FOD REMINDER
Check work area for tools and parts after completion of maintenance and inspection
TM 1-1520-238-PMS
9
Seq.
No.
Location
Item and Procedure
FUSELAGE RIGHT SIDE FORWARD
POWER OFF
1.1
Inspect aircraft forms and records for recorded discrepancies (DA PAM 738-751)
1.2
Exterior surfaces
Skin areas for cracks and distortion
Loose or missing hardware
Access panels, doors, and fairings for mounting security
Exposed hydraulic lines for leakage and chafing
Hydraulic connectors for security
1.3
1
Radar Warning Antenna
Physical damage and mounting security
1.4
2
Open Avionics Door R90
Interior panels for cracks and cleanliness
Loose or missing hardware
Interior components for physical damage and mounting security
Electrical connectors for security
Visible wiring for chafing or damaged insulation and connection security
Ammo conveyor for damaged or cracked carriers and tracks
1.5
3
STATIC PORT
OBSTRUCTIONS, CLEANLINESS, AND DAMAGE