4076390: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 7.712 INCHES MINIMUM AND 7.716 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 3.645 INCHES MINIMUM AND 3.655 INCHES MAXIMUM IN, special_features: 10 HOLES EQ SP 0.434-0.443; 2ND END O/A DIA. 6.570-6.580, end_item_identification: F100PW0229 ENGINE/CORE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-320-5343, 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 | 7.712 INCHES MINIMUM AND 7.716 INCHES MAXIMUM IN |
| material | TITANIUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 3 |
| overall_length | 3.645 INCHES MINIMUM AND 3.655 INCHES MAXIMUM IN |
| special_features | 10 HOLES EQ SP 0.434-0.443; 2ND END O/A DIA. 6.570-6.580 |
| end_item_identification | F100PW0229 ENGINE/CORE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | PWA1202 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-320-5343 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1202 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 7.712 INCHES MINIMUM AND 7.716 INCHES MAXIMUM IN |
| OVERALL LENGTH | 3.645 INCHES MINIMUM AND 3.655 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | 10 HOLES EQ SP 0.434-0.443; 2ND END O/A DIA. 6.570-6.580 |
| END ITEM IDENTIFICATION | F100PW0229 ENGINE/CORE |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.