BELL 204/205 Civil Aircraft Model Details

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General Information of BELL 204/205

Developed From : Bell UH-1 Iroquois

First Flight : 20750

Introduction : 1959

Manufacturer : Bell Helicopter

Produced : 1956-1980s

Role : Multipurpose utility helicopter

Status : Production completed

Variants : Bell 212; Bell 214

General characteristics of BELL 204/205

Capacity : 3,000 lb (1,360 kg) including up to eight-nine passengers, or equivalent cargo

Crew : one-two

Disc Area : 1,808 ft² (168.0 m²)

Empty Weight : 4,600 lb (2,085 kg)

Height : 14 ft 7 in (4.5 m)

Length : 41 ft 8 in (12.69 m)

Loaded_Weight : lb (kg)

Max Takeoff Weight : 9,500 lb (4,310 kg)

Powerplant : 1 × Lycoming T53-L-11A turboshaft, 1,100 shp (820 kW)

Rotor Diameter : 48 ft 0 in (14.63 m)

Useful Load : lb (kg)

Performance of BELL 204/205

Cruise Speed : 111 knots (125 mph, 205 km/h)

Maximum Speed : 120 knots (135 mph, 220 km/h)

Never Exceed Speed : knots (mph, km/h)

Power/Mass : hp/lb (W/kg)

Range : 300 nm (mi, 533 km)

Rate Of Climb : 1,755 ft/min (8.9 m/s)

Service Ceiling : 19,390 ft (5,910 m)

Stall Speed : knots (mph, km/h)

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