Specifications
Model | 777-200 | 777-200ER | 777-200LR | 777 Freighter | 777-300 | 777-300ER | 777-8X | 777-9X |
---|---|---|---|---|---|---|---|---|
Cockpit crew | Two | |||||||
Seating capacity, typical |
314 (3-class) 400 (2-class) 440 (maximum) |
N/A (cargo) |
386 (3-class) 451 (2-class) 550 (maximum) |
353 (3-class) | 407 (3-class) | |||
Length | 209 ft 1 in (63.7 m) | 242 ft 4 in (73.9 m) | 228 ft 2 in (69.5 m) | 250 ft 11 in (76.5 m) | ||||
Wingspan | 199 ft 11 in (60.9 m) | 212 ft 7 in (64.8 m) | 199 ft 11 in (60.9 m) | 212 ft 7 in (64.8 m) | Unfolded: 233 ft 3 in (71.1 m) Folded: ~211 ft 3 in (64.4 m) |
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Wing sweepback | 31.64° | N/A | ||||||
Tail height | 60 ft 9 in (18.5 m) | 61 ft 1 in (18.6 m) | 60 ft 8 in (18.5 m) | N/A | ||||
Cabin width | 19 ft 3 in (5.87 m) | 19 ft 7 in (5.97 m) | ||||||
Fuselage width | 20 ft 4 in (6.20 m) | |||||||
Maximum cargo capacity | 5,720 cu ft (162 m3) 32× LD3 |
23,051 cu ft (653 m3) 37× pallets |
7,640 cu ft (216 m3) 44× LD3 |
N/A | ||||
Empty weight, operating | 297,300 lb (134,800 kg) |
304,500 lb (138,100 kg) |
320,000 lb (145,150 kg) |
318,300 lb (144,400 kg) |
353,800 lb (160,500 kg) |
370,000 lb (167,800 kg) |
N/A | |
Maximum landing weight | 445,000 lb (201,840 kg) |
470,000 lb (213,180 kg) |
492,000 lb (223,168 kg) |
575,000 lb (260,816 kg) |
524,000 lb (237,680 kg) |
554,000 lb (251,290 kg) |
N/A | |
Maximum Takeoff Weight (MTOW) |
545,000 lb (247,200 kg) |
656,000 lb (297,550 kg) |
766,000 lb (347,500 kg) |
766,800 lb (347,800 kg) |
660,000 lb (299,370 kg) |
775,000 lb (351,500 kg) |
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Typical cruise speed | Mach 0.84 (560 mph, 905 km/h, 490 knots) at a cruise altitude of 35,000 ft (11,000 m) | N/A | ||||||
Maximum speed | Mach 0.89 (590 mph, 950 km/h, 512 knots) at a cruise altitude of 35,000 ft (11,000 m) | N/A | ||||||
Maximum range |
5,240 nmi (9,700 km, 6,027 mi) |
7,725 nmi (14,310 km, 8,892 mi) |
9,380 nmi (17,370 km, 10,793 mi) |
4,900 nmi (9,070 km, 5,636 mi) |
6,005 nmi (11,120 km, 6,910 mi) |
7,930 nmi (14,690 km, 9,128 mi) |
9,480 nmi (17,557 km, 10,909 mi) |
8,100 nmi (15,001 km, 9,321 mi) |
Takeoff distance at MTOW (sea level, ISA) |
8,000 ft 2,440 m |
11,100 ft 3,380 m |
9,200 ft 2,800 m |
9,300 ft 2,830 m |
10,600 ft 3,230 m |
10,000 ft 3,050 m |
N/A | |
Maximum fuel capacity | 31,000 US gal (117,348 L) |
45,220 US gal (171,176 L) |
47,890 US gal (181,283 L) |
45,220 US gal (171,176 L) |
47,890 US gal (181,283 L) |
N/A | ||
Service ceiling | 43,100 ft (13,140 m) | |||||||
Engine (×2) | PW 4077 RR 877 GE90-77B |
PW 4090 RR 895 GE90-94B |
GE90-110B1 GE90-115B1 |
PW 4098 RR 892 GE90-92B/-94B |
GE90-115B1 | GE9X | ||
Thrust (×2) | PW: 77,000 lbf (342 kN) RR: 76,000 lbf (338 kN) GE: 77,000 lbf (342 kN) |
PW: 90,000 lbf (400 kN) RR: 93,400 lbf (415 kN) GE: 93,700 lbf (417 kN) |
GE −110B: 110,100 lbf (490 kN) GE −115B: 115,300 lbf (512 kN) |
PW: 98,000 lbf (436 kN) RR: 93,400 lbf (415 kN) GE: 92,000/93,700 lbf (409 kN/418 kN) |
GE: 115,540 lbf (514 kN) | 102,000 lbf (450 kN) |
Sources: Boeing 777 specifications, Boeing 777 Airport planning report, and other sources
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