TM 1-1520-238-PM
2–113
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
29.
Tail rotor swashplates for cracks or
corrosion. Looseness between
C
stationary and rotating swashplates.
Access L530, L540
2,4
30.
Tail rotor rotating scissors for cracks,
corrosion, and security. Pivot bearings
C
for wear.
ALL
31.
Tail rotor head for cracks, distortion,
corrosion, and security. Check mounting
C
nuts for proper torque.
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
