BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL BLADE, body_width: 0.985 INCHES MINIMUM AND 1.515 INCHES MAXIMUM IN, body_height: 0.485 INCHES MINIMUM AND 0.515 INCHES MAXIMUM IN, body_length: 1.485 INCHES MINIMUM AND 1.515 INCHES MAXIMUM IN, design_type: COMPRESSOR, body_material: METAL. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-947-7114, 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 BLADE |
| body_width | 0.985 INCHES MINIMUM AND 1.515 INCHES MAXIMUM IN |
| body_height | 0.485 INCHES MINIMUM AND 0.515 INCHES MAXIMUM IN |
| body_length | 1.485 INCHES MINIMUM AND 1.515 INCHES MAXIMUM IN |
| design_type | COMPRESSOR |
| body_material | METAL |
| overall_width | 1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN |
| inclosure_type | HERMETICALLY SEALED |
| overall_height | 0.875 INCHES NOMINAL IN |
| overall_length | 3.072 INCHES MINIMUM AND 3.081 INCHES MAXIMUM IN |
| hardness_rating | 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| NSN | 2840-00-947-7114 |
| MATERIAL THICKNESS | 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN |
| DESIGN TYPE | COMPRESSOR |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5616 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| HARDNESS RATING | 32.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM BLADE |
| OVERALL WIDTH | 1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | ENGINE MODEL J57 |
| OVERALL LENGTH | 3.072 INCHES MINIMUM AND 3.081 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| MATERIAL | STEEL BLADE |