TM 1-1520-238-PM
2–111
PHASE NO.
Date
Aircraft Serial No.
Area Name and No.
EMPENNAGE, TAIL ROTOR, AND TLG – 14
Inspect
Phase
Nos.
Initial
Action Taken
Faults and/or Remarks
Status
Inspection Requirements
ALL
23.
Test tail rotor and intermediate gearbox
alarm control unit.
Access L530, L540
ALL
24.
Tail rotor flight control rods for dents,
cracks, corrosion, security, and evidence
C
of interference. Check rod ends for
looseness and worn or seized bearings.
Access L510, L530, L540, R510
ALL
25.
Tail rotor pitch change links for dents,
cracks, corrosion, security, evidence of
C
interference, worn or seized bearings,
and tolerance wear limits.
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
