TM 1-1520-238-PM 2–14 PHASE NO. Date Aircraft Serial No. Area Name and No. CREW STATIONS – 2 Inspect Phase Nos. Initial Action Taken Faults and/or Remarks Status Inspection Requirements ALL 11. Pilot directional pedals for damage and security. Supports for cracks, bends, or C corrosion. Rod assemblies for cracks, corrosion, worn bearings, and loose or missing hardware. Adjusting handle for proper attachment and operation. 2,4 12. Pilot engine power controls for bent, cracked, or broken cable supports and C brackets. Rods and rod ends for loose or worn bearings and loose or missing hardware. Check power quadrant detent operation. Remove pilot left console side panels for interior access. 2,4 13. Pilot flight control linkage for cracks, corrosion, and security. C 2,4 14. Pilot wiring harnesses for loose or missing hardware, chafed wires, loose C connections, and broken tie-wraps. Brackets for damage or corrosion. Remove pilot console side panels for access. “FOD REMINDER” Check work area for tools and parts after completion of maintenance and inspection.