Pasped Skylark: Difference between revisions

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{{Short description|American aircraft}}
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{|{{Infobox Aircraft Begin
{|{{Infobox Aircraft Begin
| name=Pasped Skylark
| name=Pasped Skylark
| image=
| image=PaspedW1Skylark.jpg
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==Design and development==
==Design and development==
The Skylark is a braced low-wing monoplane with a fixed [[Conventional landing gear|tailwheel landing gear]].<ref name="orbis" /> It is powered by a {{convert|125|hp|kW|0|abbr=on}} [[Warner Scarab]] radial engine.<ref name="orbis" /> The enclosed cockpit has side-by-side seating for two.<ref name="orbis" /> It has a welded steel fuselage and wooden wings.<ref name="orbis" /> With other two-seat aircraft of the era having a better performance on smaller engines the Skylark did not enter production.<ref name="orbis" /> The sole example was currently airworthy in February 2010 with an owner in [[Versailles, Missouri]].
The Skylark is a braced low-wing monoplane with a fixed [[Conventional landing gear|tailwheel landing gear]].<ref name="orbis" /> It is powered by a {{convert|125|hp|kW|0|abbr=on}} [[Warner Scarab]] radial engine.<ref name="orbis" /> The enclosed cockpit has side-by-side seating for two.<ref name="orbis" /> It has a welded steel fuselage and wooden wings.<ref name="orbis" /> With other two-seat aircraft of the era having a better performance on smaller engines the Skylark did not enter production.<ref name="orbis" /> The sole example was currently airworthy in February 2010 with an owner in [[Versailles, Missouri]].

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==Specifications==
==Specifications==
{{Aircraft specs
{{Aircraft specs
|ref=<ref name="aerofile" /> and Green (1956)
|ref=<ref name="aerofile" /> and <ref name="Green">{{cite book|last=Green|first=William|title=The Aircraft of the World|year=1956|publisher=Macdonald & Co (Publishers) Ltd|isbn=<!--none-->}}</ref>
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|sink rate note=
|sink rate note=
|lift to drag=
|lift to drag=
|wing loading kg/m2
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading lb/sqft=
|wing loading note=
|wing loading note=
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==References==
==References==
{{commons category|Pasped Skylark}}

===Notes===
===Notes===
{{reflist|refs=
{{reflist|refs=
<ref name="orbis">Orbis 1985, p. 2693</ref>
<ref name="orbis">Orbis 1985, p. 2693</ref>
<ref name="aerofile">{{cite web | title=American airplanes - Pa - Pi | url=http://aerofiles.com/_pa.html| publisher=www.aerofiles.com |date=2 May 2009 |accessdate=2010-02-18}}</ref>
<ref name="aerofile">{{cite web | title=American airplanes - Pa - Pi | url=http://aerofiles.com/_pa.html| publisher=www.aerofiles.com |date=2 May 2009 |access-date=2010-02-18}}</ref>
}}
}}

===Bibliography===
===Bibliography===
{{refbegin}}
{{refbegin}}
* {{cite book|last=Green|first=William|title=The Aircraft of the World|year=1956|publisher=Macdonald & Co (Publishers) Ltd|isbn=none}}
*{{cite book |title= The [[Illustrated Encyclopedia of Aircraft]] (Part Work 1982-1985)|publisher= Orbis Publishing}}
*{{cite book |last= |first= |authorlink= |coauthors= |title= The [[Illustrated Encyclopedia of Aircraft]] (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=}}
{{refend}}
{{refend}}
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{{aviation lists}}
[[Category:United States civil utility aircraft 1920-1929]]
[[Category:1930s United States civil utility aircraft]]
[[Category:Low-wing aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:Aircraft first flown in 1935]]

Latest revision as of 13:45, 14 May 2023

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

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]

Design and development[edit]

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[edit]

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[edit]

Notes[edit]

  1. ^ a b c d e f 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[edit]