856A1453G02: FIXTURE,ENGINE MAINTENANCE,AIRCR.
FIXTURE,ENGINE MAINTENANCE,AIRCR. Key specifications include end_item_identification: F-108 ENGINE, functional_classification: GG-7.4, reference_data_and_literature: SERD CFC3711. This part is cataloged in the U.S.
Government catalog under NSN 4920-01-375-5529, 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.
| functional_description | SUPPORTS P/N 856A1452G02,SHAFT WHEN CENTERING THE HIGH PRESSURE TURBINE (HPT) ROTOR AT MODULE 12 INSTALLATION OR REMOVAL IN THE HORIZIONAL POSITION |
| end_item_identification | F-108 ENGINE |
| functional_classification | GG-7.4 |
| reference_data_and_literature | SERD CFC3711 |
| NSN | 4920-01-375-5529 |
| REFERENCE DATA AND LITERATURE | SERD CFC3711 |
| FUNCTIONAL CLASSIFICATION | GG-7.4 |
| SPECIAL FEATURES | CONSIST OF A A-FRAME WELDMENT; ADJUSTABLE JACKSCREW THRU THE TOP CENTER PLATE; A V-GROOVE BLOCK ON TOP TO INTERFACE WITH THE HPT SHAFT EXTENSION,P/N 856A1454; CONSTRUCTED OF ALUMINUM AND IS ANODIZED FOR CORROSION PROTECTION |
| FUNCTIONAL DESCRIPTION | SUPPORTS P/N 856A1452G02,SHAFT WHEN CENTERING THE HIGH PRESSURE TURBINE (HPT) ROTOR AT MODULE 12 INSTALLATION OR REMOVAL IN THE HORIZIONAL POSITION |
| END ITEM IDENTIFICATION | F-108 ENGINE |
No substitute or cross-reference records for this part.