TM 1-1520-238-PM
2–116
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
2,4
39.
REPACK TLG WHEEL BEARINGS AND
CHECK FOR SMOOTH OPERATION.
C
ALL
40.
TLG shock strut for leakage, cracks,
distortion, or corrosion. Rod ends for
C
bearing damage.
2,4
41.
Tail boom end frame (F.S. 530 & 547.15)
for cracks, corrosion, worn or failed
C
bearing or bushing, and loose or
working rivets.
Access L545, R545, B545
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
