Commercial Aircraft Directory - Aircraft Specification
Airbus - A300C4
View specification units in: METRIC | IMPERIAL
SPECIFICATION
| First Flight date: | ||
| Certification date: | 18 Dec 1979 |
PRINCIPAL DIMENSIONS
| Fuselage width: | 5.64 m | |
| Fuselage height: | 7.71 m | |
| Fuselage length: | 53.61 m | |
| Cabin length: | 39.15 m | |
| Cabin width: | 5.3 m | |
| Cabin height: | 2.48 m | |
| Cabin volume: | 272 m3 | |
| Hold volume: | 140 m3 |
WEIGHTS
| Empty operating: | 88,500 kg | |
| Max zero fuel: | 124,000 kg | |
| MTOW: | 165,000 kg | |
| MLW: | 134,000 kg | |
| Standard fuel capacity: | 62,000 kg | |
| Max fuel capacity: | 62,000 kg |
SPEEDS
| Normal cruise: | 875 km/h | |
| Max cruise: | 918 km/h |
PERFORMANCE
| Long Range Cruise alt: | 10,668 m | |
| Max ceiling: | 12,192 m | |
| Take off field length: | 2,378 m | |
| Landing field length: | 1,824 m | |
| Max Payload Range: | 4,630 m | |
| Range notes: | ||
| Max passengers: | 345 | |
| Typical passengers: | 269 |
POWERPLANT
| Category: | Turbofan | |
| Manufacturer: | GE | |
| Model/Submodel: | CF6 50C2 | |
| Thrust: | 233 kN |
