TM 1-1520-238-PM
2–73
PHASE NO.
Date
Aircraft Serial No.
Area Name and No.
MAIN ROTOR – 10
Inspect
Phase
Nos.
Initial
Action Taken
Faults and/or Remarks
Status
Inspection Requirements
ALL
16.
Rotating scissors for cracks, corrosion,
and security. Pivot bearings for wear.
C
ALL
17.
Longitudinal and lateral torque links for
cracks, dents, scratches, and corrosion.
C
Attachment bolts for security. Bearings
for looseness.
Access T205L, T205R, T255
ALL
18.
Longitudinal, lateral, and collective
bellcranks for cracks, distortion, and
C
corrosion. Check floating bushing
clamp-up to rod ends.
Access T205L, T205R, T255
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
