Airbus A310-300

Airbus SAS

Airbus A310-300 aircraft
Airbus SASAirbus A310-300
Photo: MarcelX42 · CC BY-SA 4.0 · Modified

About

The A310-300 adds the tail trim tank and wingtip fences, taking usable fuel from 55,100 litres to 61,090 and take-off weight from 144 to 164 tonnes. That is what turned a short-haul widebody into a transatlantic one, and it was among the first twinjets to fly the Atlantic on ETOPS. It seats 243 in a single class, six more than the -200 in the same fuselage. Cruise speed, range, ceiling and climb rate are EUROCONTROL's figures for the A310 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)

164,900kg
0
200k
400k
577k

MTOW (Maximum Takeoff Weight)

164,000kg
0
200k
400k
575k

MLW (Maximum Landing Weight)

124,000kg
0
150k
300k
395k

MZFW (Maximum Zero Fuel Weight)

116,500kg
0
150k
300k
369k

Empty Weight

79,207kg
0
100k
200k
280k

Capacitycompared to Airbus A380-800

Passenger Capacity

275passengers
0
300
600
853

32% of A380 maximum capacity

Crew

Total
8
Cockpit
2
Cabin
6

Dimensions

Length

46.7m

Wingspan

43.9m

Height

15.9m

Engine Specifications

Engine Count

2×

Engine Model

General Electric CF6-80C2 or Pratt & Whitney JT9D-7R4 / PW4000

Fuel & Cargo

Fuel Capacity

61,090 L

Cargo Volume

112.2 m³

Production & History

Production Status

Out of production