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  Bell UH-1F "Iroquois"    
     
   
   
 
SPECIFICATIONS            Serial # :  65-7959
Rotor Diameter:  48 feet Cost:  $273,000
Length:  57 feet Max. Speed:  140 mph
Height:  14 feet, 11 inches Cruising Speed:  115 mph
Weight:  9,000 lbs. max. Range:  330 miles
Engines:  General Electric T58 of 1,070 shaft hp Service Ceiling:  24,830 feet
 
 
 
 
 
     
     
 

The UH-1 evolved from a 1955 Army competition for a new utility helicopter. The Army employed it in various roles including that of an armed escort or attack gunship in Vietnam. The USAF, USN, and USMC eventually adopted the model, as did Canada, and West Germany. The initial Army designation was the HU-1, which let to the common unofficial nickname of "Huey". It was redesignated in 1962 as the UH-1 under a tri-service agreement.

USAF orders for the Huey began in 1963 for the UH-1Fs, intended for support duties at missile sites, and for TH-1Fs for instrument and hoist training and medical evacuation. The HH-1H incorporated a longer fuselage and larger cabin for a crew of (2) and up to eleven passengers or six litters. The USAF ordered these in 1970 as a local base rescue helicopter to replace the HH-43 "Huskie". The first of the USAF's UH-1Ns, a twin-engine utility version capable of cruising on one engine, was obtained in 1970.

Warner Robins Air Logistics Center provides all logistics and program support for all UH-1s worldwide. Some versions continue to be in service today. The UH-1F on display was delivered to the USAF and the 319th Bombardment Wing (SAC) Grand Forks AFB, ND in May 1967. It served with various units until it was retired and flown to Robins AFB in October 1986.