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.
