- Bellanca 14-7
__NOTOC__ Infobox Aircraft
name=14-7
caption=Model 14-9
type=Civil utility aircraft
manufacturer=Bellanca
designer=
first flight=December 1937
introduced=
retired=
status=
primary user=
more users=
produced=
number built=ca. 50
variants with their own articles=The Bellanca 14-7 and its successors were a family of light aircraft manufactured in theUnited States shortly beforeWorld War II . Bellanca already had established itself in the market for aircraft in the 6-8 seat size, but now believed that it could also successfully sell smaller (3-4 seats) aircraft. The 14-7 was a modern, low-wingcantilever monoplane with afuselage intended to contribute lift to the design. Although the prototype flew with fixed tailwheel undercarriage, the 14-9 production version was the first US light aircraft to be mass-produced with retractable undercarriage - the main wheels rotated aft, up into wells in the wings.Development culminated in the 14-12 of 1941, at which point production ceased to allow Bellanca to work as a military subcontractor for the duration of the war when an attempt to market a militarised version as a trainer was unsuccessful. After the war, Bellanca returned to the design to create the
Bellanca 14-13 and its successors.Variants
* 14-7 - Prototype with fixed undercarriage and
LeBlond 5 E engine** 14-7L - 14-7 with
Lenape LM-5 engine14-9 - Main production version with retractable undercarriage and
Ken-Royce 5 F engine** 14-9L - with
Lenape Brave engine* 14-10L - with 100 hp (75 kW) Lycoming engine
* 14-12 - with Franklin 6AC engine
* T14-14 - militarised trainer version (single prototype only)
pecifications (14-9)
aerospecs
met or eng?= engcrew=one pilot
capacity=2 passengers
length m=10.42
length ft=34
length in=2
span m=6.48
span ft=21
span in=3
dia m=
dia ft=
dia in=
height m=
height ft=
height in=
wing area sqm=
wing area sqft=
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=
gross weight lb=eng1 number=1
eng1 type=Ken-Royce 5 Fradial engine
eng1 kw= 67
eng1 hp= 90
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=214
max speed mph=133
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=764
range miles=475
endurance h=
endurance min=
ceiling m=4,500
ceiling ft=14,750
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=armament1=
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armament6=References
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* [http://www.aerofiles.com/_bella.html aerofiles.com]ee also
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