Morane-Saulnier MS.315

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Morane-Saulnier MS.315
Morane-Saulnier MS-317 img 0515.jpg
Morane-Saulnier MS.317
Role Primary trainer
National origin France
Manufacturer Morane-Saulnier
First flight 1932
Primary user French Air Force
Number built 356

The Morane-Saulnier MS.315 is a primary training monoplane designed and built in France by Morane-Saulnier.

Development[edit]

The MS.315 was developed from the earlier MS.300 primary trainer and related variants and first flew in October 1932. The MS.315 is a parasol-wing monoplane with a tailwheel, with divided main landing gear, and powered by a 135hp (101kW) Salmson 9Nc radial engine. A production run of 346 aircraft followed the four prototypes (including 33 built after the Second World War). Five high-powered MS.317/2 variants were also produced for the civil market, and a single MS.316 was built, powered by a Regnier inverted Vee engine.

In the 1960s 40 MS.315 used as civil glider tugs were modified with a 220hp (164kW) Continental W-670K radial engine and re-designated the MS.317.


Variants[edit]

MS.315
Production version with a 135hp (101kW) Salmson 9Nc radial engine, 350 built.
MS.315/2
Higher powered civil version, five built.
MS.316
Variant powered by a Regnier inverted Vee engine, one built.
MS.317
1960s conversions with a 220hp (164kW) Continental W-670K radial engine, 40 converted.

Operators[edit]

 France
 Peru

Specifications (MS.315)[edit]

Data from [1]

General characteristics

  • Crew: 2
  • Length: 7.60 m (24 ft 11¼ in)
  • Wingspan: 12.00 m (39 ft 4½ in)
  • Height: 2.80 m (9 ft 2¼ in)
  • Wing area: 21.60 m2 (232.51 ft2)
  • Empty weight: 548 kg (1208 lb)
  • Gross weight: 860 kg (1896 lb)
  • Powerplant: 1 × Salmson 9Nc radial engine, 101 kW (135 hp)

Performance

  • Maximum speed: 170 km/h (106 mph)
  • Service ceiling: 5500 m (18,045 ft)

See also[edit]

Related lists

References[edit]

  1. ^ Orbis 1985, page 2556