Klemm Kl 31

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The Klemm Kl 31 was a touring aircraft developed in Germany in the early 1930s. It was a conventional, low-wing cantilever monoplane with four seats in an enclosed cabin. The fixed, tailskid undercarriage had divided main units. The fuselage was built from welded steel tube, while the wings were wooden. Some Kl 31s saw service with the Luftwaffe as training and liaison aircraft.

pecifications

aerospecs
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met or eng?= met

crew=1 pilot
capacity=3 passengers
length m=8.50
length ft=27
length in=11
span m=13.50
span ft=44
span in=4
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=2.30
height ft=7
height in=7
wing area sqm=20.8
wing area sqft=224
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
wing profile=
empty weight kg=690
empty weight lb=1,520
gross weight kg=1,250
gross weight lb=2,750
lift kg=
lift lb=

eng1 number=1
eng1 type=Bramo Sh 14a
eng1 kw= 120
eng1 hp= 160
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
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max speed kmh=190
max speed mph=120
max speed mach=
cruise speed kmh=
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stall speed kmh=
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range km=735
range miles=460
endurance h=
endurance min=
ceiling m=3,800
ceiling ft=12,500
g limits=
roll rate=
glide ratio=
climb rate ms=2.3
climb rate ftmin=460
sink rate ms=
sink rate ftmin=

armament1=
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armament6= aircontent
see also=
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References

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