TM 55-1520-240-PM
PHASE NO. _____
Area Name and No.
Aircraft Serial No.
Date
RIGHT FUSELAGE AREA #3
Inspect
Phase
No’s
Inspection Requirements
Status
Faults and/or Remarks
Action Taken
Initial
ALL/C
3.26 Remove, clean, inspect, and
repack forward landing gear wheel
bearings.
ALL/C
3.27 Forward landing gear support
structure for buckling, cracks,
corrosion, and loose or missing
hardware. Access 24
ALL
3.28 Forward landing gear strut for
leakage, cleanliness of exposed piston,
and normal extension (visual).
ALL
3.29 Forward external cargo hook
for freedom of motion, cleanliness,
damage, bumpers and corrosion.
Attachment fitting on structure for
cleanliness. Hook latch mechanism
for locked position. Manual release
cable for sufficient clearance between
ball fitting and lever (through inspection
window). Electrical harness and
release cable for proper installation and
cuts, kinking or fraying. Latch roller for
freedom of operation.
"FOD REMINDER"
Check work area for tools and parts after completion of maintenance and inspection.
2-16
