TM 1-1520-238-23
2-130
2.46.
FORWARD AVIONICS BAY STRUCTURE FRAME ASSEMBLY FORWARD STEP SLEEVE BUSHING
REPLACEMENT – continued
2.46.6. Installation
CAUTION
Do not allow primer or paint to enter
bushing bore or bushing damage may
result.
Do not exceed maximum ram load of
188 POUNDS or support surface dam-
age may result.
a. Install new bushing (1) in support (2).
(1) Coat outside of bushing (1) and support (2)
bushing bore. Use primer coating (item 147,
App F) and brush (item 34, App F).
(2) Press bushing (1) in support (2) bushing bore
until seated or pressed flush with mating sur-
face. Use arbor press.
(3) Form a fillet of primer 0.125 INCH thick
around edges of bushing (1). Remove ex-
cess. Use primer coating (item 147, App F)
and brush (item 34, App F).
(4) Install four rivets (3) in support (2)
(TM 1-1500-204-23).
b. Inspect (QA).
c. Install forward avionics bay airframe step as-
sembly (para 2.45).
END OF TASK
M04-3968-3
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