TM 1-1520-238-PM
210
PHASE NO.
Date
Aircraft Serial No.
Area Name and No.
FORWARD FUSELAGE 1
Inspect
Phase
Nos.
Initial
Action Taken
Faults and/or Remarks
Status
Inspection Requirements
ALL
11.
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 B40R, B60
2,4
12.
WARNING:
Do not attempt to move
jettison handle.
C
Exterior canopy jettison components for
cut or broken transfer tubes, bulged or
swollen unions, missing hardware, and
torn or missing streamer.
Access T50, L40, R40
2,4
13.
Canopy emergency release drain hose and
outlets for breaks.
Access T50, L40, R40
FOD REMINDER
Check work area for tools and parts after completion of maintenance and inspection.