Airbus A340: Difference between revisions
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==Airbus A340-500== | ==Airbus A340-500== | ||
==Airbus A340-600== | ==Airbus A340-600== | ||
==Specifications== | ==Specifications== |
Revision as of 23:36, 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
Specifications
Measurement | A340-200 | A340-300 | A340-500/-500HGW | A340-600/-600HGW |
---|---|---|---|---|
Cockpit crew | Two | |||
Seating capacity | 239 (3-class) | 295 (3-class) | 313 (3-class) | 380 (3-class) |
Length | 59.39 m 194 ft 10 in |
63.60 m 208 ft 8 in |
67.90 m 222 ft 9 in |
75.30 m 247 ft 0 in |
Wingspan | 60.30 m 197 ft 10 in |
63.45 m 208 ft 2 in | ||
Wing area | 361.6 m² 3,892 ft² |
439 m² 4,725 ft² | ||
Wing sweepback | 30° | 31.1° | ||
Height | 16.70 m 54 ft 9 in |
16.85 m 55 ft 3 in |
17.10 m 56 ft 1 in |
17.30 m 56 ft 9 in |
Cabin width | 5.28 m (17.3 ft) | |||
Fuselage width | 5.64 m (18.5 ft) | |||
Wheelbase | 23.24 m 76 ft 3 in |
25.60 m 84 ft 0 in |
27.59 m 90 ft 6 in |
32.89 m 107 ft 11 in |
Typical empty weight | 129,000 kg 284,396 lb |
129,275 kg 295,503 lb |
170,400 kg 375,668 lb |
177,000 kg 390,218 lb |
Maximum take-off weight | 275,000 kg 606,300 lb |
276,500 kg 609,600 lb |
372,000/380,000 kg 820,100 /837,800 lb |
368,000/380,000 kg 811,300/837,800 lb |
Cruising speed | Mach 0.82 (896 km/h, 484 knots, 557 mph | Mach 0.83 (907 km/h, 490 knots, 564 mph) | ||
Take off run at MTOW | 2,990 m 9,810 ft |
3,000 m 9,840 ft |
3,050 m 10,000 ft |
3,100 m 10,170 ft |
Range fully loaded | 14,800 km 8,000 NM | 13,700 km 7,400 NM | 16,020/16,700 km 8,650/9,000 NM | 14,360/14,630 km 7,750/7,900 NM |
Max. fuel capacity | 155,040 L 40,957 gal | 140,640 L 37,153 gal | 214,810/222,000 L 56,750/58,646 gal | 195,881/204,500 L 51,746/54,023 gal |
Cargo capacity | 18 LD3s/6 pallets | 30 LD3s/10 pallets | 32 LD3s/11 pallets | 42 LD3s/14 pallets |
Service ceiling | 11,887 m 39,000 ft | |||
Engines (4x) | CFM56-5C2 (138.78 kN) CFM56-5C3 (144.57 kN) CFM56-5C4 (151.25 kN) |
CFM56-5C2 (138.78 kN) CFM56-5C3 (144.57 kN) CFM56-5C4 (151.25 kN) CFM56-5C4P (149.9 kN) |
Rolls-Royce Trent 553/556 (236/249 kN) |
Trent 556/560 (249/260 kN) |