Slingsby Falke

Source: Wikipedia, the free encyclopedia.

T.61 Falke
T61F Venture T2
Role Basic Trainer
National origin United Kingdom
Manufacturer Slingsby Sailplanes
First flight 1971
Primary user Royal Air Force
Number built 76
Developed from
Scheibe SF 25B

The Slingsby Type 61 Falke was a licence-built version of the

Scheibe SF 25B Motor glider built by Slingsby Sailplanes. It entered service with the Royal Air Force
for air cadet training as the Slingsby Venture.

Development

In 1970 Slingsby acquired a licence to build the SF 25B as the Type 61A Falke, a side-by-side two-seat dual training monoplane. This first variant was powered by a 45 hp

Volunteer Gliding Schools for basic air cadet training. Following replacement by the Grob Vigilant T1
they were all sold in 1990.

Variants

T61A
Production variant fitted with a Starck Stamo MS1500 engine with manual engine start, 26 built.
T61B
As T61A but fitted with a Franklin 2A-120-A engine, one built.
T61C
Production variant fitted with a Starck Stamo MS1500 engine with an electric engine start, 8 built.
T61D
One T61A refitted with Rollason R.S.1 engine in 1972.
T61E
Production aircraft for the RAF as Venture T2, 15 built later modified to T61F.
T61F
Production aircraft for the RAF with electric engine starter as the Venture T2, 15 T61Es modified and 25 built.
T61G
One aircraft powered by a
Limbach SL1700
engine.
Venture T1
RAF designation for one T61A bought for evaluation in 1971.
Venture T2
RAF designation for production T61E and later T61F aircraft.

Former operators

 United Kingdom

RAF VGS 612 ZA652, ZA653, ZA654

RAF VGS 616 ZA625, ZA630

RAF VGS 642 XZ550 August 1978, XZ563 October 1978, ZA630 March 1980, ZA657, ZA659 replaced XZ653

RAF VGS 644 ZA634 29 March 1980.

Specifications (T61A)

T61F Venture T2

General characteristics

  • Crew: Two
  • Length: 24 ft 11 in (7.6 m)
  • Wingspan: 50 ft 4 in (15.33 m)
  • Wing area: 188 sq ft (17.47 m2)
  • Aspect ratio: 13.4
  • Empty weight: 740 lb (335 kg)
  • Gross weight: 1,170 lb (530 kg)
  • Powerplant: 1 × Starck Stamo MS1500 , 45 hp (34 kW)

Performance

  • Maximum glide ratio: 22
  • Rate of sink: 200 ft/min (1.00 m/s)

See also

Related lists

References

  1. ^ "Royal Air Force Charitable Trust Enterprises – RAF Slingsby Venture".
  • Jackson, A.J. (1974). British Civil Aircraft since 1919 Volume 3. London: Putnam. .