Morane-Saulnier MS.315
# Morane-Saulnier MS.315

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

## Development

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 tailskid, with divided main landing gear, and powered by a 135 hp (101 kW) 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 Régnier inverted Vee engine.

In the 1960s 40 MS.315 used as civil glider tugs were modified with a 220 hp (164 kW) Continental W670-K radial engine and re-designated the MS.317.

## Variants

### 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 W670-K radial engine, 40 converted.

## Operators

### France

* French Air Force
* French Navy

### Peru

* Peruvian Air Force

## Specifications (MS.315)

Data from

General characteristics

* Crew: 2
* Length: 7.60 m (24 ft 11.25 in)
* Wingspan: 12.00 m (39 ft 4.5 in)
* Height: 2.80 m (9 ft 2.25 in)
* Wing area: 21.60 $m^2$ (232.51 sq ft)
* Empty weight: 548 kg (1,208 lb)
* Gross weight: 860 kg (1,896 lb)
* Powerplant: 1 × Salmson 9Nc radial engine , 101 kW (135 hp)

Performance

* Maximum speed: 170 km/h (106 mph, 92 kn)
* Service ceiling: 5,500 m (18,045 ft)
