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 | |
|---|---|---|---|---|
| 10782 | uh-1h |  68-16123 | ||
| 10783 | uh-1h | 68-16124 | ||
| 10784 | uh-1h | 68-16125 | ||
| 10785 | uh-1h | 68-16126 | ||
| 10786 | uh-1h | 68-16127 | ||
| 10787 | uh-1h | 68-16128 | ||
| 10788 | uh-1h | 68-16129 | ||
| 10789 | uh-1h | 68-16130 | ||
| 10790 | uh-1h | 68-16131 | ||
| 10791 | uh-1h | 68-16132 | ||
| 10792 | uh-1h | 68-16133 | ||
| 10803 | uh-1h | 68-16144 N16144  AE-464 | ||
| 10804 | uh-1h |  PNP-332  PNC-0739 | ||
| 10810 | uh-1h | 68-16151  CC-CBW | ||
| 10811 | uh-1h | 68-16152 PNC-0733 | ||
| 10815 | uh-1h | 68-16156  L-1102 | L-1102 | |
| 10827 | uh-1h |  H6-16/12 | ||
| 10828 | uh-1h | H6-17/12 | ||
| 10830 | uh-1h |  ES821 | ||
| 10838 | uh-1h | 68-16179 | ||
| 10848 | uh-1h | 68-16189 68-16189 | ||
| 10850 | uh-1h | 68-16191  YI-214 | ||
| 10856 | uh-1h | 68-16197 N10432 | ||
| 10874 | uh-1h | 68-16215 | ||
| 10883 | uh-1h | AE-435 | ||
| 10920 | uh-1h | 68-16261 N443YB | ||
| 10923 | uh-1h | 68-16264 N342SD | ||
| 10924 | uh-1h | 68-16265 | ||
| 10927 | uh-1h | H6-20/12 | ||
| 10930 | uh-1h | 68-16271 N464NA |