596-3-10: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL COMP H11 OVERALL, head_style: SPLINE DRIVE SHEAR HEAD, grip_length: 0.615 INCHES MINIMUM AND 0.635 INCHES MAXIMUM IN, head_height: 0.140 INCHES NOMINAL IN, thread_class: 3A A, grip_diameter: 0.1885 INCHES MINIMUM AND 0.1894 INCHES MAXIMUM IN. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-872-0663, 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 | STEEL COMP H11 OVERALL |
| head_style | SPLINE DRIVE SHEAR HEAD |
| grip_length | 0.615 INCHES MINIMUM AND 0.635 INCHES MAXIMUM IN |
| head_height | 0.140 INCHES NOMINAL IN |
| thread_class | 3A A |
| grip_diameter | 0.1885 INCHES MINIMUM AND 0.1894 INCHES MAXIMUM IN |
| thread_length | 0.298 INCHES MINIMUM AND 0.348 INCHES MAXIMUM IN |
| surface_finish | 32.0 MICROINCHES THREADS |
| fastener_length | 0.933 INCHES MINIMUM AND 0.963 INCHES MAXIMUM IN |
| thread_direction | RIGHT-HAND |
| surface_treatment | CADMIUM OVERALL |
| head_minor_diameter | 0.383 INCHES MINIMUM AND 0.389 INCHES MAXIMUM IN |
| NSN | 2840-00-872-0663 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1202 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| OVERALL LENGTH | 2.410 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.506 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| MATERIAL THICKNESS | 0.415 INCHES NOMINAL IN |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF30 ACFT ENGINE |
| MATERIAL | TITANIUM ALLOY BLADE |
No substitute or cross-reference records for this part.