TM 1-1520-238-23
1-158.22
Change 9
1.49.
CORROSION CONTROL/INSPECTION – continued
(10) Seal pilot external armor plate with sealing compound (item 164, App F) or sealing compound (item 170A,
App F).
(11) Seal around static port brace and panel adjacent to fuselage with sealing compound (item 162, App F) or
sealing compound (item 170C, App F).
(12) Apply corrosion preventive compound (item 64, App F), followed by corrosion preventive compound
(item 62B, App F) to all electrical connectors in access are L115.
x. Nose Section (area 12)
(1) Apply corrosion preventive compound (item 64, App F), followed by corrosion preventive compound
(item 62B, App F), to all electrical connectors under access panels R40 and L40.
(2) Apply epoxy primer coating kit (item 76A, App F) or epoxy primer coating kit (item 78A, App F) to all bolt
heads, nuts, exposed threads, mounting brackets, and fasteners. Use sealing compound (item 162,
App F) or sealing compound (item 170A, App F) as an alternate, if primer is not available.
(2) Apply corrosion preventive compound (item 64, App F), followed by corrosion preventive compound
(item 62B, App F), to all electrical connectors in the TADS/PNVS turret.
y. Armament
(1) Apply lubricating oil (item 119A, App F) or corrosion preventive compound (item 63A, App F) to all ex-
posed metal areas.
z. Pilot Station (area 13)
(1) Apply corrosion preventive compound (item 63, App F) or corrosion preventive compound (item 63A,
App F) to canopy door latch, hinges, and canopy support strut.
(2) Apply sealing compound (item 162, App F) or corrosion preventive compound (item 62B, App F) to seat
attachment fittings and pins.
(3) Apply corrosion preventive compound (item 63, App F) or corrosion preventive compound (item 63A,
App F) to armor swing plate hinges and latches.
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