|This image of the Merganser taken from a Percival Aircraft brochure, c. 1947.|
|Role||Light utility aeroplane|
|Manufacturer||Percival Aircraft Limited|
|First flight||9 May 1947|
|Number built||2 (1 flying)|
Design and development
The Merganser was designed as a five-passenger, light airliner with an emphasis on "passenger appeal". To this end, a high-wing configuration and tricycle landing gear were chosen to provide the best view and a low, level floor for easy access.
The fuselage, having been completed in November 1946, was shipped by train ferry to Paris to be displayed at the Aero Show. By this time, the Merganser was already doomed, since it was designed to be powered by de Havilland Gipsy Queen 51 engines and neither these nor any suitable substitute were available.
Only one Merganser was flown; when it made its first flight on 9 May 1947 from Luton Airport, the engines were on loan from the Ministry of Supply. The company was able to carry out extensive flight trials and obtain much valuable data. Although it appeared at the SBAC Show at Radlett in September 1947, it was scrapped at Luton in August 1948.
A second Merganser was used as a static and structural test airframe.
Although the Merganser never entered production, further development, based on the data gathered from its test programme, would lead to the larger Prince, President and Pembroke series for which a suitable powerplant was available.
- P.48 Merganser
- Five to eight-seat transport, one completed and two fuselages.
- P.48A Merganser
- Proposed floatplane variant, not built.
- P.48B Merganser
- Proposed ski-plane variant, not built.
- P.49 Merganser II
- Proposed aerial survey variant, not built.
Data from British Civil Aircraft since 1919, Volume III.
- Crew: 2
- Capacity: 5 passengers
- Length: 47 ft 9 in (14.56 m)
- Wingspan: 40 ft 8 in (12.40 m)
- Height: 13 ft 9 in (4.19 m)
- Wing area: 319 ft² (29.6 m²)
- Empty weight: 5,300 lb (2,409 kg)
- Loaded weight: 7,300 lb (3,318 kg)
- Powerplant: 2 × de Havilland Gipsy Queen 51 or 71 six-cylinder inline, 296 hp (221 kW) each
- Maximum speed: 168 knots (193 mph, 311 km/h)
- Cruise speed: 139 knots (160 mph, 258 km/h)
- Range: 696 NM (800 mi, 1,228 km)
- Service ceiling: 24,000 ft (7,310 m)
- Rate of climb: 1,010 ft/min (5.1 m/s)
- Wing loading: 22.9 lb/ft² (112 kg/m²)
- Power/mass: 0.081 hp/lb (0.13 kW/kg)
- Related development
- Jackson, A.J. British Civil Aircraft 1919-1972: Volume III. London: Putnam, 1988. ISBN 0-85177-818-6.