RIGGING PILOT AND CPG DIRECTIONAL PEDAL STOP BOLTS continued

RIGGING PILOT AND CPG DIRECTIONAL PEDAL STOP BOLTS continued - TM-1-1520-238-23-7-2_451

RIGGING TAIL ROTOR DIRECTIONAL FLIGHT CONTROLS

TM-1-1520-238-23-7-2 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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TM 1-1520-238-23 11-1269 11.295. RIGGING PILOT AND CPG DIRECTIONAL PEDAL STOP BOLTS – continued s. Adjust bolt (11) to contact SPAD (1). (1) Rotate bolt (11) out of bracket (14) until it contacts SPAD (1). (2) Hold bolt (11). Tighten nut (13). (3) Lockwire bolt (11) to nut (13) and bracket (14). Use wire (item 224, App F). t. Adjust CPG left limit stop bolt (15) for a 0.020 INCH gap between bolt (15) and CPG SPAD (20). (1) Hold pedal (2) forward to maintain contact between SPAD (20) and bolt (15). (2) Hold 0.020 INCH thickness gage (21) against SPAD (20). (3) Rotate bolt (15) counterclockwise until it con- tacts gage (21) held against SPAD (20). (4) Hold bolt (15). Tighten nut (17). (5) Lockwire stop bolt (15) to nut (17) and brack- et (18). Use wire (item 224, App F). u. Inspect (QA). v. Perform directional flight control rigging maintenance operational check (TM 1-1520-238-T). w. Disconnect maintenance headset (para 1.134). x. Remove external hydraulic power from air- craft (para 1.72). y. Install gun turret assembly (TM 9-1090-208-23). z. Install access panels B60, L200, and L540 (para 2.2). aa. Inspect (QA). END OF TASK 11 13 M04-3028-14 1 14 17 15 20 21 M04-3028-15 18 2 18 PILOT STATION M04-3028-17 2 3

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