2191631: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 2.560 INCHES MINIMUM AND 2.566 INCHES MAXIMUM IN, end_item_identification: TF-30 AIRCRAFT ENGINE, engine_section_location: TURBINE, criticality_code_justification: AGAV, material_document_and_classification: PWA1007 MFR REF SINGLE MATERIAL RESPONSE OVERALL. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-356-4275, 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 |
| stage_number | 3 |
| overall_length | 2.560 INCHES MINIMUM AND 2.566 INCHES MAXIMUM IN |
| end_item_identification | TF-30 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | PWA1007 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-356-4275 |
| STAGE NUMBER | 3 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1007 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 2.560 INCHES MINIMUM AND 2.566 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| END ITEM IDENTIFICATION | TF-30 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.