TM 1-1520-238-PM
2–108
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
13.
Stabilator pivot bolts, pivot bearings,
and pivot bosses for cracks, distortion,
C
corrosion, and cleanliness. Pivot
bushings for lateral looseness.
Access LS1, RS1, L545, R545
CAUTION:
Do not use tail rotor control
push rods as hand-holds.
ALL
14.
Intermediate gearbox housing, input and
output retainers for cracks, distortion,
C
and security. Check for grease leakage
or evidence of overheating (discoloration).
Gearbox mount fittings for cracks or
distortion. Grease for proper level.
Access L510, R510
2,4
15.
Intermediate gearbox mounting bolts for
proper torque.
C
Access L510, R510
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
