9182M25P01: LOCK,COMPRESSOR BLADE,AIRCRAFT G.
LOCK,COMPRESSOR BLADE,AIRCRAFT G. Key specifications include material: STEEL, overall_width: 0.400 INCHES MINIMUM AND 0.406 INCHES MAXIMUM IN, overall_length: 0.321 INCHES NOMINAL IN, material_thickness: 0.190 INCHES MINIMUM AND 0.210 INCHES MAXIMUM IN, end_item_identification: AIRCRAFT ENGINE MODEL NO. TF-39, criticality_code_justification: AGAV.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-032-5863, 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 |
| stage_number | 2 |
| overall_width | 0.400 INCHES MINIMUM AND 0.406 INCHES MAXIMUM IN |
| overall_length | 0.321 INCHES NOMINAL IN |
| material_thickness | 0.190 INCHES MINIMUM AND 0.210 INCHES MAXIMUM IN |
| end_item_identification | AIRCRAFT ENGINE MODEL NO. TF-39 |
| criticality_code_justification | AGAV |
| NSN | 2840-01-032-5863 |
| STAGE NUMBER | 2 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 0.321 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.400 INCHES MINIMUM AND 0.406 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.190 INCHES MINIMUM AND 0.210 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | AIRCRAFT ENGINE MODEL NO. TF-39 |
| MATERIAL | STEEL |