21C6208G01: FIXTURE,MACHINING,AIRCRAFT ENGIN.
FIXTURE,MACHINING,AIRCRAFT ENGIN. Key specifications include special_features: STEEL, nominal_overall_width: 13.000 INCHES IN, functional_description: USED DURING REPAIR/MAINTENANCE OF COMPRESSOR REAR SPOOL, nominal_overall_height: 8.000 INCHES IN, nominal_overall_length: 14.000 INCHES IN, end_item_identification: J85-GE-21/-21A TURBOJET ENGINE AGE. A.
This part is cataloged in the U.S. Government catalog under NSN 4920-01-089-9937, 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 | STEEL |
| nominal_overall_width | 13.000 INCHES IN |
| functional_description | USED DURING REPAIR/MAINTENANCE OF COMPRESSOR REAR SPOOL |
| nominal_overall_height | 8.000 INCHES IN |
| nominal_overall_length | 14.000 INCHES IN |
| end_item_identification | J85-GE-21/-21A TURBOJET ENGINE AGE. A |
| NSN | 4920-01-089-9937 |
| NOMINAL OVERALL WIDTH | 13.000 INCHES IN |
| NOMINAL OVERALL LENGTH | 14.000 INCHES IN |
| NOMINAL OVERALL HEIGHT | 8.000 INCHES IN |
| SPECIAL FEATURES | STEEL |
| FUNCTIONAL DESCRIPTION | USED DURING REPAIR/MAINTENANCE OF COMPRESSOR REAR SPOOL |
| END ITEM IDENTIFICATION | J85-GE-21/-21A TURBOJET ENGINE AGE. A |
No substitute or cross-reference records for this part.