Difference between revisions of "Airbus A330"
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==A330-200F== | ==A330-200F== | ||
==A330-300== | ==A330-300== | ||
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==Specifications== | ==Specifications== | ||
Revision as of 23:40, 11 September 2009
| Airbus A330 at a Glance | |
|---|---|
| Role | Widebody Jetliner |
| Country of Origin | France |
| Manufacturer | Airbus |
| Status | In Production |
| Number Built | 633 |
| Unit Cost | 150,000,000v$-160,000,000v$ |
| 262px | |
Contents
A330-200
A330-200 SPECIFICATIONS AIRCRAFT DIMENSIONS metric imperial Overall lenagth 58.8 m. 188 ft. 8 in. Height 17.40 m. 57 ft. 1 in. Fuselage diameter 5.64 m. 18 ft. 6 in. Maximum cabin width 5.28 m. 17 ft. 4 in. Cabin length 45.0 m. 147 ft. 8 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 22.2 m. 72 ft. 10 in. Wheel track 10.69 m. 35 ft. 1 in. BASIC OPERATING DATA metric imperial Engines two CF6-80E1 or PW4000 or RR Trent 700 two CF6-80E1 or PW4000 or RR Trent 700 Engine thrust range 303-320 kN 68,000-72,000 lb. slst Typical passenger seating 253 (3-class) 293 (2-class) 253 (3-class) 293 (2-class) Range (w/max. passengers) 12,500 km. 6,750 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 230.9 (233.9 ) tonnes 509 (515.7) lbs. x 1000 Maximum takeoff weight 230 (233) tonnes 507 (513.7) lbs. x 1000 Maximum landing weight 180 (182) tonnes 396.8 (401.2) lbs. x 1000 Maximum zero fuel weight 168 (170) tonnes 370.4 (374.8) lbs. x 1000 Maximum fuel capacity 139,100 Litres 36,750 US gal. Typical operating weight empty 119.6 tonnes 263.7 lbs. x 1000 Typical volumetric payload 36.4 tonnes 80.2 lbs. x 1000
A330-200F
A330-300
Specifications
| Aircraft dimensions | A330-200 | A330-300 | A330-200F |
|---|---|---|---|
| Overall length | 58.8 m (192 ft 11 in) | 63.6 m (208 ft 10 in) | 58.8 m (192 ft 11 in) |
| Height (to top of horizontal tail) | 17.40 m (57 ft 1 in) | 16.85 m (55 ft 3 in) | 16.9 m (55 ft 5 in) |
| Fuselage diameter | 5.64 m (18 ft 6 in) | ||
| Maximum cabin width | 5.28 m (17 ft 4 in) | ||
| Cabin length | 45.0 m (147 ft 8 in) | 50.35 m (165 ft 2 in) | 40.8 m (133 ft 10 in) |
| Wingspan (geometric) | 60.3 m (197 ft 10 in) | ||
| Wing area (reference) | 361.6 m² (3,892 sq ft) | ||
| Wing sweep (25% chord) | 30 degrees | ||
| Wheelbase | 22.2 m (72 ft 10 in) | 25.6 m (84 ft) | 22.2 m (72 ft 10 in) |
| Wheel track | 10.69 m (35 ft 1 in) | ||
| Basic operating data | |||
| Engines | two CF6-80E1 or PW4000 or RR Trent 700 | ||
| Engine thrust range | 303-320 kN | ||
| Typical passenger seating | 253 (3-class) 293 (2-class) 405 (1-class) |
295 (3-class) 335 (2-class) |
- |
| Range (w/max. passengers) | 6,749 NM (12,500 km) |
5,669 NM (10,500 km) |
4,000 NM (7,400 km) |
| Cruising Speed | Mach 0.82 (871 km/h, 541 mph, 470 knots at 35,000 ft (10.7 km) cruise altitude) | ||
| Maximum Cruise Speed | Mach 0.86 (913 km/h, 568 mph, 493 knots at 35,000 ft (10.7 km) cruise altitude) | ||
| Takeoff run at MTOW | 2,220 metres (7,300 ft) | 2,500 metres (8,202 ft) | - |
| Bulk hold volume (Standard/option) | 19.7 / 13.76 m³ | 475 m³ | |
| Design weights | |||
| Maximum ramp weight | 230.9 (233.9) t | ||
| Maximum takeoff weight | 230 (233) t | ||
| Maximum landing weight | 180 (182) t | 185 (187) t | 182 (187) t |
| Maximum zero fuel weight | 168 (170) t | 173 (175) t | 173 (178) t |
| Maximum fuel capacity | 139,100 L | 97,170 L | 139,100 L |
| Typical operating weight empty | 120 t | 122 (124) t | 109 t |
| Typical volumetric payload | 36.4 t | 45.9 t | 69 t |
