PWA95207: ADAPTER,MECHANICAL TEST.
The ADAPTER,MECHANICAL TEST is a the manufacturer industrial component. Key specifications include functional_description: USED TO DEAD LOAD TEST THE ADAPTER USED TO SUPPORT THE HIGH PRESSURE ROTOR AND STATOR MODULE, end_item_identification: F117-PW-100 AIRCRAFT ENGINE, reference_data_and_literature: SERD 1775. This part is cataloged in the U.S.
Government catalog under NSN 4940-01-384-9447, 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 | USED TO DEAD LOAD TEST THE ADAPTER USED TO SUPPORT THE HIGH PRESSURE ROTOR AND STATOR MODULE |
| end_item_identification | F117-PW-100 AIRCRAFT ENGINE |
| reference_data_and_literature | SERD 1775 |
| NSN | 4940-01-384-9447 |
| REFERENCE DATA AND LITERATURE | SERD 1775 |
| SPECIAL FEATURES | CONSISTS OF A WELDED STEEL ASSEMBLY; CIRCULAR BASE SUPPORTING A RING ON SIX CYLINDRICAL PEDESTALS, AND A LONG CYLINDER; FOUR TRIANGULAR SHAPED PLATES WELDED TO THE BASE AND THE CYLINDER OUTER SURFACE, TO PROVIDE STIFFENING TO THE ASSEMBLY; MOUNTING HOLES ARE INCORPORATED IN THE BASE AND RING; APPROX. 28.3000 IN. DIA.; 37.000 IN. HT. IN |
| FUNCTIONAL DESCRIPTION | USED TO DEAD LOAD TEST THE ADAPTER USED TO SUPPORT THE HIGH PRESSURE ROTOR AND STATOR MODULE |
| END ITEM IDENTIFICATION | F117-PW-100 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.