Aerosport Scamp

{{Infobox aircraft

|name=Aerosport Scamp

|image=Aerosport_Scamp.jpg

|caption=

|type=Sport aircraft

|national_origin=United States

|manufacturer=Homebuilt

|designer=Harris Woods

|first_flight=August 21, 1973

|introduction=

|retired=

|status=

|primary_user=

|number_built=

|developed_from=

|variants=

}}

__NOTOC__

The Aerosport Scamp A is a small biplane designed for home building by Harris Woods. It featured an open cabin, tricycle undercarriage, and a T-tail.

The Scamp A first flew on August 21 1973,{{cite book|editor-last1 = Taylor| editor-first1 = JWR | title = Jane's All the World's Aircraft, 1988–1989 | year = 1988| publisher = Jane's Information Group| isbn =0-7106-0867-5|pages= 554–555 }} powered by an 1853 cc Volkswagen car engine. 1,050 sets of plans had sold by 1993. In addition to the many examples which have been completed in the United States, several examples of the type are active in the United Kingdom.

The Agrocopteros Scamp B is an agricultural crop spraying version of the Scamp, modified from kits assembled in Colombia.{{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages= 39}}

Specifications (Scamp A)

{{Aircraft specs

|ref=Jane's All the World's Aircraft, 1988–1989

|prime units?=kts

|crew=1

|length ft=14

|length in=0

|length note=

|span ft=17

|span in=6

|span note=

|height ft=5

|height in=6.5

|height note=

|wing area sqft=105

|wing area note=

|aspect ratio=

|airfoil=NACA 23012{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |access-date=16 April 2019}}

|empty weight lb=520-550

|empty weight note=

|gross weight lb=

|gross weight note=

|max takeoff weight lb=768-798

|max takeoff weight note=

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=VW

|eng1 type=4-cylinder air-cooled horizontally-opposed piston engine

|eng1 hp=60

|eng1 note=a modified Volkswagen automotive engine

|prop blade number=2

|prop name=fixed-pitch propeller

|prop dia ft=4

|prop dia in=8

|prop dia note=

|max speed kts=91

|max speed note=

|cruise speed kts=78

|cruise speed note=

|stall speed kts=39

|stall speed note=

|never exceed speed kts=

|never exceed speed note=

|range nmi=108

|range note=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling ft=12000

|ceiling note=

|g limits=+6 -3

|climb rate ftmin=

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading lb/sqft=

|wing loading note=

|fuel consumption lb/mi=

|power/mass=

|more performance=

  • Take-off run: {{cvt|400|ft|0}}
  • Landing run: {{cvt|400|ft|0}}

}}

See also

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References

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