Neha Patil (Editor)

Schleicher ASW 19

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Top speed
  
250 km/h

Length
  
6.82 m

Retired
  
1986

Wingspan
  
15 m

Introduced
  
1975

First flight
  
November 23, 1975

Schleicher ASW 19 Alexander Schleicher ASW 19 Wikipdia

Manufacturer
  
Alexander Schleicher GmbH & Co

The ASW 19 is a single-seat glider built by Alexander Schleicher GmbH & Co. It was originally designed as a Standard Class glider, but now mainly competes in the Club Class. The ASW 19 is known for its pleasant handling and some clubs use it as a training glider. It was succeeded by the all-new Schleicher ASW 24.

Contents

Schleicher ASW 19 Schleicher ASW19 Untitled Aviation Photo 1418119 Airlinersnet

Design

Schleicher ASW 19 ASW 19

Schempp-Hirth metal air brakes are fitted on the upper surface of the wing, and later models received modified brakes with an additional panel due to the somewhat disappointing effectiveness. The wings are held in place with two main pins. Up to 80 kg of water ballast can be carried. The tail unit is also of glassfibre/foam sandwich, and the horizontal tailplane has a fixed stabilizer. The fibreglass fuselage is built without the honeycombs that were used on the ASW 15B and ASW 17. It has a winch hook, which is covered by the main wheel doors, and an aerotow hook situated approximately one foot from the nose.

Variants

Schleicher ASW 19 Schleicher ASW19 Untitled Aviation Photo 1418119 Airlinersnet

With the ASW 19B version, the maximum allowed amount of water ballast increased and the take-off weight can be raised to 454 kg. Later ASW 19B were delivered with an instrument panel that lifts with the canopy. This feature can be retrofitted to older models.

Schleicher ASW 19 Schleicher ASW19 Untitled Aviation Photo 1555203 Airlinersnet

The ASW 19 Club is a version with a fixed unsprung monowheel and no water ballast carried. Only five were built for the Royal Air Force, where they were known as the Valiant TX.1.

Schleicher ASW 19 Schleicher ASW19B D9997 Priv by Michel BROSSAUD Pictaero

A single ASW 19 was fitted with a new wing profile featuring turbulator blow holes at the Technical University of Delft. This ASW 19X showed improved gliding capabilities with a best glide ratio of about 1:41.

Operators

 United Kingdom
  • Royal Air Force
  •  France
  • 3 French Air Force ("F05" n°276, "F06" n°277,"F07" n°323)
  • Specifications

    General characteristics

    Schleicher ASW 19 httpsuploadwikimediaorgwikipediacommonsthu

  • Crew: One
  • Capacity: 80 kg (176 lb) water ballast
  • Length: 6.82 m (22 ft 5 in)
  • Wingspan: 15.00 m (49 ft 3 in)
  • Height: 1.42 m (4 ft 8 in)
  • Wing area: 11.0 m2 (118 ft2)
  • Aspect ratio: 20.45
  • Empty weight: 240 kg (529 lb)
  • Gross weight: 408 kg (899 lb)
  • Performance

  • Maximum speed: 250 km/h (160 mph)
  • Maximum glide ratio: 38.5
  • Rate of sink: 0.62 m/s (122 ft/min)
  • References

    Schleicher ASW 19 Wikipedia