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 | |
|---|---|---|---|---|
| 9380 | uh-1h | 1967 |  A2-380 | |
| 9381 | uh-1h | 1967 | A2-381 | |
| 9382 | uh-1h | 1967 |  67-17184 A2-382 | |
| 9383 | uh-1h | 1967 | A2-383 | |
| 9385 | uh-1h | 1967 | 67-17187 N37TV N37TV VH-OXE | |
| 9396 | uh-1h | 67-17198  VF-1809 | ||
| 9398 | uh-1d | 67-17200 N325SD | 200 | |
| 9406 | uh-1h | 67-17208 | ||
| 9409 | uh-1h | 67-17211 N7247L | ||
| 9432 | uh-1h |  H-79 | ||
| 9436 | uh-1h | 67-17238  ? N443ZB N443ZB | ||
| 9438 | uh-1h | 67-17240 | ||
| 9445 | uh-1h | CC-CBY | ||
| 9453 | uh-1h | 67-17255 | ||
| 9454 | uh-1h | 67-17256 | ||
| 9477 | uh-1h | 1967 | 67-17279 N443VA N80JG | |
| 9479 | uh-1h | 67-17281 | ||
| 9488 | uh-1h | 67-17290 N107CH | ||
| 9492 | uh-1h |  FAC4422 | ||
| 9494 | uh-1h | 67-17296  055 | ||
| 9495 | uh-1h | 67-17297 N97KP CC-CBL  A-15 | ||
| 9499 | uh-1h | FAC4415 | ||
| 9500 | uh-1h | 67-17302 N1218F N129RA N638HA | ||
| 9502 | uh-1h | 67-17304 N816SC N816SC  PR-FEC | ||
| 9505 | uh-1d | 1968 | 67-17307 A2-505  P2-404 | |
| 9507 | uh-1h | 67-17309 A2-507 | ||
| 9519 | uh-1h | 67-17321 N366SD | 321 | |
| 9521 | uh-1h | H-80 | ||
| 9522 | uh-1h | 1968 |  H-12 | |
| 9523 | uh-1h | 1968 | H-14 |