PWA81683-2: FIXTURE,ENGINE MAINTENANCE,AIRCR.
FIXTURE,ENGINE MAINTENANCE,AIRCR. Key specifications include special_features: PRESSURE TEST, nominal_overall_width: 1.500 INCHES IN, functional_description: USED TO CHECK FOR LEAKAGE AROUND THE PLUG OF THE STARTER MESHING NOZZLE, nominal_overall_height: 3.562 INCHES IN, nominal_overall_length: 2.500 INCHES IN, end_item_identification: SUPPORT EQUIPMENT, F117-PW-100 AIRCRAFT ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 4920-01-411-1114, 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 | PRESSURE TEST |
| nominal_overall_width | 1.500 INCHES IN |
| functional_description | USED TO CHECK FOR LEAKAGE AROUND THE PLUG OF THE STARTER MESHING NOZZLE |
| nominal_overall_height | 3.562 INCHES IN |
| nominal_overall_length | 2.500 INCHES IN |
| end_item_identification | SUPPORT EQUIPMENT, F117-PW-100 AIRCRAFT ENGINE |
| reference_data_and_literature | SERD NO. 0134 |
| NSN | 4920-01-411-1114 |
| NOMINAL OVERALL WIDTH | 1.500 INCHES IN |
| NOMINAL OVERALL LENGTH | 2.500 INCHES IN |
| REFERENCE DATA AND LITERATURE | SERD NO. 0134 |
| NOMINAL OVERALL HEIGHT | 3.562 INCHES IN |
| SPECIAL FEATURES | PRESSURE TEST |
| FUNCTIONAL DESCRIPTION | USED TO CHECK FOR LEAKAGE AROUND THE PLUG OF THE STARTER MESHING NOZZLE |
| END ITEM IDENTIFICATION | SUPPORT EQUIPMENT, F117-PW-100 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.