674941: LOCK,COMPRESSOR BLADE,AIRCRAFT G.
LOCK,COMPRESSOR BLADE,AIRCRAFT G. Key specifications include material: NICKEL ALLOY, stage_number: 14, overall_width: 0.342 INCHES MINIMUM AND 0.349 INCHES MAXIMUM IN, overall_length: 0.810 INCHES MINIMUM AND 0.820 INCHES MAXIMUM IN, special_features: GOES ON THE REAR-ROTOR COMPRESSOR, material_thickness: 0.046 INCHES MINIMUM AND 0.051 INCHES MAXIMUM IN. This part is cataloged in the U.S.
Government catalog under NSN 5330-00-215-7267, 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 | NICKEL ALLOY |
| stage_number | 14 |
| overall_width | 0.342 INCHES MINIMUM AND 0.349 INCHES MAXIMUM IN |
| overall_length | 0.810 INCHES MINIMUM AND 0.820 INCHES MAXIMUM IN |
| special_features | GOES ON THE REAR-ROTOR COMPRESSOR |
| material_thickness | 0.046 INCHES MINIMUM AND 0.051 INCHES MAXIMUM IN |
| end_item_identification | J57 ACFT ENGINE |
| reference_data_and_literature | 2J-J57-14 |
| criticality_code_justification | AGAV |
| material_document_and_classification | PWA1038 ASSN STD SINGLE MATERIAL RESPONSE |
| NSN | 5330-00-215-7267 |