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 |
