4074839-02: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 18.180 INCHES NOMINAL IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.049 INCHES MINIMUM AND 0.050 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-54, end_item_identification: F100PW0229 AIRCRAFT ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-323-9765, 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.
| diameter | 18.180 INCHES NOMINAL IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 0.049 INCHES MINIMUM AND 0.050 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-54 |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5699 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-323-9765 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5699 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 18.180 INCHES NOMINAL IN |
| OVERALL LENGTH | 0.049 INCHES MINIMUM AND 0.050 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.