Technical Data Airbus A300-600
Aircraft Dimensions
| ft | m | |
| Overall length | 177ft. 5in. | 54.10 |
| Height | 54ft. 3in. | 16.54 |
| Fuselage diameter | 18ft. 5in. | 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 | 249-267 kN |
| Number of LD3 cargo containers | 22 (23) | 22 (23) |
| Typical passenger seating | 266 | 266 |
| Maximum passenger load | 361 | 361 |
| Max. operating Mach number (Mmo) | 0.82 Mo. | 0.82 Mo. |
Design Weights
| imperial | metric | |
| Max. ramp weight | 380.5 lbs. x 1000 | 172.6 t |
| Max. take-off weight | 378.5 lbs. x 1000 | 171.7 t |
| Max. landing weight | 308.6 lbs. x 1000 | 140 t |
| Max. zero fuel weight | 286.6 lbs. x 1000 | 130 t |
| Maximum fuel capacity | 18 000 US gal. | 68,150 l |
| Typical operating weight empty | 200.4 lbs. x 1000 | 90.9 t |
| Maximum payload | 76.9 lbs. x 1000 | 34.9 t |
