Technical Data Airbus A300-600F
Aircraft Dimensions
| ft | m | |
| Overall length | 177ft. 5in. | 54.10 |
| Height | 54ft. 3in. | 16.54 |
| Fuselage diameter | 18ft. 6in. | 5.64 |
| Maximum cabin width | 17ft. 4in. | 5.28 |
| Cabin length | 133ft. 6in. | 40.70 |
| Wing span (geometric) | 147ft. 1in. | 44.84 |
| Wing area (reference) | 2,800 ft2 | 260 m2 |
| Wing sweep (25% chord) | 28 degrees | 28 degrees |
| Wheelbase | 61ft. 1in. | 18.62 |
| Wheel track | 31ft. 6in. | 9.60 |
Basic Operation Data
| imperial | metric | |
| Engines | two CF6-80C2 or PW4000 | two CF6-80C2 or PW4000 |
| Engine thrust range | 56 000-61 500 lb. slst | 249-270 kN |
| Typical passenger seating | 15 (21) pallets | 15 (21) pallets |
| Range (max. pax) | 1 950 (2 650) nm | 3,650 (4,850) km |
| Max. operating Mach number (Mmo) | 0.82 Mo. | 0.82 Mo. |
| Bulk hold volume - Standard/option | 398 ft3 | 11.27 m3 |
Design Weights
| imperial | metric | |
| Max. ramp weight | 377.9 (366) lbs. x 1000 | 171.4 (168.8) t |
| Max. take-off weight | 375.9 (370.4) lbs. x 1000 | 170.5 (168) t |
| Max. landing weight | 308.6 (315.5) lbs. x 1000 | 140 (143.3) t |
| Max. zero fuel weight | 286.6 (300.9) lbs. x 1000 | 130 (136.5) t |
| Maximum fuel capacity | 18 000 (11 730) US gal. | 68,150 (44,400) l |
| Typical operating weight empty | 180.7 lbs. x 1000 | 81.9 t |
| Typical volumetric payload | 105.9 ( 120.2 ) lbs. x 1000 | 48.1 / 54.6 t |
