Piper PA-8

Piper PA-8

__NOTOC__ Infobox Aircraft
name=PA-8 Skycycle


caption=
type=Light aircraft
manufacturer=Piper Aircraft
designer=
first flight=1945
introduced=
retired=
status=
primary user=
more users=
produced=
number built=2
variants with their own articles=

The Piper PA-8 Skycycle was a 1940s American single-seat light aircraft designed and built by Piper Aircraft at Lock Haven. Towards the end of 1944 Piper announced a number of aircraft it intended to build after the war. One of these was the PWA-8 (Post War Airplane 8). An aerodynamic test aircraft was built with the name Cub Cycle and it first flew on 27 August 1944 with a small two cylinder Franklin engine. The Franklin engine was replaced by a 37hp Continental A-40-3 and the aircraft first flew with the Continental engine on 12 September 1944. The Skycycle was a fabric-covered mid-wing single-engined single-seat monoplane with a tailwheel landing gear. The fuselage was produced using a belly fuel tank as used on the F4U Corsair. The Cub Cycle was scrapped and a similar but new aircraft was built with the name Skycycle. The Skycycle first flew on 29 January 1945 using the same Continental engine as the Cub Cycle. The aircraft was further modified in 1945 with a 55hp Lycoming O-145-A2 engine and designated the PA-8 Skycycle. No further examples were built.

pecifications (PA-8)

aerospecs
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met or eng?= eng

crew=1
capacity=
length m=
length ft=15
length in=8
span m=
span ft=20
span in=0
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=
height ft=5
height in=0
wing area sqm=
wing area sqft=
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=
gross weight lb=630
lift kg=
lift lb=

eng1 number=1
eng1 type=Lycoming O-145-2
eng1 kw=
eng1 hp= 55
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
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eng2 lbf-ab=

max speed kmh=
max speed mph=120
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=400
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
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References

* Roger W. Peperell and Colin M.Smith, "Piper Aircraft and their forerunners", 1987, Air-Britain (Historians), ISBN 0 85130 149 5, Page 51 and 53.


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