Airbus A340: Difference between revisions
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==Airbus A340-500== | ==Airbus A340-500== | ||
==Airbus A340-600== | ==Airbus A340-600== | ||
A340-600 SPECIFICATIONS | |||
AIRCRAFT DIMENSIONS | |||
metric imperial | |||
Overall length 75.3 m. 247 ft. 1 in. | |||
Height 17.3 m. 56 ft. 9 in. | |||
Fuselage diameter 5.64 m. 18 ft. 6 in. | |||
Maximum cabin width 5.28 m. 17 ft. 4 in. | |||
Cabin length 60.98 m. 200 ft. 1 in. | |||
Wingspan (geometric) 63.45 m. 208 ft. 2 in. | |||
Wing area (reference) 439.4 m2 4,729 ft2 | |||
Wing sweep (25% chord) 31.1 degrees 31.1 degrees | |||
Wheelbase 32.89 m. 107 ft. 11 in. | |||
Wheel track 10.69 m. 35 ft. 1 in. | |||
BASIC OPERATING DATA | |||
metric imperial | |||
Engines RR Trent 500 RR Trent 500 | |||
Engine thrust range 249 (267) kN 56,000 (60,000) | |||
lb. slst | |||
Typical passenger seating 380 380 | |||
Range (w/max. passengers) 14,360 | |||
(14,600) km. 7,750 (7,900) | |||
nm. | |||
Max. operating Mach number (Mmo) 0.86 Mo. 0.86 Mo. | |||
Bulk hold volume - Standard/option 19.7 / 13.76 m3 695 / 486 ft3 | |||
DESIGN WEIGHTS | |||
Metric imperial | |||
Maximum ramp weight 369.2 (381.2) | |||
tonnes 813.9 (840.4) | |||
lbs. x 1000 | |||
Maximum takeoff weight 368 (380) | |||
tonnes 811.3 (837.8) | |||
lbs. x 1000 | |||
Maximum landing weight 259 (265) | |||
tonnes 571 (584.2) lbs. | |||
x 1000 | |||
Maximum zero fuel weight 245 (251) | |||
tonnes 540.1 (553.4) | |||
lbs. x 1000 | |||
Maximum fuel capacity 195,881 | |||
(204,500) Litres | |||
51,746 | |||
(54,023.2) US | |||
gal. | |||
Typical operating weight empty 177.8 (181.9) | |||
tonnes 392.0 (400.9) | |||
lbs. x 1000 | |||
Typical volumetric payload 55.6 tonnes 122.6 lbs. x | |||
1000 | |||
==Specifications== | ==Specifications== | ||
[[Category:Widebody Jetliners]] | [[Category:Widebody Jetliners]] | ||
Revision as of 06:30, 11 September 2009
| Airbus A340 at a Glance | |
|---|---|
| Role | Widebody Jetliner |
| Country of Origin | Fance |
| Manufacturer | Airbus |
| Status | In Production |
| Number Built | 368 |
| Unit Cost | 186,000,000v$-210,000,000v$ |
| File:Airplanes-Airbus A340.jpg | |
Airbus A340-200
Airbus A340-300
A340-300 SPECIFICATIONS AIRCRAFT DIMENSIONS metric imperial Overall length 63.6 m. 208 ft. 10 in. Height 16.85 m. 55 ft. 3 in. Fuselage diameter 5.64 m. 18 ft. 6 in. Maximum cabin width 5.28 m. 17 ft. 4 in. Cabin length 50.35 m. 165 ft. 3 in. Wingspan (geometric) 60.3 m. 197 ft. 10 in. Wing area (reference) 361.6 m2 3,892 ft2 Wing sweep (25% chord) 30 degrees 30 degrees Wheelbase 25.60 m. 84 ft. Wheel track 10.69 m. 35 ft. 1 in. BASIC OPERATING DATA metric imperial Engines four CFM56- 5C4/P four CFM56- 5C4/P Engine thrust range 139-151 kN 31,200-34,000 lb. slst Typical passenger seating 295 295 Range (w/max. passengers) 13,350 (13,700) km. 7,200 (7,400) nm. Max. operating Mach number (Mmo) 0.86 Mo. 0.86 Mo. Bulk hold volume - Standard/option 19.7 / 13.76 m3 695 / 486 ft3 DESIGN WEIGHTS metric imperial Maximum ramp weight 275.9 (277.4) tonnes 608.3 (611.5) lbs. x 1000 Maximum takeoff weight 275 (276.5) tonnes 606.0 (609.6) lbs. x 1000 Maximum landing weight 190 (192) tonnes 418.9 (423.3) lbs. x 1000 Maximum zero fuel weight 178 (181) tonnes 392.4 (399) lbs. x 1000 Maximum fuel capacity 140,640 (147,850) Litres 37,150 (39,060) US gal. Typical operating weight empty 129.3 (130.2) tonnes 285 (287) lbs. x 1000 Typical volumetric payload 43.5 (41) tonnes 95.9 (90.5) lbs. x 1000
Airbus A340-500
Airbus A340-600
A340-600 SPECIFICATIONS AIRCRAFT DIMENSIONS metric imperial Overall length 75.3 m. 247 ft. 1 in. Height 17.3 m. 56 ft. 9 in. Fuselage diameter 5.64 m. 18 ft. 6 in. Maximum cabin width 5.28 m. 17 ft. 4 in. Cabin length 60.98 m. 200 ft. 1 in. Wingspan (geometric) 63.45 m. 208 ft. 2 in. Wing area (reference) 439.4 m2 4,729 ft2 Wing sweep (25% chord) 31.1 degrees 31.1 degrees Wheelbase 32.89 m. 107 ft. 11 in. Wheel track 10.69 m. 35 ft. 1 in. BASIC OPERATING DATA metric imperial Engines RR Trent 500 RR Trent 500 Engine thrust range 249 (267) kN 56,000 (60,000) lb. slst Typical passenger seating 380 380 Range (w/max. passengers) 14,360 (14,600) km. 7,750 (7,900) nm. Max. operating Mach number (Mmo) 0.86 Mo. 0.86 Mo. Bulk hold volume - Standard/option 19.7 / 13.76 m3 695 / 486 ft3 DESIGN WEIGHTS Metric imperial Maximum ramp weight 369.2 (381.2) tonnes 813.9 (840.4) lbs. x 1000 Maximum takeoff weight 368 (380) tonnes 811.3 (837.8) lbs. x 1000 Maximum landing weight 259 (265) tonnes 571 (584.2) lbs. x 1000 Maximum zero fuel weight 245 (251) tonnes 540.1 (553.4) lbs. x 1000 Maximum fuel capacity 195,881 (204,500) Litres 51,746 (54,023.2) US gal. Typical operating weight empty 177.8 (181.9) tonnes 392.0 (400.9) lbs. x 1000 Typical volumetric payload 55.6 tonnes 122.6 lbs. x 1000