572108: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
Mechanisms supplied with rocker plates, to be equipped with support frames and surround plates. 2 modules. Key specifications include material: TITANIUM ALLOY BLADE, hole_type: DRILLED, head_style: HEXAGON, design_type: COMPRESSOR, head_height: 0.109 INCHES MINIMUM AND 0.141 INCHES MAXIMUM IN, thread_class: 3A A.
This part is cataloged in the U.S. Government catalog under NSN 2840-00-927-8343, 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 BLADE |
| hole_type | DRILLED |
| head_style | HEXAGON |
| design_type | COMPRESSOR |
| head_height | 0.109 INCHES MINIMUM AND 0.141 INCHES MAXIMUM IN |
| thread_class | 3A A |
| hole_diameter | 0.047 INCHES NOMINAL IN |
| hole_quantity | 1 |
| overall_width | 1.198 INCHES NOMINAL IN |
| thread_length | 0.185 INCHES MINIMUM AND 0.210 INCHES MAXIMUM IN |
| overall_length | 2.962 INCHES NOMINAL IN |
| fastener_length | 0.335 INCHES MINIMUM AND 0.340 INCHES MAXIMUM IN |
| NSN | 2840-00-927-8343 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 2.962 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.198 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| MATERIAL THICKNESS | 0.272 INCHES NOMINAL IN |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY BLADE |
No substitute or cross-reference records for this part.