TM 1-1520-238-23 11-32 Change 6 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 7-311516037 HS606S4-6 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311516041 HS606S4-12 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311516047 HS606S4-8 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311516060 HS606S4-13 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311516061 MS27641-4 0.7488 0.7493 0.7495 0.7500 Temp Yes 375 1, 2 7-311516062 HS606S4-9 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311516064 HS606S4-10 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311516065 HS606S10-12 0.7500 0.7505 0.7510 0.7515 Temp Yes 376 1, 2 MS27646-40 1.3126 1.3135 1.3115 1.3125 Press Yes 626 1 7-311516066 HS606S4-14 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 MS27646-40 1.3126 1.3135 1.3115 1.3125 Press Yes 626 1, 3, 8 7-311514096 0.3750 0.3755 0.3761 0.3766 Replacement of this bearing/bushing is not currently authorized at AVUM/AVIM level. 7-311516067 7-211514095-3 0.3754 0.3759 0.3761 0.3766 Replacement of this bearing/bushing is not currently authorized at AVUM/AVIM level. 7-311514101 0.4396 0.4401 0.4381 0.4391 Slip No N/A 15 7-311516076 HS606S3-4 0.3129 0.3134 0.3135 0.3140 Temp Yes 157 1, 2, 6 GO TO NEXT PAGE