Airbus A330: Difference between revisions

From FSAirlinesWiki
Jump to navigation Jump to search
 
Line 63: Line 63:
==A330-200F==
==A330-200F==
==A330-300==
==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
==Specifications==
==Specifications==
[[Category:Widebody Jetliners]]
[[Category:Widebody Jetliners]]

Revision as of 06:29, 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$-160,000,000v$
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

Specifications