The shop can perform overhaul, inspection, repair and functional tests on the landing gear components and flight controls for the MI-8 helicopter series.
CAPABILITIES |
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| DESCRIPTION | P/N | ||
| LANDING GEAR | MAIN LANDING GEAR | MAIN LANDING GEAR SHOCK ABSORBER | 8A-4101-00B |
| WHEEL AND RIM ASSEMBLY | KT97-310 | ||
| BREAK | KT97-220 | ||
| LANDING GEAR SUPPORT | |||
| NOSE LANDING GEAR | NOSE LANDING GEAR SHOCK ABSORBER | 8A-4201-00A | |
| SUPPORT | |||
| WHEEL AND RIM ASSEMBLY | K2116 | ||
| TAIL-SKID | SHOCK ABSORBER | V24-4301-100-7 | |
| SUPPORT | |||
| LANDING GEAR NON-REMOVABLE COMPONENTS | |||
| FLIGHT CONTROLS | DESCRIPTION | P/N | |
| POWER GRADIENT MECHANISMS | 8A-5400-120-3 / - 5 | ||
| CYCLIC CONTROL LEVER | 8A-5101-00-3 IZQ. | ||
| 8A-5101-00-5 DER. | |||
| COLLECTIVE PITCH LINK | 8A-5901-130 IZQ. | ||
| 8A-5901-140 DER. | |||
| PEDALS | 8AM T-5201-001/-002 | ||
| RODS. CAMS, CONTROL SUPPORTS | |||
| MAIN ROTOR BREAK LEVER | 8-5801-00 | ||
| FUEL SHUT OFF VALVE HANDLES | 8A-6502-90 | ||
| FLIGHT CONTROL UNITS, LONGITUDINAL, TRANSVERSAL, PEDALS, COLLECTIVE PITCH (TORQUE TUBE) | |||
| ENGINE CONTROL SHAFT | 8A-5913-40 | ||
| COLLECTIVE PITCH CONNECTION SHAFT | 8A-5901-90 | ||
| SHAFT | 8A-5913-70 | ||