4071473: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 31.234 INCHES MINIMUM AND 31.254 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 1.910 INCHES MINIMUM AND 2.050 INCHES MAXIMUM IN, end_item_identification: F100PW0229 AIRCRAFT ENGINE, engine_section_location: TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-324-1156, 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 | 31.234 INCHES MINIMUM AND 31.254 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| stage_number | 4 |
| overall_length | 1.910 INCHES MINIMUM AND 2.050 INCHES MAXIMUM IN |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5707 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-324-1156 |
| STAGE NUMBER | 4 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5707 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 31.234 INCHES MINIMUM AND 31.254 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.910 INCHES MINIMUM AND 2.050 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.