Huff-Daland LB-1

Infobox Aircraft
name=Huff-Daland LB-1


caption=
type=Single engine biplane bomber
manufacturer=Huff-Daland
designer=
first flight=1923
introduced=1923
retired=
status=
primary user=United States Army Air Service
more users=
produced=
number built=10
variants with their own articles=

The Huff-Daland LB-1 was an American biplane light bomber aircraft operated by the United States Army Air Service in the 1920s.

Derived from the XLB-1 prototype bought by the Army in 1923, the LB-1 development aircraft was powered by a single Packard 2A-2540 engine and carried an extra crewman. It proved underpowered in service trials, and was replaced by the twin-engined XLB-3.

pecifications

aerospecs
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met or eng?= eng

crew=Four
capacity=
length m=14.07
length ft=46
length in=2
span m=20.27
span ft=60
span in=6
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swept ft=
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volume m3=
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aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=5,631
gross weight lb=12,415
lift kg=
lift lb=

eng1 number=1
eng1 type=Packard 2A-2540 water-cooled vee engine
eng1 kw=600
eng1 hp= 800
eng1 kn=
eng1 lbf=
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eng1 lbf-ab=
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max speed kmh=190
max speed mph=120
max speed mach=
cruise speed kmh=
cruise speed mph=
range km= 700
range miles=430
endurance h=
endurance min=
ceiling m=3,400
ceiling ft=11,150
glide ratio=
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climb rate ftmin=
sink rate ms=
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armament1=5 × .30 machine guns
armament2=2,750 lb (1,250 kg) of bombs
armament3=
armament4=
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armament6=

aircontent
see also=
related=
similar aircraft=
sequence=
lists=
*List of military aircraft of the United States

References

Notes

Bibliography

* Donald, David, ed. "Encyclopedia of World Aircraft". Etobicoke, ON: Prospero Books, 1997. ISBN 1-85605-375-X.
* [http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=2400 USAF Museum fact sheet]