FLIGHT CONTROL SYSTEM BEARING/BUSHING REPLACEMENT (AVIM) continued
Do not allow compounds to enter bear-
ing(s). Bearing(s) may be damaged.
c. Apply appropriate primer or sealing com-
pound on mating bore in housing (2). Refer to
Table 11-1 notes column.
Do not exceed maximum ram pressure
stated in Table 11-1. Housing may be
d. Install frozen bearing/bushing (1) in housing
(2) mating bore while primer or sealing com-
pound is still wet (TM 55-1500-322-24). Install
manually or use arbor press.
(1) Install flange type bearing(s)/bushing(s):
(a) Use ram pressure applied against flange.
(b) Ensure no primer or sealing compound is
present under flange.
(c) Ensure flange is fully seated against
(2) Install sleeve type bearing(s)/bushing(s) until
seated or flush with housing surface.
(3) Install in-line bearing(s)/bushing(s) so that
they are alined with one another during instal-
e. Apply appropriate primer or sealing com-
pound around housing (2) and bearing/bush-
ing to form a fillet seal. Refer to Table 11-1
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