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Dassault Aviation SA
MD 315 Flamant



Dassault Flamant at the 2010 ILA Berlin Air Show
Role Military transport aircraft
Manufacturer Dassault Aviation
First flight 6 July 1947 (MD.315)
Introduction 1948
Retired 1981
Primary users French Air Force
Republic of Vietnam Air Force
Tunisian Air Force
Cambodian Air Force
Number built 325
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History Dassault Aviation SA
Dassault MD 315 Flamant

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 tricycle undercarriage, powered by two Renault 12S piston engines.

The Dassault MD 315 Flamant is a French light twin-engined transport airplane built shortly after World War II by Dassault Aviation for the French Air Force..

Variants

  Dassault MD312 Flamant, F-AZZR
MB 30-1
Original proposals for a bombing and navigation trainer.
MB 30-2
Original proposals for a medical and colonial roles.
MB 30-3
Original proposals for a liaison and training aircraft.
MD 303
Dassault MD 311 Flamant trainer at the Paris Air Show 2007
Prototype, one built, powered by two 310 kW (410 hp) Béarn 6D engines.
MD 311
Bombing, navigation and photography training aircraft, 41 built (1 prototype + 40 production), powered by two 310 kW (410 hp) SNECMA 12S engines.
MD 312
Multi-engine pilot trainer and six-seat transport and communications aircraft, 118 built, powered by two 310 kW (410 hp) SNECMA 12S engines.
MD 312M
Utility aircraft for French Navy. 25 built.
MD 312B
Experimental version with a single fin, rectangular fuselage windows, and a heavier loaded weight. One built, powered by two 310 kW (410 hp) SNECMA 12S engines. Used later for Mirage IV radar development.
MD 315
Ten-seat utility transport aircraft, 137 built, powered by two 310 kW (410 hp) SNECMA 12S engines.
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Avions Marcel Dassault-Breguet Aviation

Dassault Aviation SA Avions
Marcel Dassault-Breguet Aviation
Dassault MD 315 Flamant

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General Info

    • Crew: 2
    • Capacity: 10 passengers
    • Length: 12.50 m (41 ft 0 in)
    • Wingspan: 20.70 m (67 ft 11 in)
    • Height: 4.50 m (14 ft 9 in)
    • Wing area: 47.2 m2 (508 sq ft)
2

Powerplant

  • Empty weight: 4,250 kg (9,370 lb)
  • Gross weight: 5,800 kg (12,787 lb)
  • Powerplant: 2 × Renault 12S 02-201 air-cooled inverted V12 engines, 430 kW (580 hp) each
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Specifications

  • Maximum speed: 380 km/h (240 mph
  • Cruise speed: 300 km/h (190 mph, 
  • Range: 1,200 km (750 mi, 650 nmi)
  • Service ceiling: 8,000 m (26,000 ft)
4

Armament

      • Guns: 2 × .50 in (12.7 mm) Browning machine guns
      • Hardpoints: 4 , with provisions to carry combinations of:
        • Rockets: 4 x 105 mm rockets or 4 x Matra launchers (7 x 68 mm rockets each)
        • Bombs: 4 x 50 kg (110 lb) bombs
     
Special Links Avions Marcel Dassault-Breguet Aviation

Links to Youtube & Others

The first Flamant was delivered to the French Air Force in 1949 and deliveries of all versions were completed by 1953

Dassault Aviation SA Dassault MD 315 Flamant

he Flamant stayed in service until 1981. In addition to the French air force,

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Youtube Link

he Flamant stayed in service until 1981. In addition to the French air force, the Flamant served in Cambodia, Madagascar, Tunisia, and Vietnam

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Aircrafttotal : Avions Marcel Dassault-Breguet Aviation

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