Dewoitine D.26
Trainer
The Dewoitine D.26 is a single-engine single-seat trainer aircraft developed by the French manufacturer Dewoitine.
The Dewoitine D.26 was a lowered powered variant of the
Dewoitine D.27 fighter and was assembled by EKW (Eidgenösschische Konstruktionswerkstätten) in Switzerland. The D.26 was in Service with the Schweizer Luftwaffe / Swiss Air Force only.
Propulsion | 1 Radial Engine |
Engine Model | Hispano-Suiza 9Qa |
Engine Power | 184 kW | 247 hp |
Speed | 241 km/h | 130 kts 150 mph |
Service Ceiling | 7.500 m | 24.606 ft |
Rate of climb | 432 m/min | 1417 ft/min |
Range | 500 km | 270 NM 311 mi. |
Empty Weight | 763 kg | 1.682 lbs |
max. Takeoff Weight | 1.068 kg | 2.355 lbs |
Wing Span | 10,30 m | 33 ft 10 in |
Wing Area | 17,6 m² | 189 ft² |
Length | 6,72 m | 22 ft 1 in |
Height | 2,78 m | 9 ft 1 in |
First Flight | 04.12.1929 |
Production Status | out of production |
Total Production | 11 |
Developed from | Dewoitine D.27 |
ICAO Code | DWD2 |
Data for (Version) | Dewoitine D.26 |