1976 Bell 206B
JetRanger II

SPECIFICATIONS

Date of Manufacture: 1976
Total Airframe Hours: 7,905

Optional Equipment

Dual Controls High Skids with Flitestep
Range Extender Rotor Brake
Wedge Windows (front & rear) Sloping Avionics Panel
High Intensity Strobe Door Openers
Floor Protectors .

Avionics

EHSI Nav System Sandel SH 3308
VHF Comm 1 Bendix King KY 196A
VHF Comm 2 Bendix King KY 196A
Nav System Bendix King KNS 80
Digital Transponder (with Mode C) Garmin GTX327
GPS Colour Multifunction Display Bendix King KMD 150
Radar Altimeter Bendix King
Audio Panel LED Illuminated Garmin GMA 340
Chronometer Astro LC2

Exterior
Base metallic black/silver. Green/red/blue metallic stripes.

Interior
Grey leather seats and doors. Grey headlining in suede/leather. Dark blue (grey piping) carpet.

Details believed to be correct but subject to verification by inspection.

Component Status
(as at 7,870 airframe hours)

Item Life Hrs - Retirement Hrs - Overhaul
Main Rotor Blades (x2) 5,000 1,945 -
Main Rotor Hub Assembly 1,200 - 489
Main Rotor Grips (x2) 4,800 4,089 (x2) -
Main Rotor Mast Assembly 3,000 - 2,900
Main Rotor Trunnion 2,400 2.900 -
TT Straps 1,200 (2 yrs) 297 (06/08) -
Swashplate Assembly 4,800 - 1,705
Main Transmission 4,500 (1,500 I) - 1,748 (345 I)
Hydraulic Pump and Reservoir 3,600 - 1,649
Freewheel Assembly 3,000 (1,500 I) - 1,649 (149 I)
Tail Rotor Blades (x 2) 2,500 1,849 (x 2) -
Tail Rotor Yoke 4,800 4,349 -
Tail Rotor Hub 2,400 - 1,849
Tail Rotor Gearbox 6,000 (3,000 I) - 3,248 (248 I)
Hydraulic Servos (x 3) 3,600 - 3,051 (x 3)
     
Compressor 3,500 - 2,788
Impellor 3,550 (9,150 C) 2,838 (1,645 C) -
Turbine Assembly 3,500 (1,750 I) - 2,788 (1,038 I)
Wheel 1 1,775 (3,000 C) 1,063 (1,986 C) -
Wheel 2 1,775 (3,000 C) 1,063 (1,986 C) -
Wheel 3 4,550 (6,000 C) 1,773 (1,988 C) -
Wheel 4 4,550 (6,000 C) 350 (45 C) -
Fuel Control 2,500 - 6,120
Governor 2,000 - 374
Fuel Pump 2,250 - 3,797
Fuel Nozzle 2,500 - 2,251
Bleed Valve 1,500 - 252