常见航空器规格和性能参数
来自SINO云课堂
Variant | 737-600 | 737-700 | 737-800 | 737-900ER |
---|---|---|---|---|
Cockpit crew | Two | |||
2-class | 108 (8F@36" 100Y@32") | 128 (8F@36" 120Y@32") | 160 (12F@36" 148Y@32") | 177 (12F@36" 165Y@32") |
1-class | 123 @32" - 130 @ 30" | 140 @32" - 148 @ 30" | 175 @32" - 184 @ 30" | 177 @32" - 215 @ 28" |
Exit Limit | 149 | 189 | 220 | |
Seat width | First : 22in / 56 cm; Economy : 17in / 43 cm | |||
Length | 102 ft 6 in / 31.24 m | 110 ft 4 in / 33.63 m | 129 ft 6 in / 39.47 m | 138 ft 2 in / 42.11 m |
Height | 41 ft 3 in / 12.57 m | 41 ft 2 in (12.55 m) | ||
Wing | Span: 112 ft 7 in / 34.32 m, with winglets: 117 ft 5in / 35.79m; Area: 124.60 m2 (1,341.2 sq ft); Sweepback: 25°; AR: 9.44 | |||
Fuselage | Width: 12 ft 4 in (3.76 m); Cabin width: 11 ft 7 in (3.54 m); Cabin height: 86.6 in (2.20 m) | |||
Operating empty weight | 80,200 lb / 36,378 kg | 83,000 lb / 37,648 kg | 91,300 lb / 41,413 kg | 98,495 lb / 44,677 kg |
Maximum landing weight | 121,500 lb / 55,111 kg | 129,200 lb / 58,604 kg | 146,300 lb / 66,361 kg | 157,300 lb / 71,350 kg |
Maximum takeoff weight | 144,500 lb / 65,544 kg | 154,500 lb / 70,080 kg | 174,200 lb / 79,016 kg | 187,700 lb / 85,139 kg |
Fuel capacity | 6,875 US gal / 26,022 L | 7,837 US gal / 29,666 L | ||
Lower deck cargo | 720 ft³ / 20.4 m³ | 966 ft³ / 27.4 m³ | 1,555 ft³ / 44.1 m³ | 1,826 ft³ / 51.7 m³ |
Takeoff run | 6,161 ft (1,878 m) | 6,699 ft (2,042 m) | 7,598 ft (2,316 m) | 9,800 ft (3,000 m) |
Flight envelope | 41,000 feet (12,497 m) Ceiling, Mach 0.82 (470 kn; 871 km/h) MMo | |||
Cruise | Mach 0.785 (453 kn; 838 km/h) | Mach 0.781 (450 kn; 834 km/h) | Mach 0.789 (455 kn; 842 km/h) | Mach 0.79 (455 kn; 844 km/h) |
Range | 3,235 nmi (5,991 km) | 3,010 nmi (5,570 km) | 2,935 nmi (5,436 km) | 2,950 nmi (5,460 km) |
Engines (× 2) | CFM56-7B18/20/22 | CFM56-7B20/22/24/26/27 | CFM56-7B24/26/27 | |
Thrust (× 2) | 20,000–22,000 lbf
89–98 kN |
20,000–26,000 lbf
89–116 kN |
24,000–27,000 lbf
110–120 kN |
24,000–27,000 lbf
110–120 kN |
Cruise max. thrust | 5,960 lbf (26.5 kN) (climb) | |||
Engine dimensions | Fan tip diameter: 61 in (155 cm), length: 103.50 in (263 cm) | |||
Engine ground clearance | 18 in / 46 cm | 19 in / 48 cm | ||
ICAO Type | B736 | B737 | B738 | B739 |
Variant | 737 MAX 7 | 737 MAX 8 / MAX 200 | 737 MAX 9 | 737 MAX 10 |
---|---|---|---|---|
Cockpit crew | Two | |||
Seating | 138 (8J + 130Y) to 172 max | 162 (12J + 150Y) to 210 max | 178 (16J + 162Y) to 220 max | 188 to 230 max |
Seat pitch | 28–29 in (71–74 cm) in high density, 31–32 in (79–81 cm) in economy, 36 in (91 cm) in business | |||
Cargo capacity | 1,146 cu.ft / 32.45 m³ | 1,543 cu.ft / 43.69 m³ | 1,814 cu.ft / 51.37 m³ | |
Length | 116 ft 8 in / 35.56 m | 129 ft 8 in / 39.52 m | 138 ft 4 in / 42.16 m | 143 ft 8 in / 43.8 m |
Wingspan | 117 ft 10 in / 35.92 m | |||
Wing Area | 1,370 sq ft (127 m2) | |||
Overall height | 40 ft 4 in / 12.3 m | |||
Maximum takeoff weight | 177,000 lb / 80,286 kg | 181,200 lb / 82,191 kg | 194,700 lb / 88,314 kg | |
Maximum landing weight | 145,600 lb / 66,043 kg | 152,800 lb / 69,309 kg | 163,900 lb / 74,344 kg | |
Maximum zero fuel weight | 138,700 lb / 62,913 kg | 145,400 lb / 65,952 kg | 156,500 lb / 70,987 kg | |
Operating empty weight | 99,360 lb / 45,070 kg | |||
Fuel capacity | 6,820 USgal / 25,817 L, excluding ACT | |||
Engine (× 2) | CFM International LEAP-1B, 69 in (175 cm) Fan diameter | |||
Thrust (× 2) | 26,786–29,317 lbf (119–130 kN) | |||
Cruising speed | Mach 0.79 (453 kn; 839 km/h) | |||
Range (2-class) | 3,850 nmi / 7,130 km | 3,550 nmi / 6,570 km
MAX 200: 2,700 nmi (5,000 km) |
3,550 nmi / 6,570 km | 3,300 nmi / 6,110 km |
Ceiling | 41,000 ft (12,000 m) | |||
ICAO Type | B37M | B38M | B39M | B3JM |
Variant | 747-400 | 747-400ER | 747-400F | 747-400ERF | 747-8 | 747-8F |
---|---|---|---|---|---|---|
Cockpit crew | Two | |||||
Capacity | 416 (23F @ 61" + 80J @ 39" + 313Y @ 32") | 274,100 lb / 124,330 kg | 273,400 lb / 124,010 kg | 410 in 3-class | 303,700 lb / 137,700 kg | |
Unit Load Devices | 30 LD1/LD3 | 28 LD1/LD3 | + 2 LD1 + 30 x 96 by 125-in pallet on Main deck | |||
Exit limit | 550/660 | 605 | 8 | |||
Overall length | 231 ft 10 in (70.66 m) | 250 ft 2 in / 76.3 m | ||||
Wingspan | 211 ft 5 in (64.44 m) | 224 ft 7 in / 68.4 m | ||||
Wing area | 5,650 sq ft (525 m2) | 554 m2 (5,960 sq ft) | ||||
Aspect ratio | 7.91 | - | ||||
Overall height | 63 ft 8 in (19.4 m) | 63 ft 6 in / 19.4 m | ||||
Max. takeoff weight | 875,000 lb / 396,890 kg | 910,000 lb / 412,775 kg | 875,000 lb / 396,890 kg | 910,000 lb / 412,775 kg | 987,000 lb / 447,700 kg | |
Operating empty weight | 404,600 lb / 183,520 kg | 412,300 lb / 187,010 kg | 360,900 lb / 163,700 kg | 361,600 lb / 164,020 kg | 485,300 lb / 220,128 kg | 434,600 lb / 197,131 kg |
Fuel capacity | 57,285 US gal (216,840 L) | 63,705 US gal (241,140 L) | 53,985 US gal / 204,350L | 63,034 US gal / 238,610L | 59,734 US gal / 226,118L | |
Cruise | Mach 0.855 (504 kn; 933 km/h) | Mach 0.845 (498 kn; 922 km/h) | Mach 0.86 (493 kn; 914 km/h) | Mach 0.85 (488 kn; 903 km/h) | ||
Airspeed limit | Mach 0.92 (542 kn; 1,004 km/h) | Mach 0.9 (516 kn; 956 km/h) | ||||
Takeoff field length | 9,700 ft / 2,955m | 10,700 ft / 3,260m | 9,550 ft / 2,910m | 10,700 ft / 3,260m | - | |
Range | 7,285nmi / 13,490 km | 7,585nmi / 14,045 km | 2,825nmi / 5,230 km | 4,045nmi / 7,585 km | 8,000 nmi (15,000 km) | 4,120nmi / 7,630 km |
Engines (x 4) | PW4000 / GE CF6 / RR RB211 | PW4000 / GE CF6 | PW4000 / GE CF6 / RR RB211 | PW4000 / GE CF6 | GEnx-2B67 | |
Thrust (x 4) | 56,500–63,300 lbf (251–282 kN) | 62,100–63,300 lbf (276–282 kN) | 56,400–63,300 lbf (251–282 kN) | 62,100–63,300 lbf (276–282 kN) | 66,500 lbf (296 kN) | |
ICAO Type | B744 | B748 |
Variant | 757-200 | 757-200F | 757-300 |
---|---|---|---|
Cockpit crew | Two | ||
2-class seating | 200 (12F+188Y) | - | 243 (12F+231Y) |
1-class seating | 221/228, 239 max | 5 max | 280, 295 max |
Cargo volume | 1,670 ft³ / 43.3 m³ | 6,600 ft³ / 187 m³ | 2,370 ft³ / 61.7 m³ |
Width | 148 in / 3.76 m fuselage, 139.3 in / 3.54 m cabin | ||
Length | 155 ft 3 in / 47.3 m | 178 ft 7 in / 54.4 m | |
Height | 44 ft 6 in / 13.6 m | ||
Wing | 124 ft 10 in / 38.0 m span, 1,994 sq ft (185.25 m2) area, 25° sweep, 7.8 AR | ||
MTOW | 255,000 lb / 115,660 kg | 273,000 lb / 123,830 kg | |
Max. Payload | 57,160 lb / 25,920 kg | 84,420 lb / 38,290 kg | 68,140 lb / 30,910 kg |
OEW | 128,840 lb / 58,440 kg | 115,580 lb / 52,430 kg | 141,860 lb / 64,340 kg |
Fuel capacity | 11,489 US gal / 43,490 L | 11,276 US gal / 42,680 L | 11,466 US gal / 43,400 L |
Speed | Cruise Mach 0.8 (461 kn; 854 km/h), Max. Mach 0.86 (496 kn; 918 km/h) | ||
Range | 3,915nmi / 7,250 km | 2,935nmi / 5,435 km | 3,400nmi / 6,295 km |
Takeoff | 6,800 ft / 2,070 m | 6,900 ft / 2,103 m | 8,550 ft / 2,605 m |
Ceiling | 42,000 ft (13,000 m) | ||
Engines (×2) | 40,200–43,500 lbf (179–193 kN) Rolls-Royce RB211-535E4(B)
36,600–42,600 lbf (163–189 kN) Pratt & Whitney PW2000-37/40/43 | ||
ICAO Type | B752 | B753 |
Variant | 767-200 | 767-200ER | 767-300 | 767-300ER | 767-300F | 767-400ER |
---|---|---|---|---|---|---|
Cockpit crew | Two | |||||
3-class | 174 (15F, 40J, 119Y) | 210 (18F, 42J, 150Y) | 15,469 ft³ / 438m³
58-ton / 52.7 tonnes 24 88×108in pallets |
243 (16F, 36J, 189Y) | ||
2-class | 214 (18J, 196 Y) | 261 (24J, 237Y) | 296 (24J, 272Y) | |||
1-class | 245Y | 290Y | 409Y | |||
Exit limit | 290 | 351 | 375 | |||
Cargo | 3,070 ft³ / 86.9m³ | 4,030 ft³ / 114.1m³ | 4,905 ft³ / 138.9m³ | |||
ULDs | 22 LD2s | 30 LD2s | 38 LD2s | |||
Length | 159 ft 2in / 48.51m | 180 ft 3in / 54.94m | 201 ft 4in / 61.37m | |||
Wingspan | 156 ft 1in / 47.57m | 170 ft 4in / 51.92m | ||||
Wing | 3,050 ft² / 283.3m², 31.5° sweepback | 3,130 ft² / 290.7m² | ||||
Fuselage | 17 ft 9in / 5.41m height, 16 ft 6in / 5.03m width, 186in/ 4.72m Cabin width | |||||
MTOW | 315,000 lb / 142,882 kg | 395,000 lb / 179,169 kg | 350,000 lb / 158,758 kg | 412,000 lb / 186,880 kg | 450,000 lb / 204,116 kg | |
Max. payload | 73,350 lb (33,271 kg) | 78,390 lb (35,557 kg) | 88,250 lb (40,030 kg) | 96,560 lb (43,799 kg) | 119,000 lb (53,977 kg) | 101,000 lb (45,813 kg) |
OEW | 176,650 lb / 80,127 kg | 181,610 lb / 82,377 kg | 189,750 lb / 86,069 kg | 198,440 lb / 90,011 kg | 190,000 lb / 86,183 kg | 229,000 lb / 103,872 kg |
Fuel capacity | 16,700USgal / 63,217L | 24,140Usgal / 91,380L | 16,700USgal / 63,216L | 24,140USgal / 91,380L | ||
111,890 lb / 50,753 kg | 161,738 lb / 73,363 kg | 111,890 lb / 50,753 kg | 161,740 lb / 73,364 kg | |||
Range | 3,900 nmi (7,200 km) | 6,590nmi / 12,200 km | 3,900 nmi (7,200 km) | 5,980nmi / 11,070 km | 3,225nmi / 6,025 km | 5,625nmi / 10,415 km |
Cruise | Long range: 459 kn (850 km/h), Maximum: 486 kn (900 km/h) at 39,000 ft (12,000 m), Ceiling: 43,100 ft (13,100 m) | |||||
Takeoff | 6,300 ft (1,900 m) | 2,480m / 8,150 ft | 9,200 ft (2,800 m) | 2,650m / 8,700 ft | 3,290m / 10,800 ft | |
Engines (×2) | P&W JT9D-7R4/7R4E / P&W PW4052 / GE CF6-80A/A2/C2-B2 | P&W JT9D-7R4/7R4E / P&W PW4052/56 / GE CF6-80A/A2/C2-B2/C2-B4 / RB211-524G/H | P&W JT9D-7R4/7R4E / P&W PW4052 / GE CF6-80A/A2/C2-B2 / RB211-524H | GE CF6-80C2-B4/0C2-B6/C2-B8F/C2-B7F1 / PW4056/60/62 / RB211-524G/H | GE CF6-80C2-B8F/C2-B7F1 / PW4062 | |
Thrust (×2) | 48,000–52,500 lbf (214–234 kN) | 48,000–60,600 lbf (214–270 kN) | 48,000–60,600 lbf (214–270 kN) | 56,750–61,500 lbf (252–274 kN) | 60,600 lbf (270 kN) | |
ICAO Type | B762 | B763 | B764 |
Variant | 777-200 | 777-200ER | 777-200LR | 777F | 777-300 | 777-300ER |
---|---|---|---|---|---|---|
Cockpit crew | Two | |||||
3-class | 305 (24F/54J/227Y) | 301 (16F/58J/227Y) | 368 (30F/84J/254Y) | 365 (22F/70J/273Y) | ||
2-class/capacity | 313 | 317 | 224,900 lb / 102,010 kg | 396 | ||
Exit limit | 440 | 11 | 550 | |||
Length | 209 ft 1 in / 63.73 m | 242 ft 4 in / 73.86 m | ||||
Wingspan | 199 ft 11 in / 60.93 m | 212 ft 7 in / 64.80 m | 199 ft 11 in / 60.93 m | 212 ft 7 in / 64.80 m | ||
Wing sweep | 31.6° | |||||
Wing area | 4,605 sq ft (427.8 m2) | 4,702 sq ft (436.8 m2) | 4,605 sq ft (427.8 m2) | 4,702 sq ft (436.8 m2) | ||
Aspect ratio | 8.68 | 9.04 | 8.68 | 9.04 | ||
Tail height | 60 ft 9 in / 18.5 m | 61 ft 1 in / 18.6 m | 60 ft 8 in / 18.5 m | |||
Cabin width | 231 in / 5.86 m | |||||
Seat width | 18.5 in / 47 cm at 9 abreast, 17 in / 43 cm at 10 abreast | |||||
Fuselage width | 20 ft 4 in / 6.20 m | |||||
Maximum cargo capacity | 5,330 ft³ / 150.9 m³ | 23,051 ft³ / 652.7 m³ | 7,120 ft³ / 201.6 m³ | |||
Maximum takeoff weight (MTOW) | 545,000 lb / 247,200 kg | 656,000 lb / 297,550 kg | 766,000 lb / 347,452 kg | 766,800 lb / 347,815 kg | 660,000 lb / 299,370 kg | 775,000 lb / 351,533 kg |
Max. 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 |
Operating empty weight | 299,550 lb / 135,850 kg | 304,500 lb / 138,100 kg | 320,000 lb / 145,150 kg | 318,300 lb / 144,379 kg | 353,800 lb / 160,530 kg | 370,000 lb / 167,829 kg |
Fuel capacity | 31,000 US gal / 117,340 L / 207,700 lb / 94,240 kg | 45,220 US gal / 171,171 L / 302,270 lb / 137,460 kg | 47,890 US gal / 181,283 L / 320,863 lb / 145,538 kg | 45,220 US gal / 171,171 L / 302,270 lb / 137,460 kg | 47,890 US gal / 181,283 L / 320,863 lb / 145,538 kg | |
Service ceiling | 43,100 ft (13,100 m) | |||||
Cruise speed | Mach 0.84 (892 km/h; 554 mph) | |||||
Max. speed | Mach 0.89 (945 km/h; 587 mph) | |||||
Range | 5,240 nmi / 9,700 km | 7,065 nmi / 13,080 km | 8,555 nmi / 15,843 km | 4,970 nmi / 9,200 km | 6,030 nmi / 11,165 km | 7,370 nmi / 13,649 km |
Takeoff distance | 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 |
Turbofan (×2) | PW 4077
RR 877 GE90-77B |
PW 4090
RR 895 GE90-94B |
GE90-110B1
GE90-115B |
PW 4098
RR 892 GE90-92B/-94B |
GE90-115B | |
Max thrust (×2) | 77,200 lbf (343 kN) | 93,700 lbf (417 kN) | 115,300 lbf (513 kN) | 98,000 lbf (440 kN) | 115,300 lbf (513 kN) | |
ICAO Type | B772 | B77L | B773 | B77W |
Variant | 787-8 | 787-9 | 787-10 |
---|---|---|---|
Cockpit crew | Two | ||
Seating, 2-class | 242 : 24J @85" + 218Y @32" | 290 : 28J @85" + 262Y @32" | 330 : 32J @85" + 298Y @32" |
Seating, 1-class | max. 359, exit limit 381 | max. 406, exit limit 420 | max. 440, exit limit 440 |
Length | 186 ft 1 in (56.72 m) | 206 ft 1 in (62.81 m) | 224 ft (68.28 m) |
Wing | 197 ft 3 in (60.12 m) span, 246.9 in / 6.27 m mean chord, 9.59 aspect ratio, 4,058 sq ft (377 m2) area | ||
Wing sweep | 32.2° | ||
Height | 55 ft 6 in (16.92 m) | 55 ft 10 in (17.02 m) | |
Fuselage | Cabin width: 18 ft 0 in (5.49 m) External width: 18 ft 11 in (5.77 m), height: 19 ft 6 in (5.94 m) | ||
Cargo capacity | 4,826 ft³ /136.7 m³
28 LD3 or 9 (88×125) pallets |
6,090 ft³ / 172.5 m³
36 LD3 or 11 (96×125) pallets |
6,722 ft³ / 191.4 m³
40 LD3 or 13 (96×125) pallets |
MTOW | 502,500 lb / 227,930 kg | 560,000 lb / 254,011 kg | |
MLW | 380,000 lb / 172,365 kg | 425,000 lb / 192,777 kg | 445,000 lb / 201,849 kg |
Maximum ZFW | 355,000 lb / 161,025 kg | 400,000 lb / 181,437 kg | 425,000 lb / 192,777 kg |
OEW | 264,500 lb / 119,950 kg | 284,000 lb / 128,850 kg | 298,700 lb / 135,500 kg |
Fuel capacity | 33,340 US gal / 126,206 L
223,378 lb / 101,323 kg |
33,384 US gal / 126,372 L
223,673 lb / 101,456 kg | |
Speed | Max: Mach 0.90 (516 kn; 956 km/h); Cruise: Mach 0.85 (488 kn; 903 km/h) | ||
Range | 7,355 nmi (13,620 km) | 7,635 nmi (14,140 km) | 6,430 nmi (11,910 km) |
Takeoff | 8,500 ft (2,600 m) | 9,300 ft (2,800 m) | 9,100 ft (2,800 m) |
Ceiling | 43,000 ft (13,100 m) | ||
Engines (×2) | General Electric GEnx-1B or Rolls-Royce Trent 1000 | ||
Thrust (×2) | 64,000 lbf (280 kN) | 71,000 lbf (320 kN) | 76,000 lbf (340 kN) |