Schleicher ASK 16

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The ASK 16 was designed by Rudolf Kaiser for production by Alexander Schleicher GmbH & Co of Furth, Germany. The aircraft is of welded tube, wood and fabric construction and has a low-set high-aspect-ratio wing.

Seating is side-by-side for two persons under a fully transparent side-hinged canopy. The standard powerplant is a 72 h.p. Limbach Volksvagen 1700 driving a Hoffman variable-pitch propeller.[1]

The ASK 16 has a retractable tail-wheel undercarriage with the main units mounted under the wings and retracting inwards. It is fitted with dual controls to permit use in the primary training role.[2]

Production and operation

The prototype first flew on 2 February 1971. 44 aircraft were built for operation by clubs and private owners.[3] Most of the completed aircraft remained in active service in 2005, including examples flying in Germany, Ireland, Italy, Switzerland, and the United Kingdom.

Specifications

Scleicher AS-K16 showing arrangement of underwing retractable undercarriage and side-hinged canopy

Data from Simpson, 2001, p. 488

General characteristics

  • Crew: two
  • Payload: 105 kg (230 lb)
  • Length: 7.34 m (24 ft 1 in)
  • Wingspan: 16.01 m (52 ft 6 in)
  • Height: 2.08 m (6 ft 10 in)
  • Wing area: 16.0 m²[4] (205 ft²)
  • Empty weight: 213 kg (470 lb)
  • Max. takeoff weight: 318 kg (700 lb)
  • Powerplant: 1 × Limbach SL.1700.EBI piston engine, 54 kW (72 hp)

Performance

  • Maximum speed: 200 km/h (108 knots, 124 mph)
  • Cruise speed: 171 km/h (92 knots, 106 mph)
  • Range: 330 km (178 nmi, 205 mi)
  • Rate of climb: 2.5 m/s (492 ft/m)

References

Notes
  1. Simpson, 2001, p. 488
  2. Simpson, 2001, p. 487
  3. Simpson, 2001, p. 487
  4. Taylor,1971, p.504.
Bibliography
  • Simpson, Rod (2001). Airlife's World Aircraft. Airlife Publishing Ltd. ISBN 1-84037-115-3. 
  • Taylor, J.W.R. (ed.) (1971). Jane's All The World's Aircraft 1971-72. London: Sampson Low. ISBN 0-354-00094-2. 
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