701979: CASE,FAN,AIRCRAFT GAS TURBINE EN.
CASE,FAN,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 7.280 INCHES NOMINAL IN, material: STEEL OVERALL, overall_length: 7.880 INCHES MINIMUM AND 7.940 INCHES MAXIMUM IN, end_item_identification: J-69 AIRCRAFT ENGINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-117-4893, 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.
| diameter | 7.280 INCHES NOMINAL IN |
| material | STEEL OVERALL |
| overall_length | 7.880 INCHES MINIMUM AND 7.940 INCHES MAXIMUM IN |
| end_item_identification | J-69 AIRCRAFT ENGINE |
| criticality_code_justification | AGAV |
| NSN | 2840-00-117-4893 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG 4, IND 3, 2J-TF33-34, FIG 4, IND 1 |
| ENGINE SECTION LOCATION | FAN |
| SPECIAL FEATURES | USED ON THE FRONT CASE COMPRESSOR ROTOR, FAN; SUPERSEDES P/N 433477, 506262, 618962; SUPERSEDED BY P/N 672345 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CASE AND VANE ASSEMBLY,COMPRESSOR,STATOR |
| END ITEM IDENTIFICATION | TF33-PW-3/5/9/103 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.