41A12102: CAM,CONTROL.
The CAM,CONTROL is a the manufacturer industrial component. Key specifications include special_features: FACES ARE PARALLEL;BORE DIA 0.3122 IN. TO 0.3125 IN.;BORE LENGTH 0.700 IN.;FACES SPACED 0.0919 IN.
TO 0.959 IN. APART IN, end_item_identification: J-57 AIRCRAFT ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 3040-00-628-0916, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| special_features | FACES ARE PARALLEL;BORE DIA 0.3122 IN. TO 0.3125 IN.;BORE LENGTH 0.700 IN.;FACES SPACED 0.0919 IN. TO 0.959 IN. APART IN |
| end_item_identification | J-57 AIRCRAFT ENGINE |
| part_name_assigned_by_controlling_agency | FSC APPLICATION DATA:SHAFT GROUP,SPEED SET CAM P/N 67A12129A,FSCM 11599 ON BODY GROUP,BLEED CONTROL P/N 6A12352A FOR CONTROL,COMPRESSOR BLEED FSCM 11599,P/N A12110AAG |
| NSN | 3040-00-628-0916 |
| SPECIAL FEATURES | FACES ARE PARALLEL;BORE DIA 0.3122 IN. TO 0.3125 IN.;BORE LENGTH 0.700 IN.;FACES SPACED 0.0919 IN. TO 0.959 IN. APART IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FSC APPLICATION DATA:SHAFT GROUP,SPEED SET CAM P/N 67A12129A,FSCM 11599 ON BODY GROUP,BLEED CONTROL P/N 6A12352A FOR CONTROL,COMPRESSOR BLEED FSCM 11599,P/N A12110AAG |
| END ITEM IDENTIFICATION | J-57 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.