9645M18P01: LOCK,NOZZLE,TURBINE STATOR.
The LOCK,NOZZLE,TURBINE STATOR is a the manufacturer industrial component. Key specifications include overall_width: 0.495 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN, overall_length: 0.695 INCHES MINIMUM AND 0.720 INCHES MAXIMUM IN, end_item_identification: ENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE1A, criticality_code_justification: ABHP AND ABMK AND AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-003-9012, 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.
| overall_width | 0.495 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN |
| overall_length | 0.695 INCHES MINIMUM AND 0.720 INCHES MAXIMUM IN |
| end_item_identification | ENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE1A |
| criticality_code_justification | ABHP AND ABMK AND AGAV |
| NSN | 2840-01-003-9012 |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMK AND AGAV |
| OVERALL LENGTH | 0.695 INCHES MINIMUM AND 0.720 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.495 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | ENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE1A |