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
3.14 Lubricate aft landing gear grease
fittings.
ALL
3.15 Engine water wash system quick
disconnect for security and condition.
(With 74 )
ALL/C
3.16 Aft external cargo hook retaining
bolt (access panel removed) and
safety bolt for proper installation and
corrosion.
ALL
3.17 Aft 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,
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.
2-14
