Merville D.63

Source: Wikipedia, the free encyclopedia.
D.63
The sole D.63 at St Cyr l'École airfield near Paris in 1965
Role Side by side trainer
National origin France
Manufacturer Helice G. Merville
Designer André Merville
First flight 23 March 1962
Number built 1

The Merville D.63 was a modification of the

nosewheel undercarriage, modified fin and French
engine. It flew in 1962.

Development

In the 1960s, André Merville was president of the

The D.63 was wood framed and covered with a mixture of

elevator
. The fuselage was entirely ply covered. Pilot and passenger sat
propeller made by Melville Helices.[3]

The D.63 first flew on 23 March 1962[3] and appeared at the Cannes light aircraft show in July that year.[4]

Specifications

Data from Jane's All the World's Aircraft p.47[3]

General characteristics

  • Crew: Two
  • Length: 6.75 m (22 ft 2 in)
  • Wingspan: 8.38 m (27 ft 6 in)
  • Height: 2.25 m (7 ft 5 in)
  • Wing area: 11.50 m2 (123.8 sq ft)
  • Empty weight: 460 kg (1,014 lb) with oil
  • Max takeoff weight: 703 kg (1,550 lb)
  • Fuel capacity: 105 L (23.1 Imp gal; 27.2 US gal)
  • Maximimum wing loading: 61 kg/m2 (12.5 lb/sqft)
  • Maximum power loading: 14.8 lb/hp (9.0 kg/kW)
  • Powerplant: 1 ×
    flat four
    , 78 kW (105 hp)
  • Propellers: 2-bladed Merville 963, wooden, fixed pitch

Performance

  • Maximum speed: 215 km/h (134 mph, 116 kn) at sea level; like all the performance figures, this is at maximum take-off weight
  • Cruise speed: 195 km/h (121 mph, 105 kn)
  • Stall speed: 80 km/h (50 mph, 43 kn)
  • Range: 850 km (530 mi, 460 nmi) with maximum fuel


References

  1. ^ Taylor, John W R (1960). Jane's All the World's Aircraft 1960-61. London: Sampson Low, Marston & Co. Ltd. p. 137.
  2. ^ "Merville SM.31". Retrieved 12 March 2014.
  3. ^ a b c d Taylor, John W R (1964). Jane's All the World's Aircraft 1964-65. London: Sampson Low, Marston & Co. Ltd. p. 47.
  4. ^ "Light aircraft at Cannes". Flight. Vol. 82, no. 2782. 5 July 1962. p. 32.