常见航空器规格和性能参数:修订间差异
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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" | ||
|+ | |+ | ||
Boeing 737 Next Generation Characteristics | |||
! Variant | |||
! | |||
! 737-600 | ! 737-600 | ||
! 737-700 | ! 737-700 | ||
! 737-800 | ! 737-800 | ||
! 737-900ER | ! 737-900ER | ||
! | |- | ||
! | ! Cockpit crew | ||
! | | colspan="4" | 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 | |||
| colspan="2" | 149 | |||
| 189 | |||
| 220 | |||
|- | |||
! Seat width | |||
| colspan="4" | 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 | |||
| colspan="2" | 41 ft 3 in / 12.57 m | |||
| colspan="2" | 41 ft 2 in (12.55 m) | |||
|- | |- | ||
! | ! Wing | ||
| | | colspan="4" | Span: 112 ft 7 in / 34.32 m, with winglets: 117 ft 5in / 35.79m; Area: 124.60 m<sup>2</sup> (1,341.2 sq ft); Sweepback: 25°; AR: 9.44 | ||
|- | |- | ||
! | ! Fuselage | ||
| colspan=" | | colspan="4" | 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 | ||
| | | colspan="3" | 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 | ||
| colspan="4" | | | colspan="4" |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 0.789 (455 kn; 842 km/h) | ||
| Mach 0.79 (455 kn; 844 km | |Mach 0.79 (455 kn; 844 km/h) | ||
|- | |- | ||
! | ! Range | ||
| 5,991 km | |3,235 nmi (5,991 km) | ||
| 3,010 nmi | |3,010 nmi (5,570 km) | ||
| 5,436 km) | |2,935 nmi (5,436 km) | ||
| 5,460 km | |2,950 nmi (5,460 km) | ||
| | |- | ||
| | ! Engines (× 2) | ||
|CFM56-7B18/20/22 | |||
|CFM56-7B20/22/24/26/27 | |||
| | | colspan="2" |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 | |||
| colspan="4" |5,960 lbf (26.5 kN) (climb) | |||
|- | |||
! Engine dimensions | |||
| colspan="4" |Fan tip diameter: 61 in (155 cm), length: 103.50 in (263 cm) | |||
|- | |- | ||
! | ! Engine ground clearance | ||
| colspan="2" | | | colspan="2" |18 in / 46 cm | ||
| colspan=" | | colspan="2" |19 in / 48 cm | ||
|- | |- | ||
! | ! ICAO Type | ||
|B736 | |B736 | ||
|B737 | |B737 | ||
|B738 | |B738 | ||
|B739 | |B739 | ||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|+ Boeing 737 MAX Characteristics | |||
|- | |||
! Variant !! 737 MAX 7 !! 737 MAX 8 / MAX 200 !! 737 MAX 9 !! 737 MAX 10 | |||
|- | |||
!Cockpit crew | |||
| colspan="4" |Two | |||
|- | |||
!Seating | |||
|138 (8<abbr>J</abbr> + 130<abbr>Y</abbr>) to 172 max | |||
|162 (12<abbr>J</abbr> + 150<abbr>Y</abbr>) to 210 max | |||
|178 (16<abbr>J</abbr> + 162<abbr>Y</abbr>) to 220 max | |||
|188 to 230 max | |||
|- | |||
!Seat pitch | |||
| colspan="4" |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 | |||
| colspan="4" |117 ft 10 in / 35.92 m | |||
|- | |||
!Wing Area | |||
| colspan="4" |1,370 sq ft (127 m<sup>2</sup>) | |||
|- | |||
!Overall height | |||
| colspan="4" |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 | |||
| colspan="4" |6,820 USgal / 25,817 L, excluding <abbr>ACT</abbr> | |||
|- | |||
!Engine (× 2) | |||
| colspan="4" |CFM International LEAP-1B, 69 in (175 cm) Fan diameter | |||
|- | |||
!Thrust (× 2) | |||
| colspan="4" |26,786–29,317 lbf (119–130 kN) | |||
|- | |||
!Cruising speed | |||
| colspan="4" |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 | |||
| colspan="4" |41,000 ft (12,000 m) | |||
|- | |||
!ICAO Type | |||
|B37M | |B37M | ||
| | |B38M | ||
|B39M | |B39M | ||
|B3JM | |B3JM | ||
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{| class="wikitable" style="text-align: center" | {| class="wikitable" style="text-align: center" | ||
|+Boeing 747 Characteristics | |||
|- | |- | ||
! | !Variant | ||
!747-400 | !747-400 | ||
!747-400ER | !747-400ER | ||
!747-400F | !747-400F | ||
!747-400ERF | !747-400ERF | ||
!747-8 | |||
!747-8F | |||
|- | |- | ||
!Cockpit crew | |||
| colspan=" | | colspan="6" |Two | ||
|- | |- | ||
!Capacity | |||
| colspan="2"| 416 (23F @ 61" + 80J @ 39" + 313Y @ 32") | | colspan="2" |416 (23F @ 61" + 80J @ 39" + 313Y @ 32") | ||
| 274, | |274,100 lb / 124,330 kg | ||
| 273, | |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 | |30 LD1/LD3||28 LD1/LD3 | ||
| colspan="2"| + 2 LD1 + 30 x 96 by 125-in pallet on Main deck | | colspan="2" | + 2 LD1 + 30 x 96 by 125-in pallet on Main deck | ||
| | |||
| | |||
|- | |- | ||
!Exit limit | |||
| colspan="2" | 550/660 | | colspan="2" |550/660 | ||
| colspan="2" | | | colspan="2" | | ||
|605 | |||
|8 | |||
|- | |- | ||
!Overall length | |||
| colspan="4" | | | colspan="4" |231 ft 10 in (70.66 m) | ||
| colspan="2" |250 ft 2 in / 76.3 m | |||
|- | |- | ||
!Wingspan | |||
| colspan="4" | | | colspan="4" |211 ft 5 in (64.44 m) | ||
| colspan="2" |224 ft 7 in / 68.4 m | |||
|- | |- | ||
!Wing area | |||
| colspan="4" | | | colspan="4" |5,650 sq ft (525 m<sup>2</sup>) | ||
| colspan="2" |554 m<sup>2</sup> (5,960 sq ft) | |||
|- | |- | ||
!Aspect ratio | |||
| colspan="4" | | | colspan="4" |7.91 | ||
| colspan="2" | - | |||
|- | |- | ||
!Overall height | |||
| colspan="4" | | | colspan="4" |63 ft 8 in (19.4 m) | ||
| colspan="2" |63 ft 6 in / 19.4 m | |||
|- | |- | ||
!Max. takeoff weight | |||
| 875, | |875,000 lb / 396,890 kg | ||
| 910, | |910,000 lb / 412,775 kg | ||
| 875, | |875,000 lb / 396,890 kg | ||
| 910, | |910,000 lb / 412,775 kg | ||
| colspan="2" |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, | |57,285 US gal (216,840 L) | ||
| 63,705 US gal (241, | |63,705 US gal (241,140 L) | ||
| colspan="2" |53,985 US gal / 204,350L | | colspan="2" |53,985 US gal / 204,350L | ||
|63,034 US gal / 238,610L | |||
|59,734 US gal / 226,118L | |||
|- | |- | ||
!Cruise | |||
| colspan="2" | | | colspan="2" |Mach 0.855 (504 kn; 933 km/h) | ||
| colspan="2" | | | colspan="2" |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 | |||
| colspan= | | colspan="4" |Mach 0.92 (542 kn; 1,004 km/h) | ||
| colspan="2" |Mach 0.9 (516 kn; 956 km/h) | |||
|- | |- | ||
!Takeoff field length | |||
| 9, | |9,700 ft / 2,955m | ||
| 10, | |10,700 ft / 3,260m | ||
| 9, | |9,550 ft / 2,910m | ||
| 10, | |10,700 ft / 3,260m | ||
| colspan="2" | - | |||
|- | |- | ||
!Range | |||
| 7,285nmi / 13, | |7,285nmi / 13,490 km | ||
| 7,585nmi / 14, | |7,585nmi / 14,045 km | ||
| 2,825nmi / 5, | |2,825nmi / 5,230 km | ||
| 4,045nmi / 7, | |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 | ||
| colspan="2" |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) | |||
| colspan="2" |66,500 lbf (296 kN) | |||
|- | |||
!ICAO Type | |||
| colspan="4" |B744 | |||
| colspan="2" |B748 | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|+Boeing 757 Characteristics | |||
|- | |||
!Variant | |||
!757-200 | |||
!757-200F | |||
!757-300 | |||
|- | |||
!Cockpit crew | |||
| colspan="3" |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 | |||
| colspan="3" |148 in / 3.76 m fuselage, 139.3 in / 3.54 m cabin | |||
|- | |||
!Length | |||
| colspan="2" |155 ft 3 in / 47.3 m | |||
|178 ft 7 in / 54.4 m | |||
|- | |||
!Height | |||
| colspan="3" |44 ft 6 in / 13.6 m | |||
|- | |||
!Wing | |||
| colspan="3" |124 ft 10 in / 38.0 m span, 1,994 sq ft (185.25 m<sup>2</sup>) area, 25° sweep, 7.8 AR | |||
|- | |||
!MTOW | |||
| colspan="2" |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 | |||
| colspan="3" |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 | |||
| colspan="3" |42,000 ft (13,000 m) | |||
|- | |||
!Engines (×2) | |||
| colspan="3" |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 | |||
| colspan="2" |B752 | |||
|B753 | |||
|} | |||
{| class="wikitable" style="text-align: center; width: 90%" | |||
|+ 767 Airplane Characteristics | |||
|- | |||
! style="width: 10%;" |Variant | |||
! style="width: 15%;" |767-200 | |||
! style="width: 15%;" |767-200ER | |||
! style="width: 15%;" |767-300 | |||
! style="width: 15%;" |767-300ER | |||
! style="width: 15%;" |767-300F | |||
! style="width: 15%;" |767-400ER | |||
|- | |||
!Cockpit crew | |||
| colspan="6" |Two | |||
|- | |||
!3-class | |||
| colspan="2" |174 (15F, 40J, 119Y) | |||
| colspan="2" |210 (18F, 42J, 150Y) | |||
| rowspan="5" |15,469 ft³ / 438m³ | |||
58-ton / 52.7 tonnes | |||
24 88×108in pallets | |||
|243 (16F, 36J, 189Y) | |||
|- | |||
!2-class | |||
| colspan="2" |214 (18J, 196 Y) | |||
| colspan="2" |261 (24J, 237Y) | |||
|296 (24J, 272Y) | |||
|- | |||
!1-class | |||
| colspan="2" |245Y | |||
| colspan="2" |290Y | |||
|409Y | |||
|- | |||
!Exit limit | |||
| colspan="2" |290 | |||
| colspan="2" |351 | |||
|375 | |||
|- | |||
!Cargo | |||
| colspan="2" |3,070 ft³ / 86.9m³ | |||
| colspan="2" |4,030 ft³ / 114.1m³ | |||
|4,905 ft³ / 138.9m³ | |||
|- | |||
!ULDs | |||
| colspan="2" |22 LD2s | |||
| colspan="3" |30 LD2s | |||
|38 LD2s | |||
|- | |||
!Length | |||
| colspan="2" |159 ft 2in / 48.51m | |||
| colspan="3" |180 ft 3in / 54.94m | |||
|201 ft 4in / 61.37m | |||
|- | |||
!Wingspan | |||
| colspan="5" |156 ft 1in / 47.57m | |||
|170 ft 4in / 51.92m | |||
|- | |||
!Wing | |||
| colspan="5" |3,050 ft² / 283.3m², 31.5° sweepback | |||
|3,130 ft² / 290.7m² | |||
|- | |||
!Fuselage | |||
| colspan="6" |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 | |||
| colspan="2" |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 | |||
|- | |||
! rowspan="2" |Fuel capacity | |||
|16,700USgal / 63,217L | |||
|24,140Usgal / 91,380L | |||
|16,700USgal / 63,216L | |||
| colspan="3" |24,140USgal / 91,380L | |||
|- | |||
|111,890 lb / 50,753 kg | |||
|161,738 lb / 73,363 kg | |||
|111,890 lb / 50,753 kg | |||
| colspan="3" |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 | |||
| colspan="6" |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) | |||
| colspan="2" |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 | |||
| colspan="2" |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) | |||
| colspan="2" |56,750–61,500 lbf (252–274 kN) | |||
|60,600 lbf (270 kN) | |||
|- | |||
!ICAO Type | |||
| colspan="2" |B762 | |||
| colspan="3" |B763 | |||
|B764 | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|+ Boeing 777 specifications | |||
|- | |||
!Variant | |||
!777-200 | |||
!777-200ER | |||
!777-200LR | |||
!777F | |||
!777-300 | |||
!777-300ER | |||
|- | |||
!Cockpit crew | |||
| colspan="6" |Two | |||
|- | |||
!3-class | |||
|305 (24F/54J/227Y) | |||
| colspan="2" |301 (16F/58J/227Y) | |||
| | |||
|368 (30F/84J/254Y) | |||
|365 (22F/70J/273Y) | |||
|- | |||
!2-class/capacity | |||
| colspan="2" |313 | |||
|317 | |||
|224,900 lb / 102,010 kg | |||
| colspan="2" |396 | |||
|- | |||
!Exit limit | |||
| colspan="3" |440 | |||
|11 | |||
| colspan="2" |550 | |||
|- | |||
!Length | |||
| colspan="4" |209 ft 1 in / 63.73 m | |||
| colspan="2" |242 ft 4 in / 73.86 m | |||
|- | |||
!Wingspan | |||
| colspan="2" |199 ft 11 in / 60.93 m | |||
| colspan="2" |212 ft 7 in / 64.80 m | |||
|199 ft 11 in / 60.93 m | |||
|212 ft 7 in / 64.80 m | |||
|- | |||
!Wing sweep | |||
| colspan="6" |31.6° | |||
|- | |||
!Wing area | |||
| colspan="2" |4,605 sq ft (427.8 m<sup>2</sup>) | |||
| colspan="2" |4,702 sq ft (436.8 m<sup>2</sup>) | |||
|4,605 sq ft (427.8 m<sup>2</sup>) | |||
|4,702 sq ft (436.8 m<sup>2</sup>) | |||
|- | |||
!Aspect ratio | |||
| colspan="2" |8.68 | |||
| colspan="2" |9.04 | |||
|8.68 | |||
|9.04 | |||
|- | |||
!Tail height | |||
| colspan="2" |60 ft 9 in / 18.5 m | |||
| colspan="2" |61 ft 1 in / 18.6 m | |||
| colspan="2" |60 ft 8 in / 18.5 m | |||
|- | |||
!Cabin width | |||
| colspan="6" |231 in / 5.86 m | |||
|- | |||
!Seat width | |||
| colspan="6" |18.5 in / 47 cm at 9 abreast, 17 in / 43 cm at 10 abreast | |||
|- | |||
!Fuselage width | |||
| colspan="6" |20 ft 4 in / 6.20 m | |||
|- | |||
!Maximum cargo capacity | |||
| colspan="3" |5,330 ft³ / 150.9 m³ | |||
|23,051 ft³ / 652.7 m³ | |||
| colspan="2" |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 | |||
| colspan="2" |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 | |||
| colspan="6" |43,100 ft (13,100 m) | |||
|- | |||
! scope="row" |Cruise speed | |||
| colspan="6" |Mach 0.84 (892 km/h; 554 mph) | |||
|- | |||
!Max. speed | |||
| colspan="6" |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 | |||
|- | |||
! scope="row" |Turbofan (×2) | |||
|PW 4077 | |||
RR 877 | |||
GE90-77B | |||
|PW 4090 | |||
RR 895 | |||
GE90-94B | |||
| colspan="2" |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) | |||
| colspan="2" |115,300 lbf (513 kN) | |||
|98,000 lbf (440 kN) | |||
|115,300 lbf (513 kN) | |||
|- | |||
!ICAO Type | |||
| colspan="2" |B772 | |||
| colspan="2" |B77L | |||
|B773 | |||
|B77W | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|+Boeing 787 Dreamliner characteristics | |||
!Variant | |||
!787-8 | |||
!787-9 | |||
!787-10 | |||
|- | |||
!Cockpit crew | |||
| colspan="3" |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 | |||
| colspan="3" |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 m<sup>2</sup>) area | |||
|- | |||
!Wing sweep | |||
| colspan="3" |32.2° | |||
|- | |||
!Height | |||
|55 ft 6 in (16.92 m) | |||
| colspan="2" |55 ft 10 in (17.02 m) | |||
|- | |||
!Fuselage | |||
| colspan="3" |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 | |||
| colspan="2" |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 | |||
| colspan="2" |33,384 US gal / 126,372 L | |||
223,673 lb / 101,456 kg | |||
|- | |||
!Speed | |||
| colspan="3" |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 | |||
| colspan="3" |43,000 ft (13,100 m) | |||
|- | |||
!Engines (×2) | |||
| colspan="3" |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 | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|+Airbus A320 family characteristics | |||
|- | |||
!Subtype | |||
!A318 | |||
!A319 | |||
!A320 | |||
!A321 | |||
|- | |||
!Cockpit crew | |||
| colspan="4" style="text-align:center;" |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 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 | |||
|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 | |||
| colspan="4" |7.59 m (24 ft 11 in) | |||
|- | |||
!Wingspan | |||
|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 | |||
|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) | |||
|- | |||
!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) | |||
|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 | |||
| colspan="4" |39,100–41,000 ft (11,900–12,500 m) | |||
|- | |||
!Engines (×2) | |||
| colspan="4" |CFM International CFM56-5B, 68.3 in (1.73 m) fan | |||
|- | |||
! | |||
|PW6000A, 56.5 in (1.44 m) fan | |||
| colspan="3" |IAE V2500A5, 63.5 in (1.61 m) fan | |||
|- | |||
!Thrust (×2) | |||
|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" | |||
|+ Airbus A320neo family characteristics | |||
|- | |||
!Variant | |||
!A319neo | |||
!A320neo | |||
!A321neo | |||
|- | |||
!Cockpit crew | |||
| colspan="3" |Two | |||
|- | |||
!2-class seats | |||
|140 | |||
|165 | |||
|206: 16<abbr>J</abbr> @36 in + 190<abbr>Y</abbr> @30 in | |||
|- | |||
!1-class maximum | |||
|160 | |||
|195 @ 27 in | |||
|240 @ 28 in | |||
|- | |||
!Seat width | |||
| colspan="3" |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 | |||
| colspan="3" |35.80 m (117 ft 5 in) | |||
|- | |||
!Height | |||
| colspan="3" |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 | |||
| colspan="2" |26,730 l (7,060 USg) | |||
|32,940 l (8,700 USg) | |||
|- | |||
!Engines (×2) | |||
| colspan="3" |CFM International LEAP-1A or Pratt & Whitney PW1100G | |||
|- | |||
!Fan diameter | |||
| colspan="3" |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 | |||
| colspan="3" |Cruise: Mach 0.78 (450 kn; 833 km/h), Max.: Mach 0.82 (473 kn; 876 km/h) | |||
|- | |||
!Ceiling | |||
| colspan="3" |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 | |||
|} | |||
{| class="wikitable" style="text-align: center" | |||
|+ Airbus A330 characteristics | |||
!Variant | |||
!A330-200 | |||
!A330-200F | |||
! A330-300 | |||
|- | |||
!Cockpit crew | |||
| 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="3" |Wing: 60.3 m (197.83 ft), Main gear: 12.61 m (41.37 ft) | |||
|- | |||
!Wing | |||
| 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" |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 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" |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" | |||
|- | |||
!Variant | |||
!A340-300 | |||
!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 | |||
|63.45 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" |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" | |||
|+ A350 and A380 characteristics | |||
!Variant | |||
!A350-900 | |||
!A350-1000 | |||
!A380-800 | |||
|- | |||
!Cockpit crew | |||
| colspan="3" |Two | |||
|- | |||
!Seating | |||
|325/315 (48B+267Y) | |||
ULR: 173=80J+93Y | |||
|366/369 (54B+315Y) | |||
387 (2-class) | |||
|544 (4-class) | |||
|- | |||
!Exit limit | |||
| colspan="2" |440 | |||
|868 | |||
|- | |||
!Overall length | |||
|66.8 m / 219.5 ft | |||
|73.78 m / 242.7 ft | |||
|72.72 m / 238 ft 7 in | |||
|- | |||
!Wingspan | |||
| 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 / 55 ft 11 in | |||
|17.08 m / 56 ft 0 in | |||
|24.09 m / 79 ft 0 in | |||
|- | |||
!Fuselage | |||
| 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 / 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 | |||
| 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 | |||
|15,600 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" |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 | ||
|} | |} |
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 |