| Manufacturer |
Boeing Commercial Airplanes |
| National origin |
United States |
| First flight |
June 12, 1994 |
| Introduction |
June 7, 1995 with United Airlines |
| Role |
Wide-body jet airliner |
| Number built |
1,693 as of August 2022 |
| Model |
- 777-200/200ER
- 777-300
- 777-300ER
- 777-200LR/777F
|
| Cocpit crew |
Two |
| 2-class seats |
- 313 /777-200/200ER/
- 396 /777-300 and 777-300ER/
- 317 /777-200LR/777F/
|
| 3-class seats |
- 305 (24F/54J/227Y) /777-200/200ER/
- 368 (30F/84J/254Y) /777-300/
- 365 (22F/70J/273Y) /777-300ER/
- 301 (16F/58J/227Y) /777-200LR/777F/
|
| Exit limit |
- 440 /777-200/200ER/
- 550 /777-300 and 777-300ER/
- 440 /777-200LR/777F/
|
| Wing area |
- 4,605 sq ft (427.8 m2), 8.68 AR (777-200/200ER and 777-300)
- 4,702 sq ft (436.8 m2), 9.61 AR (777-300ER and 777-200LR/777F)
|
| Wingspan |
- 199 ft 11 in / 60.93 m, 31.6° Wing sweep (777-200/200ER and 777-300)
- 212 ft 7 in / 64.80 m, 31.6° Wing sweep (777-300ER and 777-200LR/777F)
|
| Fuselage width |
20 ft 4 in / 6.20 m |
| Tail height |
- 60 ft 9 in / 18.5 m /777-200/200ER/
- 60 ft 8 in / 18.5 m /777-300 and 777-300ER/
- 61 ft 1 in / 18.6 m /777-200LR/777F/
|
| Cargo volume |
- 5,330 ft³ / 150.9 m³ /777-200/200ER/
- 7,120 ft³ / 201.6 m³ /777-300 and 777-300ER/
- 5,330 ft³ / 150.9 m³ /777-200LR/777F/
|
| MTOW |
- 545,000 lb / 247,200 kg
200ER: 656,000 lb / 297,550 kg /777-200/200ER/
- 660,000 lb / 299,370 kg /777-300/
- 775,000 lb / 351,533 kg /777-300ER/
- 766,000 lb / 347,452 kg
777F: 766,800 lb / 347,815 kg /777-200LR/777F/
|
| OEW |
- 299,550 lb / 135,850 kg
200ER: 304,500 lb / 138,100 kg/777-200/200ER/
- 353,800 lb / 160,530 kg /777-300/
- 370,000 lb / 167,829 kg
300ERSF: 336,000 lb (152 t) /777-300ER/
- 320,000 lb / 145,150 kg
777F: 318,300 lb / 144,379 kg /777-200LR/777F/
|
| Cabin width |
231 in / 5.86 m, Seats: 18.5 in / 47 cm at 9 abreast, 17 in / 43 cm at 10 abreast |
| Ceiling |
43,100 ft (13,100 m) |
| Fuel capacity |
- 31,000 US gal / 117,340 L / 207,700 lb / 94,240 kg
200ER/300: 45,220 US gal / 171,171 L / 302,270 lb / 137,460 kg (777-200/200ER and 777-300)
- 47,890 US gal / 181,283 L / 320,863 lb / 145,538 kg (777-300ER and 777-200LR/777F)
|
Speed
|
Max. Mach 0.87 – Mach 0.89 (499–511 kn; 924–945 km/h), Cruise Mach 0.84 (482 kn; 892 km/h) |
Range
|
- 5,240 nmi / 9,700 km /777-200/
- 7,065 nmi / 13,080 km /777-200ER/
- 6,030 nmi / 11,165 km /777-300/
- 7,370 nmi / 13,649 km /777-300ER/
- 4,650 nmi (8,610 km) /777-300ERSF/
- 8,555 nmi / 15,843 km /777-200LR/
- 4,970 nmi (9,200 km) /777F/
|
Takeoff
|
- 8,000 ft (2,440 m) /777-200/
- 11,100 ft (3,380 m) /777-200ER/
- 10,600 ft (3,230 m) /777-300/
- 10,000 ft (3,050 m) /777-300ER/
- 9,200 ft (2,800 m) /777-200LR/
- 9,300 ft (2,830 m) /777F/
|
Engine
|
- 2× PW4000 / Trent 800 / GE90 /777-200/200ER/
- 2× PW4000 / Trent 800 /777-300/
- 2× GE90-115B /777-300ER/
- 2× GE90-110B/-115B /777-200LR/777F/
|
Max thrust
|
- 2× 77,200 lbf (343 kN) /777-200/
- 2× 93,700 lbf (417 kN) /777-200ER/
- 2× 98,000 lbf (440 kN) /777-300/
- 2× 115,300 lbf (513 kN) /777-300ER/
- 2× 110,000–115,300 lbf
489–513 kN /777-200LR/777F/
|
