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Home Helicopter Profiles Bell Bell Cobra AH-1F

Bell Cobra AH-1F

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General Data
First Flown:
1965
Length:
53 ft 1 in
Lift Capability:
n/a
Height:
13 ft 5 in
Range:
315 miles
Rotor Span:
44 ft
Top Speed:
141 mph
Empty Weight:
6,598 lb
Service Ceiling:
12,200 ft
Max Gross Weight:
at take off 10,000 lb
Engines:
1 Textron Lycoming T53-L-703 turoshaft rated at 1,800 shp
Armament:
TOW missiles, free flight rockets, 20 mm cannon in nose, 30 mm grenade launcher in nose
Accommodations:
1 Pilot and 1 gunner Cargo: n/a
Operators:
Bahrain, Israel, Japan, Jordan, Pakistan, South Korea, Thailand, Turkey, United Nations

Similar Aircraft:
Super Cobra
Other Features:


Notes
No longer in production
Three versions are shown in our image gallery. One (with the nose cannon and grenade launcher) was an original issue AH-1G that fought in Vietnam, the one with a three barrel cannon was a trainer and never saw combat. The third one shown has a 6 barrel cannon and is privately owned, no history of it is known.

Last Updated on Thursday, 18 March 2010 12:24  

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