1980 Bell 206L |
SPECIFICATIONS
Date of Manufacture: | 1980 |
Total Airframe Hours: | 7,776 |
Optional Equipment
Range Extender | Rotor Brake |
Baggage Bay Extender | Low Skid Gear |
Avionics
VHR Com x 2 | . |
VOR x2 | . |
HSI | . |
ADS | . |
Transponder with Mode C | . |
Radio Altimeter | . |
Garmin GPS | . |
Exterior
Red and white with silver accent lines
Interior
Cream leather upholstery
Details believed to be correct but subject to verification by inspection.
Component Status |
Item | Life | Hrs - Retirement | Hrs - Overhaul |
Main Rotor Blades (x2) | 3,600 | 332/2,040 | - |
Main Rotor Hub Assembly | 2,400 | - | 1,661 |
Main Rotor Grips (x2) | 4,800 | 4,538 | - |
Main Rotor Mast Assembly | 3,000 | - | 1,992 |
Main Rotor Trunnion | 24,000 | 19,223 | - |
TT Straps | 1,200 (2 yrs) | 1,200 (03/10) | - |
Support Swashplate | 4,800 | - | 1,440 |
Swashplate Assembly | 4,800 | - | 1,440 |
Main Transmission | 4,500 (1,500 I) | - | 4,192 (1,192 I) |
Freewheel Assembly | 3,000 | - | 1,193 |
Tail Rotor Blades (x 2) | 2,500 | 2,274 | - |
Tail Rotor Yoke | 5,000 | - | 1,867 |
Tail Rotor Hub | 2,400 | - | 1,661 |
Tail Rotor Gearbox | 6,000 | - | 1,193 |
Hydraulic Servos (x 3) | 3,600 | - | 3,014 (x2)/2,965 |
Compressor | 1,500 | - | 991 |
Impellor | 12,500 (25,000 C) | 7,936 (18,044 C) | - |
Turbine Assembly | 1,500 | - | 1,274 |
Wheel 1 | 1,550 (3,000 C) | 1,324 (2,505 C) | - |
Wheel 2 | 1,550 (3,000 C) | 1,324 (2,505 C) | - |
Wheel 3 | 4,550 (6,000 C) | 4,324 (5,505 C) | - |
Wheel 4 | 4,550 (6,000 C) | 2,619 (1,364 C) | - |
Fuel Control | 2,500 | - | 78 |
Governor | 2,000 | - | 931 |
Fuel Pump | 3,000 | - | 917 |
Fuel Nozzle | 2,000 | - | 1,318 |
Bleed Valve | 1,500 | - | 991 |