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 |
