Dassault MD 315 Flamant
|Dassault MD 312 Flamant of the Armée de l'Air at Basle-Mulhouse (Euroairport), September 1977|
|Role||Military transport aircraft|
|First flight||6 July 1947 (MD.315)|
|Primary users||French Air Force
Vietnam Air Force
Tunisian Air Force
Cambodian Air Force
Design and development
Design work on a twin-engined light transport started in 1946 with the MD 303, a development of an earlier project for an eight-seat communications aircraft the Marcel Bloch MB-30. The prototype MD 303 first flew on 26 February 1947 powered by two Béarn 6D engines, designed to meet a French Air Force requirement for a colonial communications aircraft. A re-engined version was ordered into production at the new Dassault factory at Bordeaux-Mérignac. The production aircraft was a low-wing monoplane with twin tail surfaces and a tri-cycle undercarriage and powered by two Renault 12S piston engines.
Three main versions of the aircraft now named Flamant (means Flamingo in French) were produced. The MD 315 10-seat colonial communication aircraft (first flown on 6 July 1947), the MD 312 six-seat transport aircraft (first flew on 27 April 1950), and the MD 311 navigation trainer (first flew on 23 March 1948. The MD 311 had a distinctive glazed nose for its role as both a bombing and navigation trainer.
The aircraft was used for pilot training, navigation training, light transport, maritime surveillance and light ground attack. During the Algerian War of Independence the plane was used for light attack with the Nord SS.11 and AS.11 antitank missiles or with machine guns, bombs, and rockets. The Flamant MD 311 (which were based in Algeria to train pilots and navigators at first) was the first aircraft in history to fire one of the world's first wire guided antitank missile in anger, using French Army SS.11 antitank missiles, in a combat experiment to get at fortified caves located in deep mountain gorges, 1956 from an aircraft based with the special unit of the French Air Force in Algeria, GOM.86. The SS.11 attacks proved extremely successful and the French Army which had provided the missiles, began an experiment which resulted in the worlds first attack helicopters firing antitank missiles. The Flamant stayed in service until 1981. In addition to the French air force, the Flamant served in Cambodia, Madagascar, Tunisia, and Vietnam.
- MB 30-1
- Original proposals for a bombing and navigation trainer.
- MB 30-2
- Original proposals fora medical and colonial roles.
- MB 30-3
- Original proposals for a liaison and training aircraft.
- MD 303
- Prototype, one built, powered by two 310 kW (410 hp) Béarn 6D engines.
- MD 311
- Bombing, navigation and photography training aircraft, 39 built, powered by two 310 kW (410 hp) SNECMA 12S engines.
- MD 312
- Six-seat transport and communications aircraft, 142 built, powered by two 310 kW (410 hp) SNECMA 12S engines.
- MD 312B
- Experimental version with heavier loaded weight, one built, powered by two 310 kW (410 hp) SNECMA 12S engines. Used later for Mirage IV radar development.
- MD 315
- 10-seat utility transport aircraft, 137 built, powered by two 310 kW (410 hp) SNECMA 12S engines.
- MD 316T
- One prototype fitted with a single-finned tail, and two 600 kW (800 hp) Wright R-1300-CB7A1 Cyclone radial piston engines.
- MD 316X
- One MD 315 aircraft fitted with two 610 kW (820 hp) SNECMA 14X Super Mars radial piston engines.
- Cambodian Air Force (MD 315)
- Cameroon Air Force (MD 315)
- Madagascar Aeronaval Force (MD 315, MD 312)
- Vietnam Air Force (MD 312, MD 315)
- Tunisian Air Force (MD 312)
Specifications (MD 315)
Data from Jane's All The World's Aircraft 1953–54
- Crew: 2
- Capacity: 10 passengers
- Length: 12.50 m (41 ft 0 in)
- Wingspan: 20.70 m (67 ft 10 in)
- Height: 4.50 m (14 ft 9 in)
- Wing area: 47.2 m² (508 ft²)
- Empty weight: 4,250 kg (9,350 lb)
- Max. takeoff weight: 5,800 kg (12,760 lb)
- Powerplant: 2 × Renault 12S 02-201 inline piston, 433 kW (580 hp) each
- Maximum speed: 380 km/h (205 knots, 236 mph)
- Cruise speed: 300 km/h (162 knots, 186 mph)
- Range: 1,200 km (648 nmi, 745 km)
- Service ceiling: 8,000 m (26,240 ft)
- Rate of climb: 5.0 m/s (985 ft/min)
- Related lists
|Wikimedia Commons has media related to Dassault Flamant.|
- COIN: French Counter-Insurgency Aircraft, 1946-1965 Pt.1
- Bridgman 1953, pp. 133–134.
- Bridgman, Leonard (ed.) Jane's All The World's Aircraft 1953-54. London:Jane's, 1953.