1982 Bell 206L-3 |
SPECIFICATION
Date of Manufacture: | 1982 |
Total Airframe Hours: | 5,982 |
Optional Equipment
High Skid Gear | Flitesteps |
Particle Separator | Increased Power Kit |
Par Avion Heater | Dual controls |
R/H Sliding door | Baggage Bay Extender |
Facet Oil Filter | Rotor Brake |
Door Openers | Wedge Windows |
Floor Protectors | - |
Avionics
Full IFR Panel | . |
VHR Com x 2 | King KY 196 |
Area Nav | King KNS 80 |
ADF | King KR 87 |
DME | King KN 62A |
RMI | . |
HSI | King KI 525 |
Audio Panel | King KMA 24H |
Noise Attenuating Headsets x 7 | . |
Exterior
Red fuselage with grey base
Interior
Corporate six place seating with grey leather and grey carpet
Component Status (as at 5,982 airframe hours) |
Item | Life | Hrs - Retirement | Hrs - Overhaul |
Main Rotor Blades (x2) | 3,600 | 208 (x2) | - |
Main Rotor Hub Assembly | 2,400 (1,200) | - | 1,675 (475) |
Main Rotor Grips (x2) | 4,800 | 3,653 | - |
Main Rotor Mast Assembly | 3,000 | - | 387 |
Main Rotor Trunnion | 24,000 RIN | 22,379 RIN | - |
TT Straps | 1,200 (2 yrs) | 1,198 (05/12) | - |
Support Swashplate | 4,800 | - | 2,396 |
Swashplate Assembly | 4,800 | - | 4,075 |
Main Transmission | 3,000 (1,500 I) | - | 387 |
Freewheel Assembly | 3,000 | - | 2,839 |
Tail Rotor Blades (x 2) | 2,500 | 2,248 | - |
Tail Rotor Yoke | 5,000 | 3,532 | - |
Tail Rotor Hub | 2,400 | - | 1,579 |
Tail Rotor Gearbox | 6,000 | - | 389 |
Hydraulic Servos (x 3) | 3,600 | - | 586 (x2)/3,574 |
Compressor | OC | - | OC |
Impellor | 12,500 (25,000 C) | 12,439 (19,538 C) | - |
Turbine Assembly | 2,000 | - | 1,181 |
Wheel 1 | 2,025 (3,000 C) | 1,206 (2,370) | - |
Wheel 2 | 2,025 (3,000 C) | 1,206 (2,370) | - |
Wheel 3 | 4,550 (6,000 C) | 3,731 (5,370) | - |
Wheel 4 | 4,550 (6,000 C) | 3,731 (5,370) | - |
Fuel Control | 2,500 | - | 586 |
Governor | 2,000 | - | 568 |
Fuel Pump | 3,000 | - | 1,385 |
Fuel Nozzle | 2,000 | - | 1,839 |
Bleed Valve | 1,500 | - | 1,040 |