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Scottish Aviation
Twin Pioneer

 
General information
Type Transport
Manufacturer Scottish Aviation
Primary users Royal Air ForceMalaysia
Nepal
Number built 87
History
Introduction date 1956
First flight 25 June 1955
Retired 1972
Developed from Scottish Aviation Pioneer

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History Scottish Aviation Limited
Scottish Aviation Twin Pioneer
Introduction date 1956, First flight 25 June 1955



The Scottish Aviation Twin Pioneer was a British STOL transport aircraft built by Scottish Aviation Limited at Prestwick Airport, Scotland, during the 1950s. It was designed for both civil and military operators. It was conceived as a twin-engined version of the Pioneer light transport. Both aircraft required "an area only 30m (99ft) by 275m (902ft) in which to operate

Powered by two Alvis Leonides radial engines, the Twin Pioneer was a high-wing cabin monoplane with a triple fin and rudder assembly and fixed tailwheel undercarriage. The prototype Twin Pioneer, registered G-ANTP, first flew at Prestwick Airport on 25 June 1955. Flight trials demonstrated that the aircraft had a very short landing run and the aircraft was displayed at the September 1955 Society of British Aircraft Constructors Show at Farnborough.

Operational history

Scottish Aviation Twin Pioneer at Labuan
RAF Twin Pioneer CC.1 wearing sand camouflage in service in 1968.

The military version could carry external stores such as bombs under the stub wings. One aircraft became the first aircraft for the newly formed Royal Malaysian Air Force when it was delivered on 16 January 1962; the type served with the air force for 12 years.

The Royal Air Force ordered 39 aircraft, which were built between 1958 and 1959, deployed in Aden and the Far East. It was used extensively by British forces in the Malayan Emergency and the later confrontation in Borneo . In August 1959, No. 78 Squadron RAF at Khormaksar received some Twin Pioneers to supplement its single engine Pioneers. The Twin Pioneers were employed in moving troops and supplies around the wilderness and on occasions lending support to the Sultan of Oman . A series of double engine failures caused problems with the squadron losing two aircraft on the same day. Unsuitable soft and hard landing strips were also causes of failures during landings. 

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Scottish Aviation Limited

Scottish Aviation Limited
Scottish Aviation Twin Pioneer
Introduction date 1956, First flight 25 June 1955

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General characteristics

    • Crew: 2 (pilot and co-pilot)
    • Capacity: 16 passengers / 12 fully equipped troops / 10 paratroopers / 12 patient litters / 3,400 lb (1,542 kg) of air-droppable cargo
    • Length: 45 ft 3 in (13.79 m)
    • Wingspan: 76 ft 6 in (23.32 m)
    • Height: 12 ft 3 in (3.73 m)
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Powerplant

    • Empty weight: 9,600 lb (4,354 kg)
    • Gross weight: 14,000 lb (6,350 kg)
    • Max takeoff weight: (6,622 kg)
    • Powerplant: × Alvis Leonides 514/8 9-cylinder air-cooled radial piston engine, 540 hp (400 kW) for take-off
    520 hp (
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Specifications

    • Maximum speed: 165 mph (266 km/h, 143 kn) at (442 m) (Civil)
    • Maximum continuous cruise: 163 mph (262 km/h) at (1,036 m) (Civil)
    • Cruise speed: 119 mph (192 km/h, 103 kn) at 5,000 ft (1,524 m) (Civil)
    • Range: 791 mi (1,273 km, 687 nmi)
    • Service ceiling: (5,200 m) (Civil)
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Armament

  • Bombs: up to 2,000 lb (907 kg) of bombs, under undercarriage sponsons
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Although mainly used in military operations, the Twin Pioneer was also successful as a commercial transport for operation in areas without proper airfields, where unprepared surfaces were often the norm.

Scottish Aviation
Twin Pioneer

Other squadrons that operated the Twin Pioneers were No. 152 Squadron RAF based at Muharraq in Bahrain and No. 21 Squadron RAF,

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Early in its operational life in 1957 the Twin Pioneer suffered two fatal accidents due to fatigue failure which caused the outer panel of the wing to detach from the aircraft in flight.

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Aircrafttotal : Scottish Aviation Limited

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