Breguet Br. 941 (940/941)
Photo ©: T. Laurent (photos at airliners.net)
Br. 941 (940/941)
STOL Transport Aircraft
The Breguet Br. 941 is a four-engine military STOL transport aircraft produced by the French manufacturer Breguet (Société Anonyme des Ateliers d'Aviation Louis Breguet).
| Crew | 2 | |
| Propulsion | 4 Turboprop Engines | |
| Engine Model | Turbomeca Turmo IIID3 | |
| Engine Power (each) | 1104 kW | 1480 shp |
| Speed | 450 km/h | 243 kts 280 mph |
| Service Ceiling | 9.500 m | 31.168 ft |
| Range | 1.000 km | 540 NM 621 mi. |
| Empty Weight | 13.460 kg | 29.674 lbs |
| max. Takeoff Weight | 26.500 kg | 58.422 lbs |
| Wing Span | 23,40 m | 76,8 ft |
| Wing Area | 83,8 m² | 902 ft² |
| Length | 23,75 m | 77,9 ft |
| Height | 9,65 m | 31,7 ft |
| First Flight | 01.06.1962 | |
| Production Status | out of production | |
| Total Production | 5 | |
| Data for (Version) | Breguet Br.941S | |
| Variants | Br.940, Br.941, Br.941S | |
| Extras | |
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