Bell Helicopter Bell 204 (UH-1)
Photo ©: Robert Domandl (Photos at airliners.net)
Bell 204 (UH-1)
Medium Utility Helicopter
| Crew | 1 / 2 | |
| Passengers | 8 - 9 | |
| Propulsion | 1 Turboshaft Engine | |
| Engine Model | Lycoming T53-13B | |
| Engine Power | 1044 kW | 1400 shp |
| Speed | 204 km/h | 110 kts 127 mph |
| Service Ceiling | 5.750 m | 18.865 ft |
| Range | 370 km | 200 NM 230 mi. |
| Empty Weight | 2.177 kg | 4.800 lbs |
| max. Takeoff Weight | 3.856 kg | 8.501 lbs |
| Rotor Blades (main/tail) | 2/2 | 2/2 |
| Main Rotor Diameter | 14,63 m | 48,0 ft |
| Tail Rotor Diameter | 1,78 m | 5,8 ft |
| Rotor Disc Area | 168,1 m² | 1809 ft² |
| Length (Fuselage) | 12,31 m | 40,4 ft |
| Length | 16,15 m | 53,0 ft |
| Height | 3,77 m | 12,4 ft |
| First Flight | 22.10.1956 | |
| Production Status | out of production | |
| Production Range | 1961-1973 | |
| Total Production | ca. 2900 | |
| ICAO Code | UH1 | |
| Data for (Version) | Bell 204B-2 | |
| Weblinks | Extras |
| Bell Helicopter Textron |
| [Photo-ID: 2461] © Karsten Palt 2009-06-25 | |
![]() | Agusta-Bell AB204B / (I)UH-1 Royal Netherlands Navy / Koninklijke Marine (MLD) Reg.: 225 c/n: 3023 |
| Militaire Luchtvaart Museum [Soesterberg] | |


