Breguet 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).
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 ft 9 in |
Wing Area | 83,8 m² | 902 ft² |
Length | 23,75 m | 77 ft 11 in |
Height | 9,65 m | 31 ft 8 in |
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 |