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Morane-Saulnier MS.250

From Wikipedia, the free encyclopedia

Role trainer
Manufacturer Morane-Saulnier
First flight 1929
Number built 2

The Morane-Saulnier MS.250 was a crew-trainer aircraft built by Morane-Saulnier in the late 1920s.


The MS.250 was a parasol-wing monoplane with swept-back wings, similar to the Morane-Saulnier MS.230, but differed in having a new tail. The cockpits had windscreens, and the rear cockpit had a gun ring. The pilot-instructor manned the front cockpit, and the trainee observer manned the rear cockpit.[1] A second aircraft was built with a more powerful engine as the MS.251.[2]


Initial design prototype, powered by a 230 hp (170 kW) Salmson 9Ab radial engine; one built.[1]
A second aircraft, powered by a 240 hp (180 kW) Lorraine 7Mc radial engine.[2]

Specifications (MS.250)

Data from [3]

General characteristics

  • Crew: 2
  • Length: 6.96 m (22 ft 10 in)
  • Wingspan: 10.7 m (35 ft 1 in)
  • Height: 2.82 m (9 ft 3 in)
  • Wing area: 19.7 m2 (212 sq ft)
  • Empty weight: 889 kg (1,960 lb)
  • Gross weight: 1,210 kg (2,668 lb)
  • Powerplant: 1 × Salmson 9Ab 9-cylinder air-cooled radial piston engine, 170 kW (230 hp)
  • Propellers: 2-bladed fixed-pitch propeller


  • Maximum speed: 189 km/h (117 mph, 102 kn)
  • Cruise speed: 152 km/h (94 mph, 82 kn)
  • Service ceiling: 5,000 m (16,000 ft)
  • Rate of climb: 4.067 m/s (800.6 ft/min)


  • Guns: provision for a machine gun in a lobster-back turret in the rear cockpit


  1. ^ a b Rickard, J. (13 March 2012). "Morane-Saulnier M.S.250". historyofwar. Retrieved 6 February 2019.
  2. ^ a b Rickard, J. (13 March 2012). "Morane-Saulnier M.S.251". historyofwar. Retrieved 6 February 2019.
  3. ^ "Morane-Saulnier MS.250". (in Russian). Retrieved 6 February 2019.
This page was last edited on 17 February 2021, at 15:19
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