PWA90111: FIXTURE,ENGINE MAINTENANCE,AIRCR.
FIXTURE,ENGINE MAINTENANCE,AIRCR. Key specifications include special_features: HIGH PRESSURE COMPRESSOR,EIGHTH STAGE; HOLDER TEST STRIP, functional_description: USED TO POSITION THE ALMEN N TEST STRIPS FOR THE AIRFOIL AND PLATFORM GLASS BEAD INTENSITY CHECK, nominal_overall_height: 6.000 INCHES IN, end_item_identification: SUPPORT EQUIPMENT,F117-PW-100 AIRCRAFT ENGINE, nominal_overall_diameter: 3.200 INCHES IN, reference_data_and_literature: SERD NO. 1877.
This part is cataloged in the U.S. Government catalog under NSN 4920-01-425-0615, 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 | HIGH PRESSURE COMPRESSOR,EIGHTH STAGE; HOLDER TEST STRIP |
| functional_description | USED TO POSITION THE ALMEN N TEST STRIPS FOR THE AIRFOIL AND PLATFORM GLASS BEAD INTENSITY CHECK |
| nominal_overall_height | 6.000 INCHES IN |
| end_item_identification | SUPPORT EQUIPMENT,F117-PW-100 AIRCRAFT ENGINE |
| nominal_overall_diameter | 3.200 INCHES IN |
| reference_data_and_literature | SERD NO. 1877 |
| NSN | 4920-01-425-0615 |
| NOMINAL OVERALL DIAMETER | 3.200 INCHES IN |
| REFERENCE DATA AND LITERATURE | SERD NO. 1877 |
| NOMINAL OVERALL HEIGHT | 6.000 INCHES IN |
| SPECIAL FEATURES | HIGH PRESSURE COMPRESSOR,EIGHTH STAGE; HOLDER TEST STRIP |
| FUNCTIONAL DESCRIPTION | USED TO POSITION THE ALMEN N TEST STRIPS FOR THE AIRFOIL AND PLATFORM GLASS BEAD INTENSITY CHECK |
| END ITEM IDENTIFICATION | SUPPORT EQUIPMENT,F117-PW-100 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.