3029T96P01: LOCK,TURBINE ROTOR BLADE,AIRCRAF.
LOCK,TURBINE ROTOR BLADE,AIRCRAF. Key specifications include material: STEEL, overall_width: 0.350 INCHES MINIMUM AND 0.360 INCHES MAXIMUM IN, overall_length: 0.900 INCHES MINIMUM AND 0.920 INCHES MAXIMUM IN, material_thickness: 0.036 INCHES MINIMUM AND 0.044 INCHES MAXIMUM IN, end_item_identification: ENGINE,ACFT,MODEL NO. J85GE-21, reference_data_and_literature: 2J-J85-94.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-005-0182, 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 | 1 |
| overall_width | 0.350 INCHES MINIMUM AND 0.360 INCHES MAXIMUM IN |
| overall_length | 0.900 INCHES MINIMUM AND 0.920 INCHES MAXIMUM IN |
| material_thickness | 0.036 INCHES MINIMUM AND 0.044 INCHES MAXIMUM IN |
| end_item_identification | ENGINE,ACFT,MODEL NO. J85GE-21 |
| reference_data_and_literature | 2J-J85-94 |
| criticality_code_justification | AGAV |
| NSN | 2840-01-005-0182 |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-J85-94 |
| OVERALL LENGTH | 0.900 INCHES MINIMUM AND 0.920 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.350 INCHES MINIMUM AND 0.360 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.036 INCHES MINIMUM AND 0.044 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | ENGINE,ACFT,MODEL NO. J85GE-21 |
| MATERIAL | STEEL |
No substitute or cross-reference records for this part.