TM 1-1520-238-23 11-26 Change 3 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 7-115116050 MS27647-4 0.7488 0.7493 0.7495 0.7500 Temp Yes 375 1, 2, 3, 4, 5 7-115116051 HS606S4-11 0.3757 0.3762 0.3762 0.3768 Temp No 188 1, 2 7-115117005 MS27647-4 0.7488 0.7493 0.7495 0.7500 Temp Yes 375 1, 2, 3, 4, 5 7-115117030 MS27647-4A 0.6238 0.6243 0.6245 0.6250 Temp Yes 313 1, 2, 3, 4, 5 7-115117037 MS27647-4A 0.6238 0.6243 0.6245 0.6250 Temp Yes 313 1, 2, 3, 4, 5 7-115117041 MS27647-4 0.7488 0.7493 0.7495 0.7500 Temp Yes 375 1, 2 7-115117042 HS606S4-12 0.3757 0.3762 0.3762 0.3768 Temp No 188 1, 2 7-115117044 MS27641-4 0.7488 0.7493 0.7495 0.7500 Temp Yes 375 1, 2 MS27641-4 0.7500 0.7505 0.7495 0.7500 Press Yes 375 1 7-115117047 HS606S4-12 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-115121005 HS606S4-16 0.3757 0.3762 0.3762 0.3768 Temp No 188 1, 2, 6 7-211516038 MS27647-4 0.7488 0.7493 0.7495 0.7500 Temp Yes 375 1, 2, 3, 4, 5 7-211516039 HS606S4-6 0.3757 0.3762 0.3762 0.3768 Temp No 188 1, 2 7-211516063 MS27641-4 0.7488 0.7493 0.7495 0.7500 Temp Yes 375 1, 2, 3, 5 GO TO NEXT PAGE