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常见航空器规格和性能参数
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{| class="wikitable" style="text-align: center" |+ Boeing 737 Next Generation Characteristics ! Variant ! 737-600 ! 737-700 ! 737-800 ! 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="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" |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 | 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" |18 in / 46 cm | colspan="2" |19 in / 48 cm |- ! ICAO Type |B736 |B737 |B738 |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 |B38M |B39M |B3JM |} {| class="wikitable" style="text-align: center; font-size:95%;" |+Boeing 747 Characteristics |- !Variant !747-400 !747-400ER !747-400F !747-400ERF !747-8 !747-8F |- !Cockpit crew | colspan="6" |Two |- !Capacity | colspan="2" |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 | colspan="2" | + 2 LD1 + 30 x 96 by 125-in pallet on Main deck | | |- !Exit limit | colspan="2" |550/660 | colspan="2" | |605 |8 |- !Overall length | colspan="4" |231 ft 10 in (70.66 m) | colspan="2" |250 ft 2 in / 76.3 m |- !Wingspan | colspan="4" |211 ft 5 in (64.44 m) | colspan="2" |224 ft 7 in / 68.4 m |- !Wing area | 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" |7.91 | colspan="2" | - |- !Overall height | colspan="4" |63 ft 8 in (19.4 m) | colspan="2" |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 | 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 (216,840 L) |63,705 US gal (241,140 L) | colspan="2" |53,985 US gal / 204,350L |63,034 US gal / 238,610L |59,734 US gal / 226,118L |- !Cruise | colspan="2" |Mach 0.855 (504 kn; 933 km/h) | 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="4" |Mach 0.92 (542 kn; 1,004 km/h) | colspan="2" |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 | colspan="2" | - |- !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 | 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; color:black;" |+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; font-size:96%;" |+ 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 |}
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