| 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 (56cm); Economy: 17in (43cm) |
|||
Length |
102ft 6in (31.24m) |
110ft 4in (33.63m) |
129ft 6in (39.47m) |
138ft 2in (42.11m) |
Height |
41ft 3in (12.57m) |
41ft 2in (12.55m) |
||
Wing |
Span: 112ft 7in (34.32m), with winglets: 117ft 5in (35.79m); Area: 124.60m2 (1,341.2ft2); Sweepback: 25°; AR: 9.44 |
|||
Fuselage |
Width: 12ft 4in (3.76m); Cabin width: 11ft 7in (3.54m); Cabin height: 86.6in (2.20m) |
|||
Operating empty weight |
80,200lb (36,378kg) |
83,000lb (37,648kg) |
91,300lb (41,413kg) |
98,495lb (44,677kg) |
Maximum landing weight |
121,500lb (55,111kg) |
129,200lb (58,604kg) |
146,300lb (66,361kg) |
157,300lb (71,350kg) |
Maximum takeoff weight |
144,500lb (65,544kg) |
154,500lb (70,080kg) |
174,200lb (79,016kg) |
187,700lb (85,139kg) |
Fuel capacity |
6,875 US gal (26,022L) |
7,837 US gal (29,666L) |
||
Lower deck cargo |
720ft3 (20.4m3) |
966ft3 (27.4m3) |
1,555ft3 (44.1m3) |
1,826ft3 (51.7m3) |
Takeoff run |
6,161ft (1,878m) |
6,699ft (2,042m) |
7,598ft (2,316m) |
9,800ft (3,000m) |
Flight envelope |
41,000ft (12,497m) Ceiling, Mach 0.82 (470kn; 871km/h) MMo |
|||
Cruise |
Mach 0.785 (453kn; 838km/h) |
Mach 0.781 (450kn; 834km/h) |
Mach 0.789 (455kn; 842km/h) |
Mach 0.79 (455kn; 844km/h) |
Range |
3,235nmi (5,991km) |
3,010nmi (5,570km) |
2,935nmi (5,436km) |
2,950nmi (5,460km) |
Engines (× 2) |
CFM56-7B18/20/22 |
CFM56-7B20/22/24/26/27 |
CFM56-7B24/26/27 |
|
Thrust (× 2) |
20,000–22,000lbf (89–98kN) |
20,000–26,000lbf (89–116kN) |
24,000–27,000lbf (110–120kN) |
24,000–27,000lbf (110–120kN) |
Cruise max. thrust |
5,960lbf (26.5kN) (climb) |
|||
Engine dimensions |
Fan tip diameter: 61in (155cm), length: 103.50in (263cm) |
|||
Engine ground clearance |
18in (46cm) |
19in (48cm) |
||
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 |
28–29in (71–74cm) in high density, 31–32in (79–81cm) in economy, 36in (91cm) in business |
|||
Cargo capacity |
1,146 cu.ft (32.45m3) |
1,543 cu.ft (43.69m3) |
1,814 cu.ft (51.37m3) |
|
Length |
116ft 8in (35.56m) |
129ft 8in (39.52m) |
138ft 4in (42.16m) |
143ft 8in (43.8m) |
Wingspan |
117ft 10in (35.92m) |
|||
Wing Area |
1,370ft2 (127m2) |
|||
Overall height |
40ft 4in (12.3m) |
|||
Maximum takeoff weight |
177,000lb (80,286kg) |
181,200lb (82,191kg) |
194,700lb (88,314kg) |
|
Maximum landing weight |
145,600lb (66,043kg) |
152,800lb (69,309kg) |
163,900lb (74,344kg) |
|
Maximum zero fuel weight |
138,700lb (62,913kg) |
145,400lb (65,952kg) |
156,500lb (70,987kg) |
|
Operating empty weight |
99,360lb (45,070kg) |
|||
Fuel capacity |
6,820 USgal (25,817L), excluding ACT |
|||
Engine (× 2) |
CFM International LEAP-1B, 69in (175cm) Fan diameter |
|||
Thrust (× 2) |
26,786–29,317lbf (119–130kN) |
|||
Cruising speed |
Mach 0.79 (453kn; 839km/h) |
|||
Range (2-class) |
3,850nmi (7,130km) |
3,550nmi (6,570km) MAX 200: 2,700nmi (5,000km) |
3,550nmi (6,570km) |
3,300nmi (6,110km) |
Ceiling |
41,000ft (12,000m) |
|||
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") |
274,100lb (124,330kg) |
273,400lb (124,010kg) |
410in 3-class |
303,700lb (137,700kg) |
|
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 |
231ft 10in (70.66m) |
250ft 2in (76.3m) |
||||
Wingspan |
211ft 5in (64.44m) |
224ft 7in (68.4m) |
||||
Wing area |
5,650ft2 (525m2) |
554m2 (5,960ft2) |
||||
Aspect ratio |
7.91 |
- |
||||
Overall height |
63ft 8in (19.4m) |
63ft 6in (19.4m) |
||||
Max. takeoff weight |
875,000lb (396,890kg) |
910,000lb (412,775kg) |
875,000lb (396,890kg) |
910,000lb (412,775kg) |
987,000lb (447,700kg) |
|
Operating empty weight |
404,600lb (183,520kg) |
412,300lb (187,010kg) |
360,900lb (163,700kg) |
361,600lb (164,020kg) |
485,300lb (220,128kg) |
434,600lb (197,131kg) |
Fuel capacity |
57,285 US gal (216,840L) |
63,705 US gal (241,140L) |
53,985 US gal (204,350L) |
63,034 US gal (238,610L) |
59,734 US gal (226,118L) |
|
Cruise |
Mach 0.855 (504kn; 933km/h) |
Mach 0.845 (498kn; 922km/h) |
Mach 0.86 (493kn; 914km/h) |
Mach 0.85 (488kn; 903km/h) |
||
Airspeed limit |
Mach 0.92 (542kn; 1,004km/h) |
Mach 0.9 (516kn; 956km/h) |
||||
Takeoff field length |
9,700ft (2,955m) |
10,700ft (3,260m) |
9,550ft (2,910m) |
10,700ft (3,260m) |
- |
|
Range |
7,285nmi (13,490km) |
7,585nmi (14,045km) |
2,825nmi (5,230km) |
4,045nmi (7,585km) |
8,000nmi (15,000km) |
4,120nmi (7,630km) |
Engines (x 4) |
PW4000/GE CF6/RR RB211 |
PW4000/GE CF6 |
PW4000/GE CF6/RR RB211 |
PW4000/GE CF6 |
GEnx-2B67 |
|
Thrust (x 4) |
56,500–63,300lbf (251–282kN) |
62,100–63,300lbf (276–282kN) |
56,400–63,300lbf (251–282kN) |
62,100–63,300lbf (276–282kN) |
66,500lbf (296kN) |
|
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 |
1,670ft3 (43.3m3) |
6,600ft3 (187m3) |
2,370ft3 (61.7m3) |
Width |
148in (3.76m) fuselage, 139.3in (3.54m) cabin |
||
Length |
155ft 3in (47.3m) |
178ft 7in (54.4m) |
|
Height |
44ft 6in (13.6m) |
||
Wing |
124ft 10in (38.0m) span, 1,994ft2 (185.25m2) area, 25° sweep, 7.8 AR |
||
MTOW |
255,000lb (115,660kg) |
273,000lb (123,830kg) |
|
Max. Payload |
57,160lb (25,920kg) |
84,420lb (38,290kg) |
68,140lb (30,910kg) |
OEW |
128,840lb (58,440kg) |
115,580lb (52,430kg) |
141,860lb (64,340kg) |
Fuel capacity |
11,489 US gal (43,490L) |
11,276 US gal (42,680L) |
11,466 US gal (43,400L) |
Speed |
Cruise Mach 0.8 (461kn; 854km/h), Max. Mach 0.86 (496kn; 918km/h) |
||
Range |
3,915nmi (7,250km) |
2,935nmi (5,435km) |
3,400nmi (6,295km) |
Takeoff |
6,800ft (2,070m) |
6,900ft (2,103m) |
8,550ft (2,605m) |
Ceiling |
42,000ft (13,000m) |
||
Engines (×2) |
40,200–43,500lbf (179–193kN) Rolls-Royce RB211-535E4(B) 36,600–42,600lbf (163–189kN) 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) |
15,469ft3 (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 |
3,070ft3 (86.9m3) |
4,030ft3 (114.1m3) |
4,905ft3 (138.9m3) |
|||
ULDs |
22 LD2s |
30 LD2s |
38 LD2s |
|||
Length |
159ft 2in (48.51m) |
180ft 3in (54.94m) |
201ft 4in (61.37m) |
|||
Wingspan |
156ft 1in (47.57m) |
170ft 4in (51.92m) |
||||
Wing |
3,050ft² (283.3m²), 31.5° sweepback |
3,130ft² (290.7m²) |
||||
Fuselage |
17ft 9in (5.41m) height, 16ft 6in (5.03m) width, 186in (4.72m) Cabin width |
|||||
MTOW |
315,000lb (142,882kg) |
395,000lb (179,169kg) |
350,000lb (158,758kg) |
412,000lb (186,880kg) |
450,000lb (204,116kg) |
|
Max. payload |
73,350lb (33,271kg) |
78,390lb (35,557kg) |
88,250lb (40,030kg) |
96,560lb (43,799kg) |
119,000lb (53,977kg) |
101,000lb (45,813kg) |
OEW |
176,650lb (80,127kg) |
181,610lb (82,377kg) |
189,750lb (86,069kg) |
198,440lb (90,011kg) |
190,000lb (86,183kg) |
229,000lb (103,872kg) |
Fuel capacity |
16,700USgal (63,217L) |
24,140Usgal (91,380L) |
16,700USgal (63,216L) |
24,140USgal (91,380L) |
||
111,890lb (50,753kg) |
161,738lb (73,363kg) |
111,890lb (50,753kg) |
161,740lb (73,364kg) |
|||
Range |
3,900nmi (7,200km) |
6,590nmi (12,200km) |
3,900nmi (7,200km) |
5,980nmi (11,070km) |
3,225nmi (6,025km) |
5,625nmi (10,415km) |
Cruise |
Long range: 459kn (850km/h), Maximum: 486kn (900km/h) at 39,000ft (12,000m), Ceiling: 43,100ft (13,100m) |
|||||
Takeoff |
6,300ft (1,900m) |
2,480m (8,150ft) |
9,200ft (2,800m) |
2,650m (8,700ft) |
3,290m (10,800ft) |
|
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) |
48,000–52,500lbf (214–234kN) |
48,000–60,600lbf (214–270kN) |
48,000–60,600lbf (214–270kN) |
56,750–61,500lbf (252–274kN) |
60,600lbf (270kN) |
|
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 |
224,900lb (102,010kg) |
396 |
||
Exit limit |
440 |
11 |
550 |
|||
Length |
209ft 1in (63.73m) |
242ft 4in (73.86m) |
||||
Wingspan |
199ft 11in (60.93m) |
212ft 7in (64.80m) |
199ft 11in (60.93m) |
212ft 7in (64.80m) |
||
Wing sweep |
31.6° |
|||||
Wing area |
4,605ft2 (427.8m2) |
4,702ft2 (436.8m2) |
4,605ft2 (427.8m2) |
4,702ft2 (436.8m2) |
||
Aspect ratio |
8.68 |
9.04 |
8.68 |
9.04 |
||
Tail height |
60ft 9in (18.5m) |
61ft 1in (18.6m) |
60ft 8in (18.5m) |
|||
Cabin width |
231in (5.86m) |
|||||
Seat width |
18.5in (47cm) at 9 abreast, 17in (43cm) at 10 abreast |
|||||
Fuselage width |
20ft 4in (6.20m) |
|||||
Maximum cargo capacity |
5,330ft3 (150.9m3) |
23,051ft3 (652.7m3) |
7,120ft3 (201.6m3) |
|||
Maximum takeoff weight (MTOW) |
545,000lb (247,200kg) |
656,000lb (297,550kg) |
766,000lb (347,452kg) |
766,800lb (347,815kg) |
660,000lb (299,370kg) |
775,000lb (351,533kg) |
Max. landing weight |
445,000lb (201,840kg) |
470,000lb (213,180kg) |
492,000lb (223,168kg) |
575,000lb (260,816kg) |
524,000lb (237,680kg) |
554,000lb (251,290kg) |
Operating empty weight |
299,550lb (135,850kg) |
304,500lb (138,100kg) |
320,000lb (145,150kg) |
318,300lb (144,379kg) |
353,800lb (160,530kg) |
370,000lb (167,829kg) |
Fuel capacity |
31,000 US gal (117,340L) 207,700lb (94,240kg) |
45,220 US gal (171,171L) 302,270lb (137,460kg) |
47,890 US gal (181,283L) 320,863lb (145,538kg) |
45,220 US gal (171,171L) 302,270lb (137,460kg) |
47,890 US gal (181,283L) 320,863lb (145,538kg) |
|
Service ceiling |
43,100ft (13,100m) |
|||||
Cruise speed |
Mach 0.84 (892km/h; 554 mph) |
|||||
Max. speed |
Mach 0.89 (945km/h; 587 mph) |
|||||
Range |
5,240nmi (9,700km) |
7,065nmi (13,080km) |
8,555nmi (15,843km) |
4,970nmi (9,200km) |
6,030nmi (11,165km) |
7,370nmi (13,649km) |
Takeoff distance |
8,000ft (2,440m) |
11,100ft (3,380m) |
9,200ft (2,800m) |
9,300ft (2,830m) |
10,600ft (3,230m) |
10,000ft (3,050m) |
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) |
77,200lbf (343kN) |
93,700lbf (417kN) |
115,300lbf (513kN) |
98,000lbf (440kN) |
115,300lbf (513kN) |
|
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 |
186ft 1in (56.72m) |
206ft 1in (62.81m) |
224ft (68.28m) |
Wing |
197ft 3in (60.12m) span, 246.9in (6.27m) mean chord, 9.59 aspect ratio, 4,058ft2 (377m2) area |
||
Wing sweep |
32.2° |
||
Height |
55ft 6in (16.92m) |
55ft 10in (17.02m) |
|
Fuselage |
Cabin width: 18ft 0in (5.49m) External width: 18ft 11in (5.77m), height: 19ft 6in (5.94m) |
||
Cargo capacity |
4,826ft3 (136.7m3) 28 LD3 or 9 (88×125) pallets |
6,090ft3 (172.5m3) 36 LD3 or 11 (96×125) pallets |
6,722ft3 (191.4m3) 40 LD3 or 13 (96×125) pallets |
MTOW |
502,500lb (227,930kg) |
560,000lb (254,011kg) |
|
MLW |
380,000lb (172,365kg) |
425,000lb (192,777kg) |
445,000lb (201,849kg) |
Maximum ZFW |
355,000lb (161,025kg) |
400,000lb (181,437kg) |
425,000lb (192,777kg) |
OEW |
264,500lb (119,950kg) |
284,000lb (128,850kg) |
298,700lb (135,500kg) |
Fuel capacity |
33,340 US gal (126,206L) 223,378lb (101,323kg) |
33,384 US gal (126,372L) 223,673lb (101,456kg) |
|
Speed |
Max: Mach 0.90 (516kn; 956km/h); Cruise: Mach 0.85 (488kn; 903km/h) |
||
Range |
7,355nmi (13,620km) |
7,635nmi (14,140km) |
6,430nmi (11,910km) |
Takeoff |
8,500ft (2,600m) |
9,300ft (2,800m) |
9,100ft (2,800m) |
Ceiling |
43,000ft (13,100m) |
||
Engines (×2) |
General Electric GEnx-1B or Rolls-Royce Trent 1000 |
||
Thrust (×2) |
64,000lbf (280kN) |
71,000lbf (320kN) |
76,000lbf (340kN) |
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 29–30in (74–76cm) pitch |
156 at 28–30in (71–76cm) pitch |
186 at 29in (74cm) pitch |
236 at 28in (71cm) pitch |
1-class, typical |
117 at 32in (81cm) pitch |
134 at 32in (81cm) pitch |
164 at 32in (81cm) pitch |
199 at 32in (81cm) pitch |
2-class, typical |
107 (8F@38in, 99Y@32in) |
124 (8F@38in, 116Y@32in) |
150 (12F@36in, 138Y@32in) |
185 (16F@36in, 169Y@32in) |
Cargo volume |
21.20m3 (749ft3) |
27.70m3 (978ft3) |
37.40m3 (1,321ft3) |
51.70m3 (1,826ft3) |
Unit load devices |
4× LD3-45 |
7× LD3-45 |
10× LD3-45 |
|
Length |
31.44m (103ft 2in) |
33.84m (111ft 0in) |
37.57m (123ft 3in) |
44.51m (146ft 0in) |
Wheelbase |
10.25m (33ft 8in) |
11.04m (36ft 3in) |
12.64m (41ft 6in) |
16.91m (55ft 6in) |
Track |
7.59m (24ft 11in) |
|||
Wingspan |
34.10m (111ft 11in) |
35.8m (117ft 5in) |
||
Wing area |
124m2 (1,330ft2), 10.3 aspect ratio |
128m2 (1,380ft2), 10 AR |
||
Wing sweepback |
25 degrees |
|||
Tail height |
12.56m (41ft 2in) |
11.76m (38ft 7in) |
||
Fuselage |
4.14m (13ft 7in) height, 3.95m (13ft 0in) width, 3.70m (12ft 2in) cabin width |
|||
MTOW |
68t (150,000lb) |
75.5t (166,000lb) |
78t (172,000lb) |
93.5t (206,000lb) |
Max. payload |
15t (33,000lb) |
17.7t (39,000lb) |
19.9t (44,000lb) |
25.3t (56,000lb) |
Fuel capacity |
24,210L (6,400 US gal) |
24,210–30,190L (6,400–7,980 US gal) |
24,210–27,200L (6,400–7,190 US gal) |
24,050–30,030L (6,350–7,930 US gal) |
OEW |
39.5t (87,100lb) |
40.8t (89,900lb) |
42.6t (93,900lb) |
48.5t (107,000lb) |
Speed |
Cruise: Mach 0.78 (447kn; 829km/h), MMO: Mach 0.82 (470kn; 871km/h) |
|||
Range, typical payload |
3,100nmi (5,750km) |
3,750nmi (6,950km) |
3,300nmi (6,100km) |
3,200nmi (5,950km) |
ACJ range |
4,200nmi (7,800km) |
6,000nmi (11,100km) |
4,300nmi (7,800km) |
- |
Takeoff run (MTOW, SL, ISA) |
1,780m (5,840ft) |
1,850m (6,070ft) |
2,100m (6,900ft) |
- |
Landing (MLW, SL, ISA) |
1,230m (4,040ft) |
1,360m (4,460ft) |
1,500m (4,900ft) |
- |
Service ceiling |
39,100–41,000ft (11,900–12,500m) |
|||
Engines (×2) |
CFM International CFM56-5B, 68.3in (1.73m) fan |
|||
Fan diameter |
PW6000A, 56.5in (1.44m) fan |
IAE V2500A5, 63.5in (1.61m) fan |
||
Thrust (×2) |
96–106kN (22,000–24,000lbf) |
98–120kN (22,000–27,000lbf) |
133–147kN (30,000–33,000lbf) |
|
| Variant | A319neo | A320neo | A321neo |
|---|---|---|---|
Cockpit crew |
Two |
||
2-class seats |
140 |
165 |
206: 16J@36in + 190Y@30in |
1-class maximum |
160 |
195@27in |
240@28in |
Seat width |
Economy at 6 abreast: 18in (46cm), 3.7m (12ft 1in) cabin width |
||
Cargo capacity |
27m3 (976ft3) |
37m3 (1,322ft3) |
51m3 (1,828ft3) |
Length |
33.84m (111ft) |
37.57m (123ft 3in) |
44.51m (146ft) |
Wingspan |
35.80m (117ft 5in) |
||
Height |
11.76m (38ft 7in) |
||
Max. takeoff weight |
75.5t (166,400lb) |
79t (174,200lb) |
97t (213,800lb) |
Max. payload |
17.7t (39,000lb) |
20t (44,100lb) |
25.5t (56,200lb) |
Operating empty |
42.6t (93,900lb) |
44.3t (97,700lb) |
50.1t (110,500lb) |
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: 81in (206cm), LEAP-1A: 78in (198cm) |
||
Max. Thrust |
107kN (24,100lbf) |
120.6kN (27,120lbf) |
147.3kN (33,110lbf) |
Speed |
Cruise: Mach 0.78 (450kn; 833km/h), Max.: Mach 0.82 (473kn; 876km/h) |
||
Ceiling |
39,100–39,800ft (11,900–12,100m) |
||
Typical range |
6,950km (3,750nmi) |
6,500km (3,500nmi) |
7,400km (4,000nmi) |
Takeoff |
- |
- |
1,988m (6,522ft) |
ICAO Type |
A19N |
A20N |
A21N |
| Variant | A330-200 | A330-200F | A330-300 |
|---|---|---|---|
Cockpit crew |
Two |
||
Capacity |
246 (36J@60in + 210Y@32in) |
70,000kg (154,324lb) |
300 (36J@60in + 264Y@32in) |
Max seating |
406 |
440 |
|
Length |
58.82m (192.98ft) |
63.67m (208.89ft) |
|
Span |
Wing: 60.3m (197.83ft), Main gear: 12.61m (41.37ft) |
||
Wing |
361.6 m² (3,892ft²), 25% chord wingsweep : 30°, 10.06 Aspect ratio |
||
Tail height |
17.39m (57’) |
16.90m (55’5’’) |
16.79m (55’) |
Fuselage |
5.64m (222in) diameter, 5.18m (204in) cabin width |
||
Seat width |
0.46m (18in) in 8 abreast economy, 0.53m (21in) in 6 abreast business |
||
Cargo volume |
132.4m3 (4673ft3) |
469.2m3 (16567ft3) |
158.4m3 (5591ft3) |
Maximum takeoff weight |
242,000kg (533,519lb) |
233,000kg (513,677lb) |
242,000kg (533,519lb) |
Maximum landing weight |
182,000kg (401,241lb) |
187,000kg (412,264lb) |
|
Max zero fuel weight |
170,000kg (374,786lb) |
178,000kg (392,423lb) |
175,000kg (385,809lb) |
Max Payload |
49,400kg (108,900lb) |
68,600kg (151,200lb) |
45,600kg (100,500lb) |
Fuel capacity |
139,090 l (36,744 US gal) - 109,185kg (240,711lb) |
||
Operating empty weight |
120,600kg (265,900lb) |
109,400kg (241,200lb) |
129,400kg (285,300lb) |
Cruise |
Mach 0.82 (470kn; 871km/h) (Mach 0.86 (493kn; 914km/h) MMO), 12,500m (41,100ft) Service ceiling |
||
Final approach speed (MLW) |
136kn (252km/h) |
139kn (257km/h) |
137kn (254km/h) |
Range |
13,450km (7,250nm) (247 pax) |
7,400km (4,000nm) |
11,750km (6,350nm) (277 pax) |
Runway (SL, ISA, MTOW/MLW) |
Takeoff: 2,770m (9,110ft), Landing: 1,730m (5,680ft) |
||
Engines (×2) |
64,530–68,530lbf (287–305kN) General Electric CF6-80E1 (except -200F) 64,500–70,000lbf (287–311kN) Pratt & Whitney PW4000 PW4164/PW4168/PW4170 67,500–71,100lbf (300–316kN) 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 |
63.69m (208.96ft) |
75.36m (247.24ft) |
Wingspan |
60.3m (197.83ft) |
63.45m (208.17ft) |
Wing |
363.1m2 (3,908ft2), 29.7° sweep, 10 AR |
437.3m2 (4,707ft2), 31.1° sweep, 9.2 AR |
Height |
16.99m (55.72ft) |
17.93m (58.84ft) |
Fuselage |
5.287m (208.15in) cabin width, 5.64m (18.5ft) outside width |
|
Cargo volume |
132.4m3 (4,680ft3) |
201.7m3 (7,120ft3) |
MTOW |
276.5t (610,000lb) |
380t (840,000lb) |
Max. PL |
52t (115,000lb) |
66t (146,000lb) |
OEW |
131t (289,000lb) |
174t (384,000lb) |
Max. Fuel |
110.4t (243,395lb) |
155.5t (342,905lb) |
Engines (×4) |
CFM International CFM56-5C |
Trent 556 |
Thrust (×4) |
138.78–151.24kN (31,200–34,000lbf) |
248.12–275.35kN (55,780–61,902lbf) |
Speed |
Mach 0.86 (493kn; 914km/h) max, Mach 0.82 (470kn; 871km/h) cruise |
|
Range, max pax |
7,150nmi (13,240km) |
7,550nmi (13,980km) |
Take off |
3,000m (10,000ft) |
3,400m (11,200ft) |
Ceiling |
12,500m (41,000ft) |
12,527m (41,100ft) |
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 |
66.8m (219.5ft) |
73.78m (242.7ft) |
72.72m (238ft 7in) |
Wingspan |
64.75m (212.43ft) |
79.75m (261ft 8in) |
|
Aspect ratio |
9.49 |
9.03 |
7.53 |
Wing area |
442m2 (4,760ft2) |
464.3m2 (4,998ft2) |
845m2 (9,100ft2) |
Overall height |
17.05m (55ft 11in) |
17.08m (56ft 0in) |
24.09m (79ft 0in) |
Fuselage |
5.96m (19.7ft) width, 6.09m (19.98ft) height |
7.14m (23ft 5in) width, 8.41m (27ft 7in) height |
|
Cabin width |
5.61m (18ft 5in), 9-abreast Seat : 18in (46cm) |
6.50m (21ft 4in) main deck 5.80m (19ft 0in) upper deck |
|
MTOW |
280t (617,295lb) |
316t (696,661lb) |
575t (1,268,000lb) |
Max. payload |
53.3t (118,000lb) |
64.2t (142,000lb) |
84t (185,000lb) |
Fuel capacity |
140,795L (37,194 US gal) 110,523kg (243,662lb) |
158,791L (41,948 US gal) 124,651kg (274,808lb) |
323,545L (85,471 US gal) |
OEW |
142.4t (314,000lb) typical 134.7–145.1t (297,000–320,000lb) |
158.8t (350,000lb) 155t (342,000lb) dry |
276.8t (610,000lb) |
MEW |
115.7t (255,075lb) |
129t (284,000lb) |
- |
Cargo capacity |
36 LD3 or 11 pallets |
44 LD3 or 14 pallets |
- |
Cruise |
Mach 0.85 (488kn; 903km/h) Typical, Mach 0.89 (513kn; 950km/h) Maximum |
Mach 0.85 (903km/h; 488kn) |
|
Range |
15,000km (8,100nmi) |
15,600km (8,400nmi) |
15,200km (8,200nmi) |
Takeoff (MTOW, SL, ISA) |
2,600m (8,500ft) |
- |
3,000m (9,800ft) |
Landing (MLW, SL, ISA) |
2,000m (6,600ft) |
- |
- |
Service ceiling |
43,100ft (13,100m) |
41,450ft (12,630m) |
13,100m (43,000ft) |
Engines (2×) |
Rolls-Royce Trent XWB |
Engine Alliance GP7200/Rolls-Royce Trent 900 |
|
Maximum thrust |
374.5kN (84,200lbf) |
431.5kN (97,000lbf) |
311kN (70,000lbf) |
ICAO Type |
A359 |
A35K |
A388 |