TM 1-1520-238-PM
2–91
PHASE NO.
Date
Aircraft Serial No.
Area Name and No.
MID AND LOWER FUSELAGE – 12
Inspect
Phase
Nos.
Initial
Action Taken
Faults and/or Remarks
Status
Inspection Requirements
2,4
8.
Pilot directional pedal control linkage cover
for cracks, corrosion, distortion, and loose
or missing hardware.
Access B90, B120, gun and turret removed.
ALL
9.
Flight control rods for dents, cracks,
corrosion, security, and evidence of
C
interference. Rod ends for looseness.
Access B80L, B80R, B75R, B85L, B85R
ALL
10.
Flight control bellcranks for cracks,
corrosion, and security. Brackets for
C
mounting security and evidence of
interference. Pivot bearings for
looseness. Check floating bushing
clamp-up.
Access B75R, B85L, B85R
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
