常见航空器规格和性能参数:修订间差异
Kejia Deng(讨论 | 贡献) 无编辑摘要 |
小无编辑摘要 |
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{|{{Infobox aircraft begin | |||
|name= Boeing 737 | |||
|image= File:South African Airlink Boeing 737-200 Advanced Smith.jpg<!-- In-flight images are preferred for aircraft; please consult talk page before changing. --> | |||
|caption=A Boeing 737-200, the first mass-produced 737 model, in operation with [[Airlink|South African Airlink]] in 2007 | |||
|alt= | |||
}}{{Infobox aircraft type | |||
|type= [[Narrow-body aircraft|Narrow-body]] [[jet airliner]] and [[Business jet]] | |||
|national origin= United States | |||
|manufacturer= [[Boeing Commercial Airplanes]] | |||
|first flight= April 9, 1967 | |||
|introduced= February 10, 1968, with [[Lufthansa]] | |||
|retired= | |||
|status= In service | |||
|primary user= [[Southwest Airlines]] <!--Limit one (1) primary user. Top 4 users listed in 'primary user' and 'more users' fields based on number of 737s in their fleets. --> | |||
|more users= [[Ryanair]] <br>[[United Airlines]] <br>[[American Airlines]]<!--Limit is three (3) in 'more users' field (4 total users). Please separate with <br />.--> | |||
|produced= 1966–present | |||
|number built= 10,000 (March 13, 2018)<ref name=Flight13march2018/> | |||
|unit cost= −100: [[United States dollar|US$]]32M{{sfn|Bowers|1989|p=495|ps=}}{{when|date=January 2018}}<!-- $32M seems an awful lot for a -100 last delivered in 1969, while a larger -200 was sold for $5.2M 3 years later; more than a 747!--><br/>-200: US$5.2M (1972)<ref>{{cite magazine |url= https://www.flightglobal.com/pdfarchive/view/1972/1972%20-%202020.html |title= Airliner price index |magazine= Flight International |date= 10 August 1972 |page= 183}}</ref> | |||
|variants with their own articles= [[Boeing T-43]] | |||
|developed into= [[Boeing 737 Classic]] <br>[[Boeing 737 Next Generation]] <br>[[Boeing 737 MAX]] | |||
}} | |||
|} | |||
{| class="wikitable" style="text-align: center" | {| class="wikitable" style="text-align: center" | ||
|+ | |+ | ||
第822行: | 第845行: | ||
{| class="wikitable" style="text-align: center" | {| class="wikitable" style="text-align: center" | ||
|+Airbus A320 family characteristics | |||
|- | |- | ||
! | !Subtype | ||
! A318 | !A318 | ||
! A319 | !A319 | ||
! A320 | !A320 | ||
! A321 | !A321 | ||
|- | |- | ||
! | !Cockpit crew | ||
| colspan="4" style="text-align:center;" | | | colspan="4" style="text-align:center;" |Two | ||
|- | |- | ||
! | !Exit limit EASA/FAA | ||
|136 | |136 | ||
|160 | |160 | ||
第838行: | 第862行: | ||
|230 | |230 | ||
|- | |- | ||
! | !1-class max. seating | ||
|132 at | |132 at 29–30 in (74–76 cm) pitch | ||
|156 at | |156 at 28–30 in (71–76 cm) pitch | ||
|186 at | |186 at 29 in (74 cm) pitch | ||
|236 at | |236 at 28 in (71 cm) pitch | ||
|- | |- | ||
! | !1-class, typical | ||
|117 at | |117 at 32 in (81 cm) pitch | ||
|134 at | |134 at 32 in (81 cm) pitch | ||
|164 at | |164 at 32 in (81 cm) pitch | ||
|199 at | |199 at 32 in (81 cm) pitch | ||
|- | |- | ||
! | !2-class, typical | ||
|107 (8F @ | |107 (8F @ 38 in, 99Y @ 32 in) | ||
|124 (8F @ | |124 (8F @ 38 in, 116Y @ 32 in) | ||
|150 (12F @ | |150 (12F @ 36 in, 138Y @ 32 in) | ||
|185 (16F @ | |185 (16F @ 36 in, 169Y @ 32 in) | ||
|- | |- | ||
! | !Cargo volume | ||
|21.20 m<sup>3</sup> (749 cu ft) | |||
|27.70 m<sup>3</sup> (978 cu ft) | |||
|37.40 m<sup>3</sup> (1,321 cu ft) | |||
|51.70 m<sup>3</sup> (1,826 cu ft) | |||
|- | |- | ||
! | !Unit load devices | ||
| | | | ||
|4× LD3-45 | |4× LD3-45 | ||
第868行: | 第892行: | ||
|10× 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 | ||
| | | colspan="4" |7.59 m (24 ft 11 in) | ||
|- | |- | ||
! | !Wingspan | ||
|colspan=" | |34.10 m (111 ft 11 in) | ||
| colspan="3" |35.8 m (117 ft 5 in) | |||
|- | |- | ||
! | !Wing area | ||
| | ||| colspan="2" |124 m<sup>2</sup> (1,330 sq ft), 10.3 aspect ratio | ||
|colspan=" | |128 m<sup>2</sup> (1,380 sq ft), 10 <abbr>AR</abbr> | ||
|- | |- | ||
! | !Wing sweepback | ||
| colspan="4" |25 degrees | |||
|- | |- | ||
! | !Tail height | ||
|12.56 m (41 ft 2 in) | |||
| colspan="3" |11.76 m (38 ft 7 in) | |||
|- | |- | ||
! colspan= | !Fuselage | ||
| colspan="4" |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 | ||
| | | colspan="4" |Cruise: Mach 0.78 (447 kn; 829 km/h), <abbr>MMO</abbr>: 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) | ||
|6, | |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) | ||
| | | - | ||
|- | |- | ||
! colspan= | !Service ceiling | ||
| colspan="4" |39,100–41,000 ft (11,900–12,500 m) | |||
|- | |- | ||
! | !Engines (×2) | ||
|colspan="4" | | | colspan="4" |CFM International CFM56-5B, 68.3 in (1.73 m) fan | ||
|- | |- | ||
! | ! | ||
| colspan=" | |PW6000A, 56.5 in (1.44 m) fan | ||
| colspan="3" |IAE V2500A5, 63.5 in (1.61 m) fan | |||
|- | |- | ||
| | !Thrust (×2) | ||
|colspan=" | |96–106 kN (22,000–24,000 lb<sub>f</sub>) | ||
| colspan="2" |98–120 kN (22,000–27,000 lb<sub>f</sub>) | |||
|133–147 kN (30,000–33,000 lb<sub>f</sub>) | |||
|- | |- | ||
! | ! | ||
! | |||
! | |||
! | |||
! | |||
|} | |} | ||
{| class="wikitable" style="text-align: center" | {| class="wikitable" style="text-align: center" | ||
|+ Airbus family | |+ Airbus A320neo family characteristics | ||
|- | |- | ||
!Variant | !Variant | ||
第975行: | 第1,010行: | ||
!A321neo | !A321neo | ||
|- | |- | ||
! Cockpit crew | !Cockpit crew | ||
| colspan="3" | Two | | colspan="3" |Two | ||
|- | |- | ||
! 2- | !2-class seats | ||
| 140 | |140 | ||
| 165 | |165 | ||
| 206: 16 | |206: 16<abbr>J</abbr> @36 in + 190<abbr>Y</abbr> @30 in | ||
|- | |- | ||
! 1-class maximum | !1-class maximum | ||
| 160 | |160 | ||
| | |195 @ 27 in | ||
| 240 @ | |240 @ 28 in | ||
|- | |- | ||
! | !Seat width | ||
| colspan="3" | | | colspan="3" |Economy at 6 abreast: 18 in (46 cm), 3.7 m (12 ft 1 in) cabin width | ||
|- | |- | ||
! Cargo capacity | !Cargo capacity | ||
| | |27 m³ (976 ft³) | ||
| | |37 m³ (1,322 ft³) | ||
| | |51 m³ (1,828 ft³) | ||
|- | |- | ||
! Length | !Length | ||
| 33. | |33.84 m (111 ft) | ||
| 37. | |37.57 m (123 ft 3 in) | ||
| 44. | |44.51 m (146 ft) | ||
|- | |- | ||
! Wingspan | !Wingspan | ||
| colspan="3" | 35. | | colspan="3" |35.80 m (117 ft 5 in) | ||
|- | |- | ||
! Height | !Height | ||
| colspan="3" | 11. | | colspan="3" |11.76 m (38 ft 7 in) | ||
|- | |- | ||
! | !Max. takeoff weight | ||
| 75. | |75.5 t (166,400 lb) | ||
| | |79 t (174,200 lb) | ||
| | |97 t (213,800 lb) | ||
|- | |- | ||
! Max. | !Max. payload | ||
|17.7 t (39,000 lb) | |||
| | |20 t (44,100 lb) | ||
|25.5 t (56,200 lb) | |||
|- | |- | ||
! Operating empty | !Operating empty | ||
| | |42.6 t (93,900 lb) | ||
| | |44.3 t (97,700 lb) | ||
| | |50.1 t (110,500 lb) | ||
|- | |- | ||
! | !Fuel capacity | ||
| colspan="2" | 26,730 l (7,060 USg) | | colspan="2" |26,730 l (7,060 USg) | ||
| 32,940 l (8,700 USg) | |32,940 l (8,700 USg) | ||
|- | |- | ||
! Engines (×2) | !Engines (×2) | ||
| colspan="3" | | | colspan="3" |CFM International LEAP-1A or Pratt & Whitney PW1100G | ||
|- | |- | ||
! Fan diameter | !Fan diameter | ||
| colspan="3" |PW1100G: | | colspan="3" |PW1100G: 81 in (206 cm), LEAP-1A: 78 in (198 cm) | ||
|- | |- | ||
! Max. | !Max. Thrust | ||
| | |107 kN (24,100 lbf) | ||
|120.6 kN (27,120 lbf) | |||
|147.3 kN (33,110 lbf) | |||
|- | |- | ||
! Speed | !Speed | ||
| colspan="3" | Cruise: | | colspan="3" |Cruise: Mach 0.78 (450 kn; 833 km/h), Max.: Mach 0.82 (473 kn; 876 km/h) | ||
|- | |- | ||
! Ceiling | !Ceiling | ||
| colspan=3 | | | colspan="3" |39,100–39,800 ft (11,900–12,100 m) | ||
|- | |- | ||
! Typical range | !Typical range | ||
| 6, | |6,950 km / 3,750 nmi | ||
| 6, | |6,500 km / 3,500 nmi | ||
|7, | |7,400 km / 4,000 nmi | ||
|- | |- | ||
! Takeoff | !Takeoff | ||
| | | - | ||
| | | - | ||
| | |1,988 m (6,522 ft) | ||
|- | |- | ||
! ICAO Type | !ICAO Type | ||
|A19N | |A19N | ||
|A20N | |A20N | ||
第1,060行: | 第1,095行: | ||
{| class="wikitable" style="text-align: center" | {| class="wikitable" style="text-align: center" | ||
|+ Airbus A330 | |+ Airbus A330 characteristics | ||
! | !Variant | ||
! A330-200 | !A330-200 | ||
! A330-200F | !A330-200F | ||
! A330-300 | ! A330-300 | ||
|- | |- | ||
! Cockpit crew | !Cockpit crew | ||
| colspan=3 | Two | | colspan="3" |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 | ||
| colspan="2" |58.82 m (192.98 ft) | |||
|63.67 m (208.89 ft) | |||
|- | |- | ||
! | !Span | ||
| colspan=" | | colspan="3" |Wing: 60.3 m (197.83 ft), Main gear: 12.61 m (41.37 ft) | ||
|- | |- | ||
! | !Wing | ||
| colspan="3" | | | colspan="3" |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 | ||
| | | colspan="3" |5.64 m (222 in) diameter, 5.18 m (204 in) cabin width | ||
| | |||
|- | |- | ||
! | !Seat width | ||
| colspan="3" | | | colspan="3" |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) | ||
| | | colspan="2" |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 | !Max Payload | ||
| | |49,400 kg (108,900 lb) | ||
| | |68,600 kg (151,200 lb) | ||
| | |45,600 kg (100,500 lb) | ||
|- | |- | ||
! | !Fuel capacity | ||
| | | colspan="3" |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 | ||
| | | colspan="3" |Mach 0.82 (470 kn; 871 km/h) (Mach 0.86 (493 kn; 914 km/h) M<sub>MO</sub>), 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) | ||
| colspan="3" |Takeoff: 2,770 m (9,110 ft), Landing: 1,730 m (5,680 ft) | |||
| | |||
|- | |- | ||
! | !Engines (×2) | ||
| colspan="3" | | | colspan="3" |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 | |||
|} | |} | ||
{| class="wikitable" style="text-align: center" | {| class="wikitable" style="text-align: center" | ||
|- | |- | ||
! Variant | !Variant | ||
! A340- | !A340-300 | ||
! A340- | !A340-600 | ||
|- | |||
!Cockpit crew | |||
| colspan="2" |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. | |63.45 m / 208.17 ft | ||
|- | |- | ||
! | !Wing | ||
| | |363.1 m<sup>2</sup> (3,908 sq ft), 29.7° sweep, 10 AR | ||
| | |437.3 m<sup>2</sup> (4,707 sq ft), 31.1° sweep, 9.2 AR | ||
|- | |- | ||
! | !Height | ||
| | |16.99 m / 55.72 ft | ||
| | |17.93 m / 58.84 ft | ||
|- | |- | ||
! | !Fuselage | ||
| | | colspan="2" |5.287 m / 208.15 in cabin width, 5.64 m / 18.5 ft outside width | ||
| | |||
|- | |- | ||
! | !Cargo volume | ||
| | |132.4 m<sup>3</sup> (4,680 cu ft) | ||
|201.7 m<sup>3</sup> (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 lb<sub>f</sub>) | ||
| | |248.12–275.35 kN (55,780–61,902 lbf) | ||
|- | |- | ||
! | !Speed | ||
| colspan=2| | | colspan="2" |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 | ||
|} | |} | ||
{| class="wikitable" style="text-align: center" | {| class="wikitable" style="text-align: center" | ||
|+ A350 | |+ A350 and A380 characteristics | ||
! | !Variant | ||
!A350-900 | !A350-900 | ||
!A350-1000 | !A350-1000 | ||
!A380-800 | |||
|- | |- | ||
!Cockpit crew | |||
|colspan=" | | colspan="3" |Two | ||
|- | |- | ||
!Seating | |||
|325/315 (48B+267Y) | |325/315 (48B+267Y) | ||
|366/369 (54B+315Y) | ULR: 173=80J+93Y | ||
|366/369 (54B+315Y) | |||
387 (2-class) | |||
|544 (4-class) | |||
|- | |- | ||
!Exit limit | |||
|colspan=2 |440 | | colspan="2" |440 | ||
|868 | |||
|- | |- | ||
!Overall length | |||
|66.8 m / 219. | |66.8 m / 219.5 ft | ||
|73.78 m / 242. | |73.78 m / 242.7 ft | ||
|72.72 m / 238 ft 7 in | |||
|- | |- | ||
!Wingspan | |||
|colspan="2" |64.75 m / 212. | | colspan="2" |64.75 m / 212.43 ft | ||
|79.75 m / 261 ft 8 in | |||
|- | |- | ||
!Aspect ratio | |||
| | |9.49 | ||
| | |9.03 | ||
|7.53 | |||
|- | |- | ||
!Wing area | |||
| | |442 m<sup>2</sup> (4,760 sq ft) | ||
| | |464.3 m<sup>2</sup> (4,998 sq ft) | ||
|845 m<sup>2</sup> (9,100 sq ft) | |||
|- | |- | ||
!Overall height | |||
|17.05 m / | |17.05 m / 55 ft 11 in | ||
|17.08 m / | |17.08 m / 56 ft 0 in | ||
|24.09 m / 79 ft 0 in | |||
|- | |- | ||
!Fuselage | |||
|colspan="2" |5.96 m / 19. | | colspan="2" |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 | |||
|colspan="2" |5.61 m / | | colspan="2" |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, | |280 t / 617,295 lb | ||
|316 t / 696, | |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, | |129 t (284,000 lb) | ||
| - | |||
|- | |- | ||
!Cargo capacity | |||
| | |36 LD3 or 11 pallets | ||
|44 LD3 or 14 pallets | |44 LD3 or 14 pallets | ||
| - | |||
|- | |- | ||
!cruise | |||
|colspan="2" | | | colspan="2" |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 | |15,000 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×) | |||
|colspan="2" | | | colspan="2" |Rolls-Royce Trent XWB | ||
|Engine Alliance GP7200 / Rolls-Royce Trent 900 | |||
|- | |- | ||
!Maximum thrust | |||
|374. | |374.5 kN / 84,200 lbf | ||
|431. | |431.5 kN / 97,000 lbf | ||
| | |311 kN (70,000 lbf) | ||
|- | |- | ||
! | !ICAO Type | ||
|A359 | |||
|A35K | |||
|A388 | |||
| | |||
| | |||
| | |||
|} | |} |
2022年1月25日 (二) 12:25的最新版本
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) |
ICAO Type | B788 | B789 | B78X |
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) | |
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 |
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 |
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 |