Boeing B747-400 KLM nc. City of Atlanta. PH-BFA Guided by the Marshall at Gate A15 terminal 1
| Measurement | 747-100B | 747-200B | 747-300 | 747-400 747-400ER |
747-8I |
|---|---|---|---|---|---|
| Cockpit crew | Three | Two | |||
| Typical seating capacity | SR: 550 (1-class) 539 (1-class) 452 (2-class) 366 (3-class) |
565 (1-class) 496 (2-class) 412 (3-class) |
660 (1-class) 524 (2-class) 416 (3-class) |
605 (maximum) 467 (3-class) |
|
| Length | 231 ft 10 in (70.6 m) | 250 ft 2 in (76.25 m) | |||
| Interior cabin width | 20 feet (6.1 m) | ||||
| Wingspan | 195 ft 8 in (59.6 m) | 211 ft 5 in (64.4 m) | 224 ft 7 in (68.5 m) | ||
| Wing area | 5,500 ft2 (510.95 m2) | 5,650 ft2 (525 m2) | 5963 ft2 (554 m2) | ||
| Wing sweep | 37.5º | ||||
| Aspect ratio | 6.9 | 7.9 | 8.5 | ||
| Tail height | 63 ft 5 in (19.3 m) | 63 ft 8 in (19.4 m) | 63 ft 6 in (19.4 m) | ||
| Maximum cargo capacity | 6,190 ft3 (175.3 m3) = 30xLD1 | 6,025 ft3 (170.5 m3) ER: 5,599 ft3 (158.6 m3) |
5,705 ft3 (161.5 m3) | ||
| Operating empty weight | 358,000 lb (162,400 kg) |
383,000 lb (174,000 kg) |
392,800 lb (178,100 kg) |
393,263 lb (178,756 kg) ER: 406,900 lb (184,600 kg) |
472,900 lb (214,503 kg) |
| Maximum takeoff weight | 735,000 lb (333,390 kg) |
833,000 lb (377,842 kg) |
875,000 lb (396,890 kg) ER: 910,000 lb (412,775 kg) |
975,000 lb (442,253 kg) |
|
| Cruising speed (at 35,000 ft (11,000 m) altitude) |
Mach 0.84 (555 mph, 893 km/h, 481 knots ) |
Mach 0.85 (567 mph, 913 km/h, 493 kn) ER: Mach 0.855 (570 mph, 918 km/h, 495 kn) |
Mach 0.855 (570 mph, 918 km/h, 495 kn) |
||
| Maximum speed | Mach 0.89 (594 mph, 955 km/h, 516 kn) |
Mach 0.92 (614 mph, 988 km/h, 533 kn) |
|||
| Required runway at MTOW* | 10,466 ft (3,190 m) | 10,893 ft (3,320 m) | 9,902 ft (3,018 m) ER: 10,138 ft (3,090 m) |
10,138 ft (3,090 m) | |
| Maximum range at MTOW (with max payload) |
5,300 nmi 6,100 mi; 9,800 km |
6,850 nmi 7,880 mi; 12,690 km |
6,700 nmi 7,700 mi; 12,400 km |
7,260 nmi 8,350 mi; 13,450 km ER: 7,670 nmi 8,830 mi; 14,200 km |
8,000 nmi 9,200 mi; 15,000 km |
| Maximum fuel capacity | 48,445 U.S. gal (40,339 imp gal/183,380 L) |
52,410 U.S. gal (43,640 imp gal/199,158 L) |
57,285 U.S. gal (47,700 imp gal/216,840 L) ER: 63,705 U.S. gal (53,045 imp gal/241,140 L) |
64,225 U.S. gal (53,478 imp gal/243,120 L) |
|
| Engine models (x 4) | PW JT9D-7A/-7F/-7J RR RB211-524B2 GE CF6-45A2 (747SR) |
PW JT9D-7R4G2 GE CF6-50E2 RR RB211-524D4 |
PW JT9D-7R4G2 GE CF6-80C2B1 RR RB211-524D4 |
PW 4062 GE CF6-80C2B5F RR RB211-524G/H ER: GE CF6-80C2B5F |
GEnx-2B67 |
| Engine thrust (per engine) | PW 46,500 lbf (207 kN) RR 50,100 lbf (223 kN) |
PW 54,750 lbf (244 kN) GE 52,500 lbf (234 kN) RR 53,000 lbf (236 kN) |
PW 54,750 lbf (244 kN) GE 55,640 lbf (247 kN) RR 53,000 lbf (236 kN) |
PW 63,300 lbf (282 kN) GE 62,100 lbf (276 kN) RR 59,500/60,600 lbf (265/270 kN) ER: GE 62,100 lbf (276 kN) |
66,500 lbf (296 kN) |
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