Airbus A310

· Airbus · 2 × Pratt & Whitney PW4000

Airplanes

Length

46.66 m

Flat Wing Span

43.9 m

Height

15.867 m

Flat Wing Area

219 m²

Max Seating

243

Max Mach

0.84 Mach

Max Ceiling

12530 m

Number of Engines

Aircraft Engine

First Flight

1982-04-03

Entry Into service

1983-04-01

Number Built

255

Maximum Take-Off Weight

164 t (paragliders: kg)

Total Fuel Capacity

61070

Maximum Range

9537.8 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Airbus A310	164	61070	9537.8

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Airbus A310 MRTT		47.4	43.9	214	Compare
Airbus CC-150 Polaris		46.66	43.9	194	Compare
Boeing E-767	General Electric CF6	48.5	47.6		Compare
Kawasaki C-2	General Electric CF6	43.9	44.4		Compare
Tupolev Tu-330		42	43.5		Compare
Boeing KC-767	General Electric CF6	48.5	47.6	200	Compare

All data (25 fields)

Name: Airbus A310
Manufacturer: Airbus
Description: The Airbus A310 is a wide-body airliner designed and manufactured by Airbus Industrie GIE, then a consortium of European aerospace manufacturers.
ICAO Code: A310
First Flight: 1982-04-03
Entry Into service: 1983-04-01
Designer: Airbus
Length (m): 46.66
Height (m): 15.867
Cockpit Crew: 2
Max Seating: 243
Max Ceiling (m): 12530
Capacity Description: 243 passengers, 112.2 m3 (3,962 cu ft) cargo volume
Max Mach (Mach): 0.84
National Origin: Multi-national
Number Built: 255
Powerplant Description: 2 × Pratt & Whitney PW4156A high bypass turbofan, 249.08 kN thrust each
Primary Users: Mahan Air, ULS Airlines Cargo, Iran Air, Ariana Afghan Airlines
Status: In limited service
Wikipedia Article (URL): en.wikipedia.org/wiki/Airbus_A310
Flat Wing Span (m): 43.9
Flat Wing Area (m²): 219
Wake Category: H
Aircraft Engine: Pratt & Whitney PW4000
Number of Engines: 2