RIG COPILOTS COCKPIT CONTROL ASSEMBLY

ASSEMBLE COPILOTS COCKPIT CONTROL ASSEMBLY (Continued) - TM-55-1520-240-23-9_423

RIG COPILOTS COCKPIT CONTROL ASSEMBLY (Continued)

TM-55-1520-240-23-9 CH-47D Heilcopter Manual
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TM 55-1520-240-23-9 11-79 RIG COPILOT’S COCKPIT CONTROL ASSEMBLY 11-79 INITIAL SETUP Applicable Configurations: All Tools: Aircraft Mechanic’s Tool Kit, NSN 5180-00-323-4692 Rigging Set, Controls (T39) Torque Wrench, 30 to 150 Inch-Pounds Scale, 6 Inch Materials: None Parts: Cotter Pins Personnel Required: Medium Helicopter Repairer Inspector References: Task 1-13 Equipment Condition: Off Helicopter Task Rigging Fixture (T39) Installed (Task 11-22) Do not drive a rig pin into rigging hole. Damage to component will result. Do not lubricate rig pin. Lubrication will cause accumulation of dirt at rigging hole. NOTE Impedance bolts are installed in flight control connections. These bolts are self-retaining and require a special nut and torque (Task 1-13). RIG YAW CONTROL 1. Insert rig pin (1) fully in rigging hole (2) of support assembly (3) through yaw bellcrank (4) and through rigging pin hole in bottom of support assembly (3). If pin slides freely, go to step 10. If pin does not slide freely, remove pin. Perform steps 2 thru 10. 11-408

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