“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection
TM 1-1520-238-PMS
C 7
85
Seq.
No.
Location
Item and Procedure
FUSELAGE – LEFT SIDE FORWARD
POWER OFF
11.1
–––
Exterior Surfaces
Skin areas for cracks and distortion
Loose or missing hardware
Access panels and fairings for mounting security
Exposed hydraulic lines for leakage, chafing, and security
11.2
1
Open Door L187
2
UTILITY RETURN ACCUMULATOR VALVE FOR MISSING DUST CAP, LEAKAGE
3
UTILITY RETURN ACCUMULATOR PRESSURE GAGE FOR PROPER PRESSURE INDICATION
11.3
4
MAIN LANDING GEAR SHOCK STRUT
CRACKS, DISTORTION, AND CORROSION
STRUT TOP AND BOTTOM MOUNTS FOR SECURITY
FLUID LEAKAGE ON STRUT EXTERIOR
STRUT EXTENSION FOR NORMAL HELICOPTER GROUND ATTITUDE
Clean exposed piston rod with lubricating oil (VVL800A)
5
LOCKING SHEAR COLLAR IN LOCKED POSITION (RED STRIPE VISIBLE AND LOCK PIN INSTALLED)
COLLAR FOR CRACKS
