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Dimensions & key data

Key figures

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  Range 4 050 nm 7 500 km
Typical seating x 266 (2-class)
  Max payload 76.9 lb x 1 000 34.9 tonnes
A300-600 Wing span Wing span 147 ft 1 in 44.84 m
A300-600 Overall length Overall length 177 ft 5 in 54.10 m
A300-600 Height Height 54 ft 3 in 16.5 m
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Dimensions

Overall length 177 ft 5 in 54.10 m
Cabin length 133 ft 6 in 40.70 m
Fuselage width 18 ft 0 in 5.64 m
Max cabin width 17 ft 4 in 5.28 m
Wing span (geometric) 147 ft 1 in 44.84 m
Height 54 ft 3 in 16.5 m
Track 31 ft 6 in 9.60 m
Wheelbase 61 ft 1 in 18.62 m

A300-600R

The A300-600R variant of Airbus’ cornerstone A300 entered commercial service in 1988, bringing increased range for this twin-engine jetliner as a result of a fuel trim tank located in its tail. From that point forward, all new production A300-600s were A300-600Rs.

Capacity

Pax
Typical seating 266 (2-class)
Max -
Freight
LD3 capacity underfloor 22 (23) 22 (23)
Max pallet number underfloor - -
Bulk hold volume 749 ft³ 21.21 m³
Total volume - -

Performance

Range 4 050 nm 7 500 km
Mmo M0.82
Max ramp weight 380.5 - lb x 1000 172.6 - tonnes
Max take-off weight 378.5 - lb x 1000 171.7 - tonnes
Max landing weight 308.6 lb x 1000 140 tonnes
Max zero fuel weight 286.6 lb x 1000 130 tonnes
Max fuel capacity 18 000 USG 68 150 litres

Engines

PW4000 x2 PW4000
CF6-80C2 x2 CF6-80C2
Thrust range 56,000-61,500 lb slst 249-270 kN