Airbus A300-600R

Airbus SAS

Airbus A300-600R aircraft
Airbus SASAirbus A300-600R
Photo: Samslipknot at English Wikipedia · Public domain · Modified

About

The A300-600R adds a tail trim tank — 6,150 litres in the horizontal stabiliser, moving fuel aft to trim the aeroplane in cruise — and 6.7 tonnes of take-off weight, for 68,150 litres of fuel against the -600's 62,000. Certified in March 1988, it is the last and heaviest passenger A300 and the version most of the surviving fleet flies. Cruise speed, range, ceiling and climb rate are EUROCONTROL's figures for the A306 type code rather than a certificate's: a type certificate states limits and weights, not cruise performance, and the source does not distinguish sub-variants.

Weightscompared to Airbus A380-800

MRW (Maximum Ramp Weight)

172,600kg
0
200k
400k
577k

MTOW (Maximum Takeoff Weight)

171,700kg
0
200k
400k
575k

MLW (Maximum Landing Weight)

140,000kg
0
150k
300k
395k

MZFW (Maximum Zero Fuel Weight)

130,000kg
0
150k
300k
369k

Empty Weight

88,805kg
0
100k
200k
280k

Capacitycompared to Airbus A380-800

Passenger Capacity

361passengers
0
300
600
853

42% of A380 maximum capacity

Crew

Total
10
Cockpit
2
Cabin
8

Dimensions

Length

54.1m

Wingspan

44.8m

Height

16.7m

Engine Specifications

Engine Count

2×

Engine Model

General Electric CF6-80C2 or Pratt & Whitney PW4158

Fuel & Cargo

Fuel Capacity

68,150 L

Cargo Volume

158.54 m³

Production & History

Production Status

Out of production