4057120: DAMPER,TURBINE BLADE,AIRCRAFT TU.
DAMPER,TURBINE BLADE,AIRCRAFT TU. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 0.847 INCHES NOMINAL IN, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-124-0707, 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 OVERALL |
| stage_number | 2 |
| overall_length | 0.847 INCHES NOMINAL IN |
| end_item_identification | ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT F100-PW-229 (F15E, F16C/D); ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E) A |
| criticality_code_justification | AGAV |
| NSN | 2840-01-124-0707 |
| STAGE NUMBER | 2 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 0.847 INCHES NOMINAL IN |
| END ITEM IDENTIFICATION | ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT F100-PW-229 (F15E, F16C/D); ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E) A |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.