PWA81575: FIXTURE,MACHINING,AIRCRAFT ENGIN.
FIXTURE,MACHINING,AIRCRAFT ENGIN. Key specifications include nominal_overall_height: 4.000 INCHES IN, end_item_identification: C-17 AIRCRAFT ENGINE F117-PW-100, nominal_overall_diameter: 22.000 INCHES IN, reference_data_and_literature: SERD NO.1398. This part is cataloged in the U.S.
Government catalog under NSN 4920-01-394-0375, 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 | FIXTURE,MACHINING - HIGH PRESSURECOMPRESSOR INLET GUIDE VANE INNER SHROUD. CONSISTS OF A STEEL BASE WITH TWELVE (12) ADJUSTABLE STEEL CLAMPS, ONE ALUMINUM RING CLAMP, AND TWO (2) PAIR OF DIAMOND PINS |
| functional_description | FIXTURE USED TO HOLD BOTH HALVES OF THE INLET GUIDE VANE INNER SHROUD SEGMENT ASSY'S DURING MACHINING OF THE TRUNION HOLES |
| nominal_overall_height | 4.000 INCHES IN |
| end_item_identification | C-17 AIRCRAFT ENGINE F117-PW-100 |
| nominal_overall_diameter | 22.000 INCHES IN |
| reference_data_and_literature | SERD NO.1398 |
| NSN | 4920-01-394-0375 |
| NOMINAL OVERALL DIAMETER | 22.000 INCHES IN |
| REFERENCE DATA AND LITERATURE | SERD NO.1398 |
| NOMINAL OVERALL HEIGHT | 4.000 INCHES IN |
| SPECIAL FEATURES | FIXTURE,MACHINING - HIGH PRESSURECOMPRESSOR INLET GUIDE VANE INNER SHROUD. CONSISTS OF A STEEL BASE WITH TWELVE (12) ADJUSTABLE STEEL CLAMPS, ONE ALUMINUM RING CLAMP, AND TWO (2) PAIR OF DIAMOND PINS |
| FUNCTIONAL DESCRIPTION | FIXTURE USED TO HOLD BOTH HALVES OF THE INLET GUIDE VANE INNER SHROUD SEGMENT ASSY'S DURING MACHINING OF THE TRUNION HOLES |
| END ITEM IDENTIFICATION | C-17 AIRCRAFT ENGINE F117-PW-100 |
No substitute or cross-reference records for this part.