Aircraft Serial No.
Area Name and No.
EMPENNAGE, TAIL ROTOR, AND TLG 14
Faults and/or Remarks
36a. Perform chordwise inspection of the
doubler and spar edges located in
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
Tail rotor blade bushings (inside root
fittings) for looseness. Dust boots for
damage, misalinement, and security.
37a. Disassemble and repack tail landing gear
fork per TM 1-1520-238-23-2.
TLG arms for cracks, bending,
distortion, and security. Pivot pin and
bushing for looseness.
Access L545, R545
Check work area for tools and parts after completion of maintenance and inspection.