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FLIGHT CONTROL SYSTEM BEARING/BUSHING REPLACEMENT (AVIM) – continued
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TM-1-1520-238-23-7-1 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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FLIGHT CONTROL SYSTEM BEARING/BUSHING REPLACEMENT (AVIM) – continued

TM 1-1520-238-23 Change 7 11-37 11.4. FLIGHT CONTROL SYSTEM BEARING/BUSHING REPLACEMENT (AVIM) – continued TABLE  11-1 Flight Control System Bearing/Bushing Replacement Data – continued Next Higher Assembly P/N Notes Max Hyd Ram Pressure (pounds) Cadmium Plated Slip, Press, or Temp Fit Bearing/ Bushing OD (inches) Mating Bore Size (inches) Bearing/ Bushing P/N 7-311525064 (FSP) HS4619-11C010B 0.8749 0.8759 0.8762 0.8767 Temp No 438 2, 7 MS14103-12 1.3750 1.3760 1.3745 1.3750 Press No 687 4, 7, 33 7-311527009 7-115127019 0.4997 0.5005 0.5007 0.5017 Temp No 251 2, 7 7-115127020 0.4997 0.5005 0.5007 0.5017 Temp No 251 2, 6, 7 7-311527035 (FSP) HS4736KR 6CWGH 0.8119 0.8128 0.8120 0.8125 Temp No 406 2, 4, 7, 27, 29, 34, 35, 39 7-211527014 1.5619 1.5628 1.5620 1.5625 Temp No 781 2, 4, 7, 28, 30, 34, 35,38, 39 NOTE 1.   Apply primer coating (item 147, App F) using brush (item 34, App F) on mating bore. Install bearing/ bushing while primer is still wet. 2.   Use carbon dioxide (item 40, App F) (dry ice). If necessary, use heater. 3.   Use staking tool kit (TM 55-1500-322-24). Determine correct staking pressure in accordance with TM 55-1500-322-24. 4.   Stake both sides (TM 55-1500-322-24). 5.   Use fly cutter if necessary for removal. If removing bearing from aluminum housing, use of fly cutter is mandatory. 6.   Use appropriate bushing driver set. 7.   Apply sealing compound (item 176, App F) using brush (item 34, App F) on mating bore. Install bearing/bushing while sealing compound is still wet. 8.   Use ring stake method (TM 55-1500-322-24). 9.   Use adhesive (item 5, App F). 10.   Aline inside diameters to be within 0.0005 INCH. 11.   Install with care to prevent damage to surface finish on flange surface. 12.   Bushing 7-311511120 must be installed before bushing 7-311511202-13. 13.   Clean ID of bearing/bushing. Use cleaner (item 43, App F). GO TO NEXT PAGE

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