TM 1-1520-238-PM
2–93
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
ALL
14.
LVDTs for cracks, corrosion, and
mounting security. Wiring harness for
C
loose connections, chafing, or
deterioration and evidence of
interference. Rod ends for looseness.
Access B80L, B80R, B85L, B85R
2,4
15.
Ammo bay interior bulkheads for cracks,
distortion, or corrosion. Stringers for
C
bending or misalinement.
Access B200 – ammo magazine removed
for access.
2,4
16.
Ammo bay interior wing support
structure for cracks, corrosion, loose or
C
missing fasteners, and security.
Access B200 – ammo magazine removed
for access.
ALL
17.
Ammo bay interior fuel cell stress panels
for cracks, delamination, distortion,
C
loose or missing fasteners. Fuel vent
tube for chafing.
Access B200 – ammo magazine removed
for access.
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
