Slingsby Tandem Tutor
| T.31B Tandem Tutor | |
|---|---|
 | |
| Cadet TX3 at the RAF Museum | |
| Role | Training glider |
| National origin | United Kingdom |
| Manufacturer | Slingsby Sailplanes Ltd |
| First flight | 1949 |
| Primary user | Royal Air Force |
| Number built | ca. 230 |
| Developed from | Slingsby Tutor |
The T.31 Tandem Tutor is a British military training glider, designed and built by Slingsby and used in large numbers by the Air Training Corps between 1951 and 1986.
Design and development
The T.31 was a tandem two-seat development of the T.8 Tutor (RAF Cadet TX.2). The fuselage was based on that of the T.29 Motor Tutor, increased in length and widened slightly; the wings and tail were unchanged. A single T.31A prototype was flown in 1949, followed by the production T.31B, with spoilers and a small additional wing bracing strut.
Operational history
Chief customer for the T.31B was the Royal Air Force for Air Cadet training; its aircraft were designated as Cadet TX Mark 3. As it was so similar to their existing single-seaters, it allowed easy conversion to solo. The RAF took delivery of 126 TX.3s between 1951 and 1959.
It also found a market with civilian clubs in the UK, although most of these were built from kits and spares, using existing Tutor wings. T.31s were exported to Burma, Ceylon, Israel, Jordan, Lebanon, Pakistan and Rhodesia. In addition, small numbers were built in Argentina, Israel and New Zealand.[1] The T.35 Austral was a one-off development with span increased to 15.64 m (51 ft 3¾ in),[2] sold to the Waikerie Gliding Club in Australia in 1952
After the RAF Cadet TX.3s were replaced by GRP gliders in the mid-1980s, the fleet was sold off, but never gained the same popularity with civilian owners as the side-by-side T.21, being a cheaper glider designed for "circuits and bumps", and only marginally soarable. Some were instead converted to simple ultra-light aircraft as Motor Cadets, with the front cockpit replaced by a Volkswagen or similar engine, and a three-point undercarriage.
Aircraft on display
Royal Air Force Museum, Hendon.
Operators
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Specifications (Slingsby T.31 Tandem Tutor)
Data from Coates, Andrew. “Jane's World Sailplanes & Motor Gliders new edition”. London, Jane's. 1980. ISBN 0-7106-0017-8
General characteristics
- Crew: 2
- Length: 7.1 m (23 ft 3½ in)
- Wingspan: 13.2 m (43 ft 3 ½ in)
- Wing area: 15.8 m2 (170.1 ft2)
- Aspect ratio: 11.1
- Wing profile: Göttingen 426
- Empty weight: 176 kg (388 lb)
- Gross weight: 376 kg (829 lb)
Performance
- Maximum speed: 130 km/h (80.8 mph)
- Stall speed: 61 km/h (38 mph)
- Maximum glide ratio: 18.5 @ 73km/h (41.6 mph)
- Rate of sink: 1.05 m/s (206.4 ft/min)
See also
- Related development
- Related lists
References
Citations
- ↑ T.31 Production list
- ↑ Ellison 1971, p. 202
- ↑ US Southwest Soaring Museum (2010). "Sailplanes, Hang Gliders & Motor Gliders". Retrieved 26 May 2011.
Cited sources
- Ellison, N.H. British Gliders and Sailplanes 1922-1970. A & C Black, 1971
- Coates, Andrew. “Jane's World Sailplanes & Motor Gliders new edition”. London, Jane's. 1980. ISBN 0-7106-0017-8
Other sources
- Simons, M. Slingsby Sailplanes. Airlife Publishing, 1996 - ISBN 1-85310-732-8
- Taylor, J. H. (ed) (1989) Jane's Encyclopedia of Aviation. Studio Editions: London. p. 29
- RAF Museum
External links
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