2840PL0664279: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 52.850 INCHES MINIMUM AND 52.950 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 0.040 INCHES NOMINAL IN, special_features: T.O. 2J-F100-24, FIG 131, IN 26 IN, 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 2840-01-215-3550, 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 | 52.850 INCHES MINIMUM AND 52.950 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| stage_number | 2 |
| overall_length | 0.040 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-24, FIG 131, IN 26 IN |
| end_item_identification | ACFT ENG F100-PW-220/125B |
| engine_section_location | TURBINE |
| criticality_code_justification | ABMZ AND CZCJ AND CZBJ AND ABHP |
| material_document_and_classification | AMS5587 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-215-3550 |
| STAGE NUMBER | 2 |
| CRITICALITY CODE JUSTIFICATION | ABMZ AND CZCJ AND CZBJ AND ABHP |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5587 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 52.850 INCHES MINIMUM AND 52.950 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.040 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-24, FIG 131, IN 26 IN |
| END ITEM IDENTIFICATION | ACFT ENG F100-PW-220/125B |
| MATERIAL | NICKEL ALLOY OVERALL |