BELL 206 Civil Aircraft Model Details

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General Information of BELL 206

Developed From : Bell YOH-4

Developed Into : Bell 407

First Flight : December 8, 1962 (206)[1]; 10 January 1966 (206A)[2]

Introduction : 1967

Manufacturer : Bell Helicopter Textron

National Origin : Canada

Number Built : 7,300[3]

Produced : 1962-2010

Role : Multipurpose Utility helicopter

Status : In service

Unit_Cost : approx. US$900,000 to $1.2 million[3]

Variants : OH-58 Kiowa; Panha Shabaviz 2061

General characteristics of BELL 206

Capacity : four passengers

Crew : one pilot

Disc Area : 872 ft² (81.1 m²)

Empty Weight : 2,331 lb (1,057 kg)

Height : 9 ft 4 in (2.83 m)

Length : 39 ft 8 in (12.11 m)

Max Takeoff Weight : 3,200 lb (1,451 kg)

Powerplant : 1 × Allison 250-C30P turboshaft, 420 shp; derated to 317 shp due to drivetrain limitations (310 kW)

Rotor Diameter : 33 ft 4 in (10.16 m)

Performance of BELL 206

Maximum Speed : 120 knots (222 km/h, 138 mph)

Never Exceed Speed : 130 knots (241 km/h, 150 mph)

Power/Mass : 0.26 hp/lb (427.48784 W/kg)

Range : 374 nmi (430 mi, 693 km)

Rate Of Climb : 1,350 ft/min (6.9 m/s)

Service Ceiling : 13,500 ft (4,115 m)

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