TM 1-1520-238-23
Change 2
2-122.1
2.43.
FORWARD AVIONICS BAY ACCESS DOOR REMOVAL/INSTALLATION – continued
2.43.3. Removal
a. Remove access door (1) from forward avion-
ics bay (2).
(1) Remove hinge pin (3) from hinge (4)
(TM 1-1500-204-23).
(2) Unfasten seven thumb latches (5) and re-
move door (1).
2.43.4. Cleaning
a. Wipe removed and attaching parts and sur-
faces with a clean rag.
2.43.5. Inspection
a. Check door for loose or damaged hinge
(TM 1-1500-204-23).
b. Check door for corrosion (para 1.49).
NOTE
Steps c and d refer to aircraft equipped
with EMI provisions.
c. Check door and mating surface for loose or
damaged EMI gasket (para 2.1).
d. Check door and avionics bay mating surface
for damaged EMI conductive coating. Repair
door and mating surface (para 2.34).
2.43.6. Installation
a. Install door (1) on avionics bay (2).
(1) One person aline and hold door (1) in posi-
tion.
(2) Install
pin
(3)
in
hinge
(4)
(TM 1-1500-204-23).
(3) Fasten seven latches (5) on door (1).
b. Inspect (QA).
END OF TASK
M04-1491-2A
2
5
1
1
3
4
VIEW LOOKING UP
2
5
1
1
3
4
M04-1491-3A
VIEW LOOKING UP
