9685M85G62: ROTOR,COMPRESSOR,AIRCRAFT GAS TU.
ROTOR,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include diameter: 18.130 INCHES MINIMUM AND 18.134 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 47.991 INCHES MINIMUM AND 48.023 INCHES MAXIMUM IN, special_features: ORIGINAL NAME COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE, end_item_identification: ACFT ENG TF-39. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-176-3386, 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 | 18.130 INCHES MINIMUM AND 18.134 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 47.991 INCHES MINIMUM AND 48.023 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE |
| end_item_identification | ACFT ENG TF-39 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-00-176-3386 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 18.130 INCHES MINIMUM AND 18.134 INCHES MAXIMUM IN |
| OVERALL LENGTH | 47.991 INCHES MINIMUM AND 48.023 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG TF-39 |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.