常见航空器规格和性能参数

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Kejia Deng讨论 | 贡献2018年7月21日 (六) 20:23的版本
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Boeing 737 Next Generation Characteristics
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
Boeing 737 MAX Characteristics
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
Boeing 747 Characteristics
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
Boeing 757 Characteristics
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
767 Airplane Characteristics
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
Boeing 777 specifications
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
Boeing 787 Dreamliner characteristics
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)
ICAO Type B788 B789 B78X
Airbus A320 family characteristics
Subtype A318 A319 A320 A321
Cockpit crew Two
Exit limit EASA/FAA 136 160 195/190 230
1-class max. seating 132 at 29–30 in (74–76 cm) pitch 156 at 28–30 in (71–76 cm) pitch 186 at 29 in (74 cm) pitch 236 at 28 in (71 cm) pitch
1-class, typical 117 at 32 in (81 cm) pitch 134 at 32 in (81 cm) pitch 164 at 32 in (81 cm) pitch 199 at 32 in (81 cm) pitch
2-class, typical 107 (8F @ 38 in, 99Y @ 32 in) 124 (8F @ 38 in, 116Y @ 32 in) 150 (12F @ 36 in, 138Y @ 32 in) 185 (16F @ 36 in, 169Y @ 32 in)
Cargo volume 21.20 m3 (749 cu ft) 27.70 m3 (978 cu ft) 37.40 m3 (1,321 cu ft) 51.70 m3 (1,826 cu ft)
Unit load devices 4× LD3-45 7× LD3-45 10× LD3-45
Length 31.44 m (103 ft 2 in) 33.84 m (111 ft 0 in) 37.57 m (123 ft 3 in) 44.51 m (146 ft 0 in)
Wheelbase 10.25 m (33 ft 8 in) 11.04 m (36 ft 3 in) 12.64 m (41 ft 6 in) 16.91 m (55 ft 6 in)
Track 7.59 m (24 ft 11 in)
Wingspan 34.10 m (111 ft 11 in) 35.8 m (117 ft 5 in) 
Wing area 124 m2 (1,330 sq ft), 10.3 aspect ratio 128 m2 (1,380 sq ft), 10 AR
Wing sweepback 25 degrees
Tail height 12.56 m (41 ft 2 in) 11.76 m (38 ft 7 in)
Fuselage 4.14 m (13 ft 7 in) height, 3.95 m (13 ft 0 in) width, 3.70 m (12 ft 2 in) cabin width
MTOW 68 t (150,000 lb) 75.5 t (166,000 lb) 78 t (172,000 lb) 93.5 t (206,000 lb)
Max. payload 15 t (33,000 lb) 17.7 t (39,000 lb) 19.9 t (44,000 lb) 25.3 t (56,000 lb)
Fuel capacity 24,210 L

6,400 US gal

24,210–30,190 L

6,400–7,980 US gal

24,210–27,200 L

6,400–7,190 US gal

24,050–30,030 L

6,350–7,930 US gal

OEW 39.5 t (87,100 lb) 40.8 t (89,900 lb) 42.6 t (93,900 lb) 48.5 t (107,000 lb)
Speed Cruise: Mach 0.78 (447 kn; 829 km/h), MMO: Mach 0.82 (470 kn; 871 km/h)
Range, typical payload 3,100 nmi, 5,750 km 3,750 nmi, 6,950 km 3,300 nmi, 6,100 km 3,200 nmi, 5,950 km
ACJ range 4,200 nmi, 7,800 km 6,000 nmi, 11,100 km 4,300 nmi, 7,800 km -
Takeoff run (MTOW, SL, ISA) 1,780 m (5,840 ft) 1,850 m (6,070 ft) 2,100 m (6,900 ft) -
Landing (MLW, SL, ISA) 1,230 m (4,040 ft) 1,360 m (4,460 ft) 1,500 m (4,900 ft) -
Service ceiling 39,100–41,000 ft (11,900–12,500 m)
Engines (×2) CFM International CFM56-5B, 68.3 in (1.73 m) fan
PW6000A, 56.5 in (1.44 m) fan IAE V2500A5, 63.5 in (1.61 m) fan
Thrust (×2) 96–106 kN (22,000–24,000 lbf) 98–120 kN (22,000–27,000 lbf) 133–147 kN (30,000–33,000 lbf)
Airbus A320neo family characteristics
Variant A319neo A320neo A321neo
Cockpit crew Two
2-class seats 140 165 206: 16J @36 in + 190Y @30 in
1-class maximum 160 195 @ 27 in 240 @ 28 in
Seat width Economy at 6 abreast: 18 in (46 cm), 3.7 m (12 ft 1 in) cabin width
Cargo capacity 27 m³ (976 ft³) 37 m³ (1,322 ft³) 51 m³ (1,828 ft³)
Length 33.84 m (111 ft) 37.57 m (123 ft 3 in) 44.51 m (146 ft)
Wingspan 35.80 m (117 ft 5 in)
Height 11.76 m (38 ft 7 in)
Max. takeoff weight 75.5 t (166,400 lb) 79 t (174,200 lb) 97 t (213,800 lb)
Max. payload 17.7 t (39,000 lb) 20 t (44,100 lb) 25.5 t (56,200 lb)
Operating empty 42.6 t (93,900 lb) 44.3 t (97,700 lb) 50.1 t (110,500 lb)
Fuel capacity 26,730 l (7,060 USg) 32,940 l (8,700 USg)
Engines (×2) CFM International LEAP-1A or Pratt & Whitney PW1100G
Fan diameter PW1100G: 81 in (206 cm), LEAP-1A: 78 in (198 cm)
Max. Thrust 107 kN (24,100 lbf) 120.6 kN (27,120 lbf) 147.3 kN (33,110 lbf)
Speed Cruise: Mach 0.78 (450 kn; 833 km/h), Max.: Mach 0.82 (473 kn; 876 km/h)
Ceiling 39,100–39,800 ft (11,900–12,100 m)
Typical range 6,950 km / 3,750 nmi 6,500 km / 3,500 nmi 7,400 km / 4,000 nmi 
Takeoff - - 1,988 m (6,522 ft)
ICAO Type A19N A20N A21N
Airbus A330 characteristics
Variant A330-200 A330-200F A330-300
Cockpit crew Two
Capacity 246 (36J @ 60 in + 210Y @ 32 in) 70,000 kg (154,324 lb) 300 (36J @ 60 in + 264Y @ 32 in)
Max seating 406 440
Length 58.82 m (192.98 ft) 63.67 m (208.89 ft)
Span Wing: 60.3 m (197.83 ft), Main gear: 12.61 m (41.37 ft)
Wing 361.6 m² (3,892 ft²), 25% chord wingsweep : 30°, 10.06 Aspect ratio
Tail height 17.39m / 57’ 16.90m / 55’5’’ 16.79m / 55’
Fuselage 5.64 m (222 in) diameter, 5.18 m (204 in) cabin width
Seat width 0.46 m (18 in) in 8 abreast economy, 0.53 m (21 in) in 6 abreast business
Cargo volume 132.4 m³ (4673 ft³) 469.2 m³ (16567 ft³) 158.4 m³ (5591 ft³)
Maximum takeoff weight 242,000 kg (533,519 lb) 233,000 kg (513,677 lb) 242,000 kg (533,519 lb)
Maximum landing weight 182,000 kg (401,241 lb) 187,000 kg (412,264 lb)
Max zero fuel weight 170,000 kg (374,786 lb) 178,000 kg (392,423 lb) 175,000 kg (385,809 lb)
Max Payload 49,400 kg (108,900 lb) 68,600 kg (151,200 lb) 45,600 kg (100,500 lb)
Fuel capacity 139,090 l (36,744 US gal) - 109,185 kg (240,711 lb)
Operating empty weight 120,600 kg (265,900 lb) 109,400 kg (241,200 lb) 129,400 kg (285,300 lb)
Cruise Mach 0.82 (470 kn; 871 km/h) (Mach 0.86 (493 kn; 914 km/h) MMO), 12,500 m (41,100 ft) Service ceiling
Final approach speed (MLW) 136 kn (252 km/h) 139 kn (257 km/h) 137 kn (254 km/h)
Range 13,450 km / 7,250 nm (247 pax) 7,400 km / 4,000 nm 11,750 km / 6,350 nm (277 pax)
Runway (SL, ISA, MTOW/MLW) Takeoff: 2,770 m (9,110 ft), Landing: 1,730 m (5,680 ft)
Engines (×2) 64,530–68,530 lbf (287–305 kN) General Electric CF6-80E1 (except -200F)

64,500–70,000 lbf (287–311 kN) Pratt & Whitney PW4000 PW4164/PW4168/PW4170 67,500–71,100 lbf (300–316 kN) Rolls-Royce Trent 700 768/772

ICAO Type A332 A332 A333
Variant A340-300 A340-600
Cockpit crew Two
Seating 277 (3-class)  or 335 (30F + 305Y) 326  or 380 (12F + 54J + 314Y)
Exit limit 375/440/375 440
Length 63.69 m / 208.96 ft 75.36 m / 247.24 ft
Wingspan 60.3 m / 197.83 ft 63.45 m / 208.17 ft
Wing 363.1 m2 (3,908 sq ft), 29.7° sweep, 10 AR 437.3 m2 (4,707 sq ft), 31.1° sweep, 9.2 AR
Height 16.99 m / 55.72 ft 17.93 m / 58.84 ft
Fuselage 5.287 m / 208.15 in cabin width, 5.64 m / 18.5 ft outside width
Cargo volume 132.4 m3 (4,680 cu ft) 201.7 m3 (7,120 cu ft)
MTOW 276.5 t (610,000 lb) 380 t (840,000 lb)
Max. PL 52 t (115,000 lb) 66 t (146,000 lb)<
OEW 131 t (289,000 lb) 174 t (384,000 lb)
Max. Fuel 110.4 t / 243,395 lb 155.5 t / 342,905 lb 
Engines (×4) CFM International CFM56-5C Trent 556
Thrust (×4) 138.78–151.24 kN (31,200–34,000 lbf) 248.12–275.35 kN (55,780–61,902 lbf)
Speed Mach 0.86 (493 kn; 914 km/h) max, Mach 0.82 (470 kn; 871 km/h) cruise
Range, max pax 7,150 nmi (13,240 km) 7,550 nmi (13,980 km)
Take off 3,000 m (10,000 ft) 3,400 m (11,200 ft)
Ceiling 12,500 m (41,000 ft) 12,527 m (41,100 ft)
ICAO Type A343 A346
A350 and A380 characteristics
Variant A350-900 A350-1000 A380-800
Cockpit crew Two
Seating 325/315 (48B+267Y)

ULR: 173=80J+93Y

366/369 (54B+315Y)

387 (2-class) 

544 (4-class)
Exit limit 440 868
Overall length 66.8 m / 219.5 ft 73.78 m / 242.7 ft 72.72 m / 238 ft 7 in
Wingspan 64.75 m / 212.43 ft 79.75 m / 261 ft 8 in
Aspect ratio 9.49 9.03 7.53
Wing area 442 m2 (4,760 sq ft) 464.3 m2 (4,998 sq ft) 845 m2 (9,100 sq ft)
Overall height 17.05 m / 55 ft 11 in 17.08 m / 56 ft 0 in 24.09 m / 79 ft 0 in
Fuselage 5.96 m / 19.7 ft width, 6.09 m / 19.98 ft height 7.14 m / 23 ft 5 in width, 8.41 m / 27 ft 7 in height
Cabin width 5.61 m / 18 ft 5 in, 9-abreast Seat : 18 in / 46 cm 6.50 m (21 ft 4 in) main deck

5.80 m (19 ft 0 in) upper deck

MTOW 280 t / 617,295 lb 316 t / 696,661 lb 575 t / 1,268,000 lb)
Max. payload 53.3 t (118,000 lb) 64.2 t (142,000 lb) 84 t (185,000 lb)
Fuel capacity 140,795 L (37,194 US gal)

110,523 kg (243,662 lb)

158,791 L (41,948 US gal)

124,651 kg (274,808 lb)

323,545 L / 85,471 USgal
OEW 142.4 t (314,000 lb) typical

134.7–145.1 t (297,000–320,000 lb)

158.8 t (350,000 lb)

155 t (342,000 lb) dry

276.8 t (610,000 lb)
MEW 115.7 t (255,075 lb) 129 t (284,000 lb) -
Cargo capacity 36 LD3 or 11 pallets 44 LD3 or 14 pallets -
cruise Mach 0.85 (488 kn; 903 km/h) Typical, Mach 0.89 (513 kn; 950 km/h) Maximum Mach 0.85 (903 km/h; 488 kn)
Range 15,000 km / 8,100 nmi 15,600 km (8,400 nmi) 15,200 km / 8,200 nmi
Takeoff (MTOW, SL, ISA) 2,600 m (8,500 ft) - 3,000 m (9,800 ft)
Landing (MLW, SL, ISA) 2,000 m (6,600 ft) - -
Service ceiling 43,100 ft (13,100 m) 41,450 ft (12,630 m) 13,100 m (43,000 ft)
Engines (2×) Rolls-Royce Trent XWB Engine Alliance GP7200 / Rolls-Royce Trent 900
Maximum thrust 374.5 kN / 84,200 lbf 431.5 kN / 97,000 lbf 311 kN (70,000 lbf)
ICAO Type A359 A35K A388