753212: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL STEM, bonnet_type: INSIDE SPRING, connection_type: THREADED INTERNAL PIPE FIRST END, connection_style: PLAIN,OPTIONAL END(PIPE) SECOND END, style_designator: ANGLE, thread_direction: RIGHT-HAND FIRST END. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-166-2356, 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 STEM |
| bonnet_type | INSIDE SPRING |
| connection_type | THREADED INTERNAL PIPE FIRST END |
| connection_style | PLAIN,OPTIONAL END(PIPE) SECOND END |
| style_designator | ANGLE |
| thread_direction | RIGHT-HAND FIRST END |
| features_provided | PRESSURE TIGHT OUTLET SIDE |
| disk_loading_method | SPRING |
| flow_control_device | PISTON |
| nominal_thread_size | 0.500 INCHES FIRST END IN |
| valve_operation_method | MANUAL |
| bonnet_attachment_method | THREADED |
| NSN | 2840-00-166-2356 |
| DESIGN TYPE | COMPRESSOR |
| HARDNESS RATING | 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| OVERALL LENGTH | 2.782 INCHES MINIMUM AND 2.791 INCHES MAXIMUM IN |
| OVERALL WIDTH | 1.160 INCHES MINIMUM AND 1.170 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| MATERIAL THICKNESS | 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN |
| SPECIAL FEATURES | TOLARANCE, FIT |
| END ITEM IDENTIFICATION | ENGINE MODEL TF33 |