TM 1-1520-238-PM
2–112
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
26.
Tail rotor flight control bellcranks for
cracks, corrosion, security, and evidence
C
of interference. Floating bushing
clamp-up and pivot bearings for
looseness.
Access L510, L530, L540, R510
ALL
27.
Tail rotor flight control servocylinder for
leakage, cracks, and corrosion. Rod end
C
and base clevis for bearing damage and
attachment security. Rod end for radial
looseness. Inspect servocylinder control
linkage fasteners for damage, corrosion,
and security.
Access L530, L540
2,4
28.
Inspect and clean tail rotor flight control
servocylinder pressure filter.
Access L530, L540
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
