(7)Do not apply corrosion inhibiting compounds on grease joints or sealed
bearings. These compounds dissolve grease and other lubricants. They are
penetrating compounds and can get around the seals and into the bear-ings.
(8)Do not apply corrosion inhibiting compounds on interior materials such
as liners. The compounds change the flammable quality of these materi-als.
(9)Relubricate interior door fittings as necessary.
(10)Restore door to normal.
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CORROSION PREVENTION MANUAL
ELECTRICAL/ELECTRONICS ACCESS DOOR
B. Frequency of Application. Periodically inspect the door structure and con-dition of the corrosion inhibitor. Reapply corrosion inhibiting compound as
required. Local areas where gouges and scratches have occurred should be
treated at the first opportunity consistent with the maintenance schedule.
C. Treat the door opening at the same time as the door.
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CORROSION PREVENTION MANUAL
ELECTRICAL/ELECTRONICS ACCESS DOOR
LEAF SPRING TYPE DRAIN VALVE
PLUNGER TYPE DRAIN VALVE
DETAIL I
Electrical/Electronics Access Door
Figure 1
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CORROSION PREVENTION MANUAL
CHAPTER
53
FUSELAGE
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CORROSION PREVENTION MANUAL
DOORS
AREA
Section 41
Section 43
Section 44
PROBLEM
Corrosion of interior structure
Plugged drains
Corrosion of inside wheel wellsurfaces
Corrosion of door surroundingstructure
Corrosion of galley/ lavatoryfloorsand cargo
bays
Corrosion of interior structures
Corrosion of external fuselage skin
Plugged drains
Corrosion of door surroundingstructure
Corrosion under latch fittingfor electrical/
electronics access door
Corrosion of fairing skin and structure
Corrosion of interior cargocompartment struc-
ture
Corrosion of panels and stringers in forward
cargo compartment
Corrosion of interior structure
Plugged drains
INDEX
TERMINATING
PREVENTION ACTION
VOLUME 2 (IF ANY)
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