FLIGHT CONTROL SYSTEM BEARING/BUSHING REPLACEMENT (AVIM)

TM 1-1520-238-23 11-42 11.4. FLIGHT CONTROL SYSTEM BEARING/BUSHING REPLACEMENT (AVIM) – continued CAUTION 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. CAUTION Do not exceed maximum ram pressure stated in Table 11-1. Housing may be damaged. 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 housing surface. (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- lation. 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 notes column. GO TO NEXT PAGE M04-4319-4 1 2