2840PL0696912: FLAMEHOLDER,AFTERBURNER,TURBINE.
FLAMEHOLDER,AFTERBURNER,TURBINE. Key specifications include material: NICKEL ALLOY FLAMEHOLDER, overall_length: 7.855 INCHES NOMINAL IN, special_features: HEATREAT; T.O. 2J-F100-54, end_item_identification: F100PW0229 AIRCRAFT ENGINE, engine_section_location: AFTERBURNER, criticality_code_justification: AGAV.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-323-4310, 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 FLAMEHOLDER |
| overall_length | 7.855 INCHES NOMINAL IN |
| special_features | HEATREAT; T.O. 2J-F100-54 |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | AFTERBURNER |
| criticality_code_justification | AGAV |
| material_document_and_classification | PWA1165 ASSN STD SINGLE MATERIAL RESPONSE FLAMEHOLDER |
| NSN | 2840-01-323-4310 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1165 ASSN STD SINGLE MATERIAL RESPONSE FLAMEHOLDER |
| OVERALL LENGTH | 7.855 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | AFTERBURNER |
| SPECIAL FEATURES | HEATREAT; T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY FLAMEHOLDER |