A300-600ST

Family: A300 · Airbus · 2 × CF6-80C2A8

Length

56.15 m

Flat Wing Span

44.84 m

Height

17.24 m

Flat Wing Area

260 m²

Max Mach

0.7 Mach

Max Ceiling

10668 m

Number of Engines

Aircraft Engine

First Flight

1994-09-13

Entry Into service

1996-01-15

Number Built

Maximum Take-Off Weight

155 t (paragliders: kg)

Total Fuel Capacity

23860

Maximum Range

2779 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
A300-600ST	155	23860	2779

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Airbus A310 MRTT		47.4	43.9	214	Compare
Airbus A310	Pratt & Whitney PW4000	46.66	43.9	243	Compare
Antonov An-218		59.79	50	400	Compare
767-200	Pratt & Whitney PW4000	54.94	47.57		Compare
Boeing E-767	General Electric CF6	48.5	47.6		Compare
Airbus CC-150 Polaris		46.66	43.9	194	Compare

All data (27 fields)

Name: A300-600ST
Manufacturer: Airbus
Family: A300
Description: The Airbus A300-600ST (Super Transporter) or Beluga is a specialised wide-body airliner used to transport aircraft parts and outsize cargoes.
ICAO Code: A3ST
EASA TCDSN: EASA.A.014
Program Launch: 1991-08-22
First Flight: 1994-09-13
Certification: 1995-10-25
Entry Into service: 1996-01-15
Launch Customer: Airbus Transport Int.
Type: Oversized freight aircraft
Length (m): 56.15
Height (m): 17.24
Cockpit Crew: 2
Max Ceiling (m): 10668
Capacity Description: 47000 kg typical load
Max Mach (Mach): 0.7
Number Built: 5
Powerplant Description: 2 × General Electric CF6-80C2A8 turbofan, 257 kN thrust each
Primary Users: Airbus Transport International
Wikipedia Article (URL): en.wikipedia.org/wiki/Airbus_Beluga
Flat Wing Span (m): 44.84
Flat Wing Area (m²): 260
Wake Category: H
Aircraft Engine: CF6-80C2A8
Number of Engines: 2