Difference between revisions of "Airbus A330"

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==A330-200==
 
==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==
 
==A330-200F==
 
==A330-300==
 
==A330-300==
 +
 
==Specifications==
 
==Specifications==
 +
{| class=wikitable style="text-align: center;"
 +
|-
 +
! Aircraft dimensions !! A330-200 !!  A330-300 !! A330-200F
 +
|- bgColor="#c9d5e6"
 +
| Overall length || 58.8 m (192 ft 11 in) || 63.6 m (208 ft 10 in) || 58.8 m (192 ft 11 in)
 +
|- bgColor="#e1e8f1"
 +
| 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)
 +
|- bgColor="#c9d5e6"
 +
| Fuselage diameter || colspan="3" | 5.64 m (18 ft 6 in)
 +
|- bgColor="#e1e8f1"
 +
| Maximum cabin width || colspan="3" | 5.28 m (17 ft 4 in)
 +
|- bgColor="#c9d5e6"
 +
| Cabin length ||  45.0 m (147 ft 8 in) || 50.35 m (165 ft 2 in) || 40.8 m (133 ft 10 in)
 +
|- bgColor="#e1e8f1"
 +
| Wingspan (geometric) || colspan="3" | 60.3 m (197 ft 10 in)
 +
|- bgColor="#c9d5e6"
 +
| Wing area (reference) || colspan="3" | 361.6 m² (3,892 sq ft)
 +
|- bgColor="#e1e8f1"
 +
| Wing sweep (25% chord) || colspan="3" | 30 degrees 
 +
|- bgColor="#c9d5e6"
 +
| Wheelbase || 22.2 m (72 ft 10 in) || 25.6 m (84 ft) || 22.2 m (72 ft 10 in)
 +
|- bgColor="#e1e8f1"
 +
| Wheel track || colspan="3" | 10.69 m (35 ft 1 in)
 +
|-
 +
! Basic operating data || colspan="3" |
 +
|- bgColor="#c9d5e6"
 +
| Engines || colspan="3" | two CF6-80E1 or PW4000 or RR Trent 700
 +
|- bgColor="#e1e8f1"
 +
| Engine thrust range || colspan="3" |303-320 kN 
 +
|- bgColor="#c9d5e6"
 +
| Typical passenger seating || 253 (3-class)<br>293 (2-class)<br>405 (1-class) || 295 (3-class)<br>335 (2-class) || - 
 +
|- bgColor="#e1e8f1"
 +
| Range (w/max. passengers) || 6,749 NM<br>(12,500&nbsp;km) || 5,669 NM<br>(10,500&nbsp;km) || 4,000 NM<br>(7,400&nbsp;km)
 +
|- bgColor="#c9d5e6"
 +
| Cruising Speed || colspan="3" | Mach 0.82 (871&nbsp;km/h, 541 mph, 470 knots at 35,000 ft (10.7&nbsp;km) cruise altitude)
 +
|- bgColor="c9d5e6"
 +
| Maximum Cruise Speed || colspan="3" | Mach 0.86  (913&nbsp;km/h, 568 mph, 493 knots at 35,000 ft (10.7&nbsp;km) cruise altitude)
 +
|- bgColor="#e1e8f1"
 +
| Takeoff run at MTOW || 2,220 metres (7,300 ft) || 2,500 metres (8,202 ft) || -
 +
|-
 +
| Bulk hold volume (Standard/option) || colspan="2" | 19.7 / 13.76 m³ || 475 m³
 +
|-
 +
! Design weights || colspan="3" |
 +
|- bgColor="#c9d5e6"
 +
| Maximum ramp weight || colspan="3" | 230.9 (233.9) [[tonne|t]]
 +
|- bgColor="#e1e8f1"
 +
| Maximum takeoff weight || colspan="3" | 230 (233) t
 +
|- bgColor="#c9d5e6"
 +
| Maximum landing weight || 180 (182) t || 185 (187) t || 182 (187) t     
 +
|- bgColor="#e1e8f1"
 +
| Maximum zero fuel weight || 168 (170) t || 173 (175) t || 173 (178) t
 +
|- bgColor="#c9d5e6"
 +
| Maximum fuel capacity || 139,100 L || 97,170 L  || 139,100 L 
 +
|- bgColor="#e1e8f1"
 +
| Typical operating weight empty || 120 t || 122 (124) t  || 109 t 
 +
|- bgColor="#c9d5e6"
 +
| Typical volumetric payload || 36.4 t || 45.9 t || 69 t
 +
|}
 +
 
[[Category:Widebody Jetliners]]
 
[[Category:Widebody Jetliners]]

Latest revision as of 18:16, 24 December 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

A330-200

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
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