FLIGHT CONTROL SYSTEM BEARING/BUSHING REPLACEMENT (AVIM) continued
11.4.6. Installation (Slip or Pressure Fit Method)
Do not allow compounds to enter bear-
ing(s). Bearing(s) can be damaged.
a. 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 or housing may be
b. Install bearing/bushing (1) in housing (2) mat-
ing bore while primer or sealing compound 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-
GO TO NEXT PAGE