TM 1-1520-238-23
Change 9
1-158.33
1.49.
CORROSION CONTROL/INSPECTION continued
5
Tail landing gear
Apply to all bolt heads, nuts, and exposed threads at strut frame mount.
Apply to all bolt heads, nuts, and exposed threads on trailing arm and
wheel.
Apply epoxy primer coating kit (item 78A, App F) to wheel lug nuts,
then apply topcoat polyurethane coating (item 140B, App F).
8
Main rotor and mast
Apply to all bolt heads, nuts, exposed threads, retainers, control rod
ends, linkages, and exposed metal areas.
10
Landing gear
Apply epoxy primer coating kit (item 78A, App F) to wheel lug nuts,
then apply topcoat polyurethane coating (item 140B, App F).
Application of sealing compound (item 162, App F) or sealing compound (item 170A, App F) in coastal and
tropical areas.
NOTE: 1. Inspect and reapply when there are visible cracks or loss of adhesion.
2. Where torque stripe is used, apply corrosion preventive compound (item 62B, App F).
Area
Location
Specifics
1
Main Landing gear
Apply to all bolt heads, nuts, exposed threads, and metal connectors on
shock strut.
Apply to metal clamps on trailing arm and all unprotected, exposed
metal areas at upper end.
2
Fuselage right side, center
Apply to wing mounting bolts.
Transmission deck
Apply to screw heads, seams, and mounting brackets on air speed
transducer.
Apply to screw heads, mounting brackets, and seams on both air speed
transducers.
3
Engine nacelle right
Apply corrosion preventive compound (item 62B, App F) to leveling jack
RN1.
4
Fuselage right side, aft
Apply to all tail rotor drive shaft hanger mount bolts.
Apply to all tail rotor drive shaft coupling flanges and bolts.
5
Tail section
Apply to vertical stabilizer mounting bolts.
Apply to horizontal stabilator mounting bolts and servo attachment
fittings.
Directional servo actuator
Seal cracks at base.
Intermediate gearbox
Apply to all bolt heads, nuts, exposed threads, and fittings.
Tail rotor gearbox
Apply to all bolt heads, nuts, exposed threads, and fittings.
9
Engine nacelle
Apply corrosion preventive compound (item 62B, App F) to leveling jack
LN1.
10
Fuselage left side, center
Apply to wing mounting bolts.
11
Fuselage left side, forward
Apply to metal clamps on trailing arm and all unprotected, exposed
metal areas at upper end.
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