4062387: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 16.130 INCHES MINIMUM AND 16.210 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: COMPRESSOR, overall_length: 1.419 INCHES MINIMUM AND 1.435 INCHES MAXIMUM IN, end_item_identification: F100/200/220 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-325-6164, 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 | 16.130 INCHES MINIMUM AND 16.210 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | COMPRESSOR |
| stage_number | 7 |
| overall_length | 1.419 INCHES MINIMUM AND 1.435 INCHES MAXIMUM IN |
| end_item_identification | F100/200/220 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5665 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-325-6164 |
| STAGE NUMBER | 7 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5665 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 16.130 INCHES MINIMUM AND 16.210 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.419 INCHES MINIMUM AND 1.435 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | F100/200/220 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.