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| Technical features | ||
| Wingspan | 21,30 m | ![]() |
| Length | 16,60 m | |
| Height | 5,60 m | |
| Wing aera | 50,10 m2 | |
| Empty weight | 10365 kg | |
| Gross weight | 12517 kg | |
| Max weight | 15876 kg | |
| Crew | 3 | |
| Max speed | 571 km/h | |
| Cruise speed | 457 km/h | |
| Ceiling | 6735 m | |
| Range | 2255 km | |
| Engines | 2 Pratt & Whitney R-2800-27 or -79 Double Wasp of 2000cv each | |
| CAEA's specimen |
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B-26 BuAer 44-35859, constructor number 29138 is an A-26C-50-DT converted to B-26APQ13, delivered to France by United States on june 16, 1960. It starts its career at the CEAM from july to november 1960, then at CIB 328, registered as F-UKEY / 328-EY until january 1967, being reformed on march 27, 1968 at Châteaudun. Then it come back and stay several years behind the base HQ of BA 106 Bordeaux-Mérignac before its dismantling by a CAEA team in 2000. Visible parts |
Contact : Denis Dumoulin
Images of engines arrival at Hangar 2
Gear up on March 18, 2000
Nose dismantling on June 24, 2000
Fuselage outdoor on February 24, 2001Aircraft condition on March 11, 2000
At Hangar 2 on June 10, 2000
Wingframe sheltered on November 11, 2000
Again sheltered on BA106 October 2001
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