TM 1-1520-238-PM
2–107
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
9.
Stabilator structure and skins for cracks,
dents, distortion, and loose or missing
C
rivets or fasteners.
ALL
10.
Stabilator tip fairings for cracks and
loose or missing screws.
C
ALL
11.
Stabilator actuator for cracked,
deformed, or jammed jackscrew, and
C
loose rod end bearings. Wiring for
chafing, deterioration, security, and
proper connection. Stabilator fittings for
cracks, loose or missing hardware, and
worn or seized bearings.
Access L545, R545
ALL
12.
Stabilator position transducer for
mounting security. wiring for connection
C
security and chafing.
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
