TM 1-1520-238-PM
2–36
PHASE NO.
Date
Aircraft Serial No.
Area Name and No.
LEFT WING AND PYLONS – 5
Inspect
Phase
Nos.
Initial
Action Taken
Faults and/or Remarks
Status
Inspection Requirements
2,4
12.
Pitot/static lines for cracks, chafing, and
mounting security.
C
Remove wing trailing edge for access.
ALL
13.
Pylon actuator controller brackets for
cracks, corrosion, or warping.
Access P3
ALL
14.
Pylon station director bracket for cracks,
corrosion, or warping.
Access P1
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
