TM 1-1520-238-PM
2–114
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
ALL
32.
Tail rotor fork yoke teetering bearing for
cracks, separation, or deterioration.
C
Teetering bearing center studs for
looseness.
ALL
32a. Inspect 3 nuts securing tail rotor fork to tail
rotor output shaft for proper torque and
wear.
ALL
33.
Tail rotor teetering stops for cracks or
distortion.
C
ALL
34.
Tail rotor root blade bolt heads and nuts
for cracks or looseness.
C
ALL
35.
Tail rotor blade spars and root finger
doublers for delamination.
C
ALL
36.
Tail rotor blade leading edges for cracks,
dents, distortion, or erosion. Leading
C
edge tips for loose or missing hardware.
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
