Airbus A330
| 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$-160,000,000v$ |
| File:Airplanes-Airbus A330.jpg | |
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
A330-300 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 25.6 m. 84 ft. 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 295 (3-class) 335 (2-class) 295 (3-class) 335 (2-class) Range (w/max. passengers) 10,500 km. 5,650 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 185 (187) tonnes 407.9 (412.3) lbs. x 1000 Maximum zero fuel weight 173 (175) tonnes 381.4 (385.8) lbs. x 1000 Maximum fuel capacity 97,170 Litres 25,670 US gal. Typical operating weight empty 122.2 (124.5) tonnes 267.2 (274.5) lbs. x 1000 Typical volumetric payload 45.9 tonnes 101.2 lbs. x