|
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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