| 777-200LR |
Cockpit crew | Two |
Seating capacity, typical | 301 (3-class) |
| |
Length | 211 ft 1 in (63.7 m) |
Wingspan | 212 ft 7 in (64.8 m) |
Wing Sweepback | 31.64° |
Tail Height | 61 ft 9 in (18.8 m) |
Cabin Width | 19 ft 3 in (5.86 m) |
Fuselage Width | 20 ft 4 in (6.19 m) |
Cargo Capacity | 5,302 ft³ (150 m³) |
Empty Weight | 326,000 lb |
(148,181 kg) | |
Maximum take-off weight | 766,000 lb |
(347,450 kg) | |
Cruising Speed at 35,000 ft cruise altitude | 0.84 Mach (560 mph, 905 km/h, 490 knots) |
Maximum Cruise Speed at 35,000 ft cruise altitude | 0.89 Mach (587 mph, 945 km/h, 510 knots) |
| 7,500 nm |
(13,890 km) | |
| 9,450 nm |
(17,500 km) | |
Takeoff run at MTOW ISA+15 MSL | 11,600 ft (3,536 m) |
Maximum Fuel Capacity | 53,440 |
(202,290 L) | |
Service Ceiling | 43,100 ft (13,140 m) |
Engine (x 2) | GE90-110B |
GE90-115B | |
| |
Thrust (x 2) | GE: 110,000 lbf (480 kN) |
GE: 115,000 lbf (510 kN) | |
|