TM 1-1520-238-PM
2–101
PHASE NO.
Date
Aircraft Serial No.
Area Name and No.
TAILBOOM – 13
Inspect
Phase
Nos.
Initial
Action Taken
Faults and/or Remarks
Status
Inspection Requirements
ALL
9.
Drive shaft damper brackets for cracks,
dents, corrosion, and mounting security.
C
Access R410, R475
ALL
10.
Drive shaft dampers for proper friction
adjustment.
C
Access R410, R475
ALL
11.
Tail rotor flight control rods for dents,
cracks, corrosion, security, and evidence
C
of interference. Check rod ends for
looseness. Check wear sleeves for
debond and excessive wear.
Access R410, R475
ALL
12.
Tail rotor flight control bellcranks for
cracks, corrosion, security, and evidence
C
of interference. Pivot bearings for
looseness.
Access R410, R475
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
