4076770: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 1.000 INCHES NOMINAL IN, overall_length: 3.140 INCHES NOMINAL IN, special_features: T.O. 2J-F100-54; STATORS RUN COUNTERCLOCKWISE; MATL IS COBALT, end_item_identification: F100PW0229 ACFT ENG, engine_section_location: COMBUSTION CHAMBER.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-323-9769, 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 |
| overall_width | 1.000 INCHES NOMINAL IN |
| overall_length | 3.140 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-54; STATORS RUN COUNTERCLOCKWISE; MATL IS COBALT |
| end_item_identification | F100PW0229 ACFT ENG |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | AGAV |
| material_document_and_classification | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-323-9769 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA647 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 3.140 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| SPECIAL FEATURES | T.O. 2J-F100-54; STATORS RUN COUNTERCLOCKWISE; MATL IS COBALT |
| END ITEM IDENTIFICATION | F100PW0229 ACFT ENG |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.