Savoia-Marchetti S.71

__NOTOC__ Infobox Aircraft
name=Savoia-Marchetti S.71


caption=
type=Eight-passenger light transport
national origin=Italy
manufacturer=Savoia-Marchetti
designer=
first flight=1930
introduced=
retired=
status=
primary user=
more users=
produced=
number built=7
variants with their own articles=The Savoia-Marchetti S.71 was am Italian eight-passenger light transport designed and built by Savoia-Marchetti. The S.71 was a three-engined high-wing cantilever monoplane with a fixed tailwheel landing gear. It had a crew of four and room for eight passengers. The first four aircraft were powered by three 240hp (179kW) Walter Castor radial engines but the last three had 370hp (276kW) Piaggio P.VII engines.

pecifications (Castor-powered)

aerospecs
ref= [Oribis 1985, page 2894]
met or eng?= met

crew=4
capacity=8 passengers
length m=14
length ft=45
length in=11¼
span m=21.20
span ft=69
span in=6¾
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=4.10
height ft=13
height in=5½
wing area sqm=60
wing area sqft=645.86
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=2900
empty weight lb=6393
gross weight kg=4600
gross weight lb=10141
lift kg=
lift lb=

eng1 number=3
eng1 type=Walter Castor radial engine
eng1 kw= 179
eng1 hp= 240
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
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eng2 kw=
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max speed kmh=235
max speed mph=146
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1600
range miles=994
endurance h=
endurance min=
ceiling m=5250
ceiling ft=17,550
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=

aircontent
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References

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*cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=