PWA57028: FIXTURE,ENGINE MAINTENANCE,AIRCR.
FIXTURE,ENGINE MAINTENANCE,AIRCR. Key specifications include special_features: STEEL AND ALUMINUM; THIS WILL BE REPLACED BY REOP TOOLING, functional_description: USED DURING BUILD-UP OF THE 2ND STAGE TURBINE DISK ONTO THE REAR OF THE TURBINE FRONT HUB, nominal_overall_height: 11.000 INCHES IN, end_item_identification: F100-PW-100/200/220/220E AIRCRAFT ENGINE, nominal_overall_diameter: 22.000 INCHES IN, reference_data_and_literature: SERD NO. 4672; T.O.
2J-F100-94. This part is cataloged in the U.S. Government catalog under NSN 4920-01-194-3768, 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 | STEEL AND ALUMINUM; THIS WILL BE REPLACED BY REOP TOOLING |
| functional_description | USED DURING BUILD-UP OF THE 2ND STAGE TURBINE DISK ONTO THE REAR OF THE TURBINE FRONT HUB |
| nominal_overall_height | 11.000 INCHES IN |
| end_item_identification | F100-PW-100/200/220/220E AIRCRAFT ENGINE |
| nominal_overall_diameter | 22.000 INCHES IN |
| reference_data_and_literature | SERD NO. 4672; T.O. 2J-F100-94 |
| part_name_assigned_by_controlling_agency | FIXTURE ENGINE MAINTENANCE CLAMPING PLATE |
| NSN | 4920-01-194-3768 |
| NOMINAL OVERALL DIAMETER | 22.000 INCHES IN |
| REFERENCE DATA AND LITERATURE | SERD NO. 4672; T.O. 2J-F100-94 |
| NOMINAL OVERALL HEIGHT | 11.000 INCHES IN |
| SPECIAL FEATURES | STEEL AND ALUMINUM; THIS WILL BE REPLACED BY REOP TOOLING |
| FUNCTIONAL DESCRIPTION | USED DURING BUILD-UP OF THE 2ND STAGE TURBINE DISK ONTO THE REAR OF THE TURBINE FRONT HUB |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FIXTURE ENGINE MAINTENANCE CLAMPING PLATE |
| END ITEM IDENTIFICATION | F100-PW-100/200/220/220E AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.