- Pilatus P-4
__NOTOC__ Infobox Aircraft
name=Pilatus P-4
caption=
type=Five-seat cabin monoplane
national origin=Switzerland
manufacturer=Pilatus
designer=
first flight=1948
introduced=
retired=1957
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The Pilatus P-4 was a Swiss five-seat cabin monoplane designed and built byPilatus but had little sales success.Design and development
The P-4 was a high-wing braced monoplane with a fixed tailwheel landing gear and a braced tail unit. It was powered by a nose-mounted 190hp (142kW)
Lycoming O-435 engine and an enclosed cabin for the pilot and four passengers. The seats could be removed to accommodate cargo or two stretchers formedevac transport. The aircraft (Registered "HB-AET") first flew on the22 March 1948 but did not enter series production due to the company's other production commitments. The P-4 crashed and was destroyed on the13 October 1957 .pecifications (P-4)
aerospecs
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met or eng?= metcrew=1
capacity=4
length m=
length ft=
length in=
span m=11.85
span ft=38
span in=10½
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volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=1500
gross weight lb=3307
lift kg=
lift lb=eng1 number=1
eng1 type=Lycoming O-435
eng1 kw= 142
eng1 hp= 190
eng1 kn=
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eng2 number=
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eng2 lbf-ab=max speed kmh=245
max speed mph=152
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lists=References
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*cite book |last= |first= |authorlink= |coauthors= |title= TheIllustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=
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