Hannover CL.V

__NOTOC__ Infobox Aircraft
name=CL.V, F.6, FF.7 "Hauk"


caption=
type=Attack aircraft
national origin=Germany
manufacturer=Hannover, Kjeller
designer=
first flight=avyear|1918
introduced=
retired=
status=
primary user="Luftstreitkräfte"
more users=Norwegian army air service
produced=
number built=ca 120
variants with their own articles=The Hannover CL.V was a ground attack aircraft built in Germany during World War I, which formed the basis for a sport aircraft following the war. Derived from the Hannover CL.II, the CL.V shared the same basic conventional biplane configuration and incorporated the overhanging, aerodynamically-balanced ailerons developed for the Hannover CL.III. The characteristic biplane tail used on earlier Hannover CL-class machines was dispensed with, and a conventional empennage was fitted to the prototype, although production machines reverted to the earlier design. The "Idflieg" placed an order for 100 aircraft, but only 46 of these were built before the end of the war, and none of them had been put into service by that time. Hannover built another 62 examples after the Armistice,

In its civil configuration, designated F.6, the aircraft dispensed entirely with the rear cockpit, and once again used the monoplane tail unit that had been fitted to the CL.V prototype.

In 1923, another 14 CL.Vs were produced for the Norwegian army air service by Kjeller. These were known as the Kjeller FF.7 "Hauk" ("Hawk") and remained in service until 1929.

pecifications (CL.V)

aerospecs
ref=
met or eng?= met

crew=Two, pilot and gunner
capacity=
length m=7.00
length ft=23
length in=0
span m=10.56
span ft=34
span in=8
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=2.84
height ft=9
height in=3
wing area sqm=28.5
wing area sqft=307
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=720
empty weight lb=1,587
gross weight kg=1,080
gross weight lb=2,380
lift kg=
lift lb=

eng1 number=1
eng1 type=BMW IIIa
eng1 kw= 138
eng1 hp= 185
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=
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max speed kmh=185
max speed mph=115
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h= 3
endurance min=
ceiling m=9,000
ceiling ft=29,530
glide ratio=
climb rate ms=5.0
climb rate ftmin=990
sink rate ms=
sink rate ftmin=

armament1=2 × fixed, forward-firing 7.92 mm MG08 machine guns
armament2=1 × trainable, rearward-firing 7.92 mm Parabellum MG14 machine gun
armament3=
armament4=
armament5=
armament6= aircontent
see also=
related=
similar aircraft=
lists=

References

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