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Encyclopedia - Fairchild A-10 Thunderbolt
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Fairchild A-10A Thunderbolt II | General | | Crew : | One | | First Flight : | 21 October 1975 | | Country of Origin : | USA | Powerplant | | Number Of Engines : | Two | | Powerplant type : | General Electric TF34-GE-100 turbofans | | Max Power Rating : | 4,112kg (9,065lb) | Dimensions | | Length : | 16.26m (53ft 4in) | | Height : | 4.47m (14ft 8in) | | Wingspan : | 17.53m (57ft 6in) | | Wing Area : | 47.01m2 (506sq ft) | | Tailplane Span : | 5.74m (18ft 10in) | Weights | | Empty Weight : | 11,321kg (24,959lb) | | Max Take-off Weight : | 22,680kg (50,000lb) | | Internal fuel load : | 4,853kg (10,700lb) | Landing Gear | | Type : | Retractable tricycle type with a single wheel on each unit | | Wheelbase : | 5.40m (17ft 8.75in) | | Wheel Track : | 5.25m (17ft 2.5in) | Performance | | Max Speed At Sea Level : | 381kt (707km/h; 439mph) | | Service Ceiling : | 45,000ft (13,636m) |
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