The Bell Huey was the first mass-produced helicopter powered by a jet turbine. With its distinctive whomp-whomp sound that could be heard miles away, the UH/AH-1 aircraft have totaled more than 27 million flight hours since Oct. 20, 1956 when the granddaddy of all H-1's, the XH-40, made its first flight. Since then, more than 16,000 H-1 helicopters have been produced by Bell and its licensees -- making it the most successful military aircraft in aviation history
The Model 205 ( military version known as UH-1H ), compared to the 204, has a longer fuselage and a more powerful engine that gives better overall performance.
The Model 205 ( military version known as UH-1H ), compared to the 204, has a longer fuselage and a more powerful engine that gives better overall performance.
Derivatives & Versions
| 205A | ||
| 205A-1 | ||
| CH-118 Iroquois | ||
| HH-1H Iroquois | USAF variant of the UH-1H for SAR and general support duties. | |
| UH-1D Iroquois | ||
| UH-1H Iroquois | ||
| UH-1V Iroquois | Conversions to MEDEVAC role from UH-1H, by US Army Electronics Command. | |
| → AB205 | 1966 | |
| → UH-1D | 1967 | UH-1H for Germany (D was for Deutschland). |
| → 212 | 1968 | The Bell 212 Twin Two-Twelve is a two-bladed, twin-engined, medium helicopter developed from the Bell 205 ( Huey ) powered by a, then revolutionary, Pratt & Whitney Canada Twin-Pac engine made up of two coupled PT6 power turbines driving a common gearbox. |
| → 214 | 1970 | The 214A/C Huey Plus was a development of the Bell 205 originally designed for Iran which received more than 300 aircraft of this type. |
| → UH-1H | 1970 | Fuji licensed-built Bell 205B (UH-1H) with uprated Ichihara licensed-built Lycoming T-58 engine. |
| → 210 | 2004 | The Bell 210 is a refurbished UH-1H Huey (Bell 205) fuselage fitted with Bell 212 components: main rotor hub and blades, tail rotor, main and tail rotor support structure, transmission, rotating controls, and tail boom. |
| HUEY II | 2005 | Following the Bell 210 experience, the Bell Huey II upgrade kit combines commercial Bell 212 dynamic components with the reliable Honeywell T53-L-703 engine, leading to an increase in hover performance in hot conditions with an increase of the max gross weight to 10,500 lbs while lowering direct operating costs. |
| TH-1H Iroquois | 2006 | Basic trainer for the USAF based on the HUEY II. |
Airframes (1877)
| C/N | Model | Built | Reg | |
|---|---|---|---|---|
| 5086 | uh-1d |  65-10042 | ||
| 5087 | uh-1d | 65-10043 | ||
| 5088 | uh-1d | 65-10044 | ||
| 5089 | uh-1d | 65-10045 | ||
| 5090 | uh-1d | 65-10046 | ||
| 5091 | uh-1d | 65-10047 | ||
| 5092 | uh-1d | 65-10048 | ||
| 5093 | uh-1d | 65-10049 | ||
| 5094 | uh-1d | 1965 | 65-10050 N615BV  ZS-HHG | |
| 5095 | uh-1d | 65-10051 | ||
| 5096 | uh-1d | 65-10052 | ||
| 5097 | uh-1d | 65-10053 | ||
| 5098 | uh-1d | 65-10054 65-10054 | ||
| 5099 | uh-1d | 65-10055 | ||
| 5100 | uh-1d | 65-10056 | ||
| 5101 | uh-1d | 65-10057 | ||
| 5102 | uh-1d | 65-10058 | ||
| 5103 | uh-1d | 65-10059 | ||
| 5104 | uh-1d | 65-10060 N343WN | ||
| 5105 | uh-1d | 65-10061 N22SD N911KP | 3 | |
| 5106 | uh-1d | 65-10062 | ||
| 5107 | uh-1d | 65-10063 | ||
| 5108 | uh-1d | 65-10064 | ||
| 5109 | uh-1d | 65-10065 | ||
| 5110 | uh-1d | 65-10066 | ||
| 5111 | uh-1d | 65-10067 N775AR | ||
| 5112 | uh-1d | 65-10068 | ||
| 5113 | uh-1d | 65-10069 | ||
| 5114 | uh-1d | 65-10070 | ||
| 5115 | uh-1d |  AE-442 |