TM 1-1520-238-PM
2115
C1
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
36a. Perform chordwise inspection of the
doubler and spar edges located in
C
transition area of the tail rotor blade. The
transition area of the blade root fittings
begin 1.5 inches from the center line of
the blade retention bolt and ends 2.5
inches from the center line of the blade
retention bolt.
ALL
37.
Tail rotor blade bushings (inside root
fittings) for looseness. Dust boots for
C
damage, misalinement, and security.
2,4
37a. Disassemble and repack tail landing gear
fork per TM 1-1520-238-23-2.
2,4
38.
TLG arms for cracks, bending,
distortion, and security. Pivot pin and
C
bushing for looseness.
Access L545, R545
FOD REMINDER
Check work area for tools and parts after completion of maintenance and inspection.