TM 1-1520-238-23
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Change 2
2.126.
ACCESS DOOR T290L OR T290R REMOVAL/INSTALLATION – continued
2.126.3. Removal
a. Remove access door (1) from support assem-
bly (2).
(1) With one person holding door (1), remove 12
screws (3) from 3 hinges (4).
(2) Remove shims (5). Secure to respective
hinge and identify for proper location.
2.126.4. Cleaning
a. Wipe door and mounting surface with a clean
rag.
2.126.5. Inspection
a. Check door mount for cracks, nicks, dents,
elongated screw holes, and loose or missing
nutplates (para 2.11).
b. Check door for cracks, nicks, dents, and
loose or missing hardware (para 2.11).
NOTE
Steps c. and d. refer to aircraft equipped
with EMI provisions.
c. Check door and support mating surface for
loose or damaged EMI gasket (para 2.1).
d. Check door and support mating surface for
damaged EMI conductive coating. Repair door
and mating surface (para 2.34).
2.126.6. Installation
a. Install door (1) on support assembly (2).
(1) With one person holding door (1), install
shims (5) under three hinges (4).
(2) Install 12 screws (3) in 3 hinges (4).
b. Inspect (QA).
c. Secure access doors T250L, T250R, T290L,
T290R, and L325 (para 2.2).
END OF TASK
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1
M04-2958-2
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5
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M04-2958-3
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3
4
5
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