ROTOR,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY OVERALL, hole_type: DRILLED, head_style: DOUBLE HEXAGON W/HOLE, head_height: 0.320 INCHES MINIMUM AND 0.340 INCHES MAXIMUM IN, thread_class: 3A A, hole_diameter: 0.070 INCHES NOMINAL IN. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-076-4208, 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.
| material | TITANIUM ALLOY OVERALL |
| hole_type | DRILLED |
| head_style | DOUBLE HEXAGON W/HOLE |
| head_height | 0.320 INCHES MINIMUM AND 0.340 INCHES MAXIMUM IN |
| thread_class | 3A A |
| hole_diameter | 0.070 INCHES NOMINAL IN |
| hole_quantity | 4 |
| thread_length | 0.552 INCHES MINIMUM AND 0.572 INCHES MAXIMUM IN |
| fastener_length | 0.552 INCHES MINIMUM AND 0.572 INCHES MAXIMUM IN |
| thread_direction | RIGHT-HAND |
| features_provided | FINISHED HEAD |
| width_between_flats | 0.304 INCHES MINIMUM AND 0.313 INCHES MAXIMUM IN |
| NSN | 2840-00-076-4208 |
| DIAMETER | 13.582 INCHES MINIMUM AND 13.587 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | ACFT ENG J69 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| SPECIAL FEATURES | ORIGINAL NAME COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE |
| MATERIAL | STEEL OVERALL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5355 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ENGINE SECTION LOCATION | COMPRESSOR |
| DESIGN TYPE | AXIAL COMPRESSOR |
| OVERALL LENGTH | 7.152 INCHES NOMINAL IN |