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Bell Helicopter Bell 205 (UH-1)

Bell 205 UH-1D © Karsten Palt
Photo ©: Karsten Palt

Bell 205 (UH-1)

Medium Utility Helicopter

Crew1 / 2
Passengers8 - 9
 
Propulsion1 Turboshaft Engine
Engine ModelLycoming T53-L-13
Engine Power1044 kW1400 shp
 
Speed204 km/h110 kts
  127 mph
Service Ceiling3.840 m12.600 ft
Range556 km300 NM
345 mi.
 
Empty Weight2.363 kg5.210 lbs
max. Takeoff Weight4.309 kg9.500 lbs
 
Rotor Blades (main/tail)2/22/2
Main Rotor Diameter14,63 m48,0 ft
Tail Rotor Diameter2,59 m8,5 ft
Rotor Disc Area168,1 m²1809 ft²
Length (Fuselage)12,65 m41,5 ft
Length17,62 m57,8 ft
Height4,43 m14,5 ft
 
First Flight16.08.1961
Production Statusout of production
Total Production>10000
Developed fromBell 204
 
ICAO CodeUH1
FAA TCDSH1SW
Data for (Version)Bell 205 UH-1H

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