Pasped Skylark

The Pasped W-1 Skylark is a 1930s American two-seat single-engined cabin monoplane designed and built by the Pasped Aircraft Company of Glendale, California.[1]

Pasped Skylark
Role Two-seat cabin monoplane
National origin United States
Manufacturer Pasped Aircraft Company
First flight 1935
Status airworthy in 2010
Primary user private pilot owner
Number built 1

Design and development

The Skylark is a braced low-wing monoplane with a fixed tailwheel landing gear.[1] It is powered by a 125 hp (93 kW) Warner Scarab radial engine.[1] The enclosed cockpit has side-by-side seating for two.[1] It has a welded steel fuselage and wooden wings.[1] With other two-seat aircraft of the era having a better performance on smaller engines the Skylark did not enter production.[1] The sole example was currently airworthy in February 2010 with an owner in Versailles, Missouri.

Specifications

Data from [2] and [3]

General characteristics

  • Crew: 2
  • Length: 25 ft 0 in (7.62 m)
  • Wingspan: 35 ft 11 in (10.95 m)
  • Height: 7 ft 11 in (2.41 m)
  • Wing area: 187 sq ft (17.4 m2)
  • Empty weight: 1,288 lb (584 kg)
  • Max takeoff weight: 1,885 lb (855 kg)
  • Powerplant: 1 × Warner Scarab radial engine, 125 hp (93 kW)

Performance

  • Maximum speed: 139 mph (224 km/h, 121 kn)
  • Cruise speed: 125 mph (201 km/h, 109 kn)
  • Minimum control speed: 35 mph (56 km/h, 30 kn)
  • Range: 475 mi (764 km, 413 nmi)
  • Service ceiling: 16,000 ft (4,900 m)
  • Rate of climb: 850 ft/min (4.3 m/s)

References
Wikimedia Commons has media related to Pasped Skylark.

Notes
  1. Orbis 1985, p. 2693
  2. "American airplanes - Pa - Pi". www.aerofiles.com. 2 May 2009. Retrieved 2010-02-18.
  3. Green, William (1956). The Aircraft of the World. Macdonald & Co (Publishers) Ltd.

Bibliography
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