4064208: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 56.860 INCHES MINIMUM AND 56.960 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 0.040 INCHES MINIMUM IN, special_features: T.O. 2J-F100-24, FIG 132, IND 7 AND 15, end_item_identification: ACFT ENG F100-PW-220/125B, engine_section_location: TURBINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-216-0448, 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 | 56.860 INCHES MINIMUM AND 56.960 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| stage_number | 1 |
| overall_length | 0.040 INCHES MINIMUM IN |
| special_features | T.O. 2J-F100-24, FIG 132, IND 7 AND 15 |
| end_item_identification | ACFT ENG F100-PW-220/125B |
| engine_section_location | TURBINE |
| criticality_code_justification | MATT AND CZBJ AND CZCJ AND ABHP AND ABMZ |
| material_document_and_classification | AMS5687 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-216-0448 |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | MATT AND CZBJ AND CZCJ AND ABHP AND ABMZ |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5687 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 56.860 INCHES MINIMUM AND 56.960 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.040 INCHES MINIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-24, FIG 132, IND 7 AND 15 |
| END ITEM IDENTIFICATION | ACFT ENG F100-PW-220/125B |
| MATERIAL | NICKEL ALLOY OVERALL |