TM 1-1520-238-23 Change 3 11-33 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 7-311516078 HS606S3-5 0.3129 0.3134 0.3135 0.3140 Temp Yes 157 1, 2 7-311517002 MS27647-4 0.7488 0.7493 0.7495 0.7500 Temp Yes 375 1, 2, 3, 4, 5, 8 7-311517003 HS606S4-11 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311517012 MS27646-38 1.0608 1.0613 1.0615 1.0625 Temp Yes 531 1, 2 MS27646-38 1.0627 1.0632 1.0615 1.0625 Press Yes 531 1 7-311517020 HS606S4-15 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2, 16 7-311517038 HS606S4-7 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2, 16 7-311517039 MS27641-4 0.7488 0.7493 0.7495 0.7500 Temp Yes 375 1, 2, 3 MS27641-4 0.7500 0.7505 0.7495 0.7500 Press Yes 375 1 7-311517040 HS606S4-7 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311517043 HS606S4-18 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311517052 MS27640-4 0.9002 0.9007 0.9009 0.9014 Temp Yes 450 1, 2, 3 MS27640-4 0.9019 0.9024 0.9009 0.9014 Slip Yes N/A 1 7-311517053 HS606S4-9 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 7-311517055 HS606S4-11 0.3757 0.3762 0.3762 0.3768 Temp Yes 188 1, 2 GO TO NEXT PAGE