- |
<-- |
19.4 |
Number of Pilots |
2 Pilots |
<-- |
<-- |
<-- |
<-- |
Number of Seats |
234* ( F 12 / C 63 / Y 159) |
376 ( S 18 / Y 358) |
250 ( F 12 / C 68 / Y 170) |
477 ( S 18 / Y 459) |
337 ( F 15 / C 62 / Y 260) |
Maximum Take-off Weight |
293,900 |
202,900 |
247,200 |
233,900 |
394,600 |
Maximum Landing Weight(kg) |
208,600 |
201,800 |
<-- |
233,900 |
264,900 |
Maximum Zero Fuel Weight(kg) |
195,000 |
190,500 |
<-- |
224,500 |
242,600 |
Maximum Operating Limit Speed |
920(M0.87) |
<-- |
<-- |
950(M0.89) |
980(M0.92) |
Cruise Speed |
900(M0.84) |
870(M0.80) |
890(M0.83) |
890(M0.83) |
910(M0.85) |
Maximum Altitude |
13,100 |
<-- |
<-- |
<-- |
13,700 |
Range |
13,000 |
4,300 |
8,740 |
4,500 |
12,370 |
Fuel Tank Capacity |
171,160 |
117,300 |
<-- |
171,160 |
215,500 |
Engine |
PW4090 |
PW4074 |
PW4077 |
PW4090 |
C F 6_80 C 2B1 F |
Engine Thrust(kg)xNumber of Engines |
40,910x2 |
33,790x2 |
35,020x2 |
40,910x2 |
26,310x4 |
| * The first B777-200ER to be introduced will have 291 seats (C56, Y235) | |||
| F :First Class | C : Business Class | Y : Economy Class or Regular Seating | S :Super Seat |