TM 55-1520-240-PM
PHASE NO. _____
Area Name and No.
Aircraft Serial No.
Date
LEFT FUSELAGE, AREA #2
Inspect
Phase
No’s
Inspection Requirements
Status
Faults and/or Remarks
Action Taken
Initial
ALL
2.27 Aft landing gear strut for leaks,
cleanliness of exposed piston, normal
extension (visual).
ALL
2.28 Aft landing gear support structure
for buckling, cracks, corrosion, and
loose or missing fasteners.
ALL/C
2.29 Aft landing gear drag links for
security, corrosion, cracks, nicks,
dents, twisting, and displacement
of bearings from bores. All surfaces
of lower drag link for cracks, with
particular attention to area around
forward trunnion anti-rotation bolt hole.
Access 61
ALL/C
2.30 Lubricate aft landing gear grease
fittings.
ALL
2.31 Engine water wash system quick
disconnect for security and damage.
(With 74 )
ALL
2.32 Static ground wire for security and
ground contact.
"FOD REMINDER"
Check work area for tools and parts after completion of maintenance and inspection.
2-10
