- Piper PA-7
__NOTOC__ Infobox Aircraft
name=PA-7 Skycoupe
caption=
type=Light aircraft
manufacturer=Piper Aircraft
designer=
first flight=1944
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The Piper PA-7 Skycoupe was a 1940s American two-seat light aircraft designed and built by
Piper Aircraft atLock Haven . Towards the end of1944 Piper announced a number of aircraft it intended to build after the war. One of these was the PWA-1 Skycoupe (Post War Airplane 1). A prototype was built in 1943, it was a two-seat side-by-side low-wing cantilever monoplane with a twin-boom fuselage with a tricycle landing gear. It had a Franklin 4ACG-199-H3 engine driving a pusher propeller. In 1945 it was redesignated the PA-7 Skycoupe but no further examples were built.pecifications (PA-7)
aerospecs
ref=
met or eng?= engcrew=2
capacity=
length m=
length ft=
length in=
span m=
span ft=30
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=
height in=
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=1597
lift kg=
lift lb=eng1 number=1
eng1 type=Franklin 4AC G-199-H3
eng1 kw=
eng1 hp= 113
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=max speed kmh=
max speed mph=110
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=
armament2=
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armament4=
armament5=
armament6=aircontent
see also=
related=
similar aircraft=
sequence=
lists=References
* Roger W. Peperell and Colin M.Smith, "Piper Aircraft and their forerunners", 1987, Air-Britain (Historians), ISBN 0 85130 149 5, Page 47 and 50.
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