4076424: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 19.700 INCHES MINIMUM AND 19.740 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, stage_number: 10, overall_length: 0.360 INCHES MINIMUM AND 0.390 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-24, FIG 138, IND 13A A.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-396-8876, 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 | 19.700 INCHES MINIMUM AND 19.740 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 10 |
| overall_length | 0.360 INCHES MINIMUM AND 0.390 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-24, FIG 138, IND 13A A |
| end_item_identification | F100/200 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | ABHP AND ABMZ AND CZBJ AND CZCJ |
| material_document_and_classification | AMS5662 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-396-8876 |
| STAGE NUMBER | 10 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND CZBJ AND CZCJ |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5662 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 19.700 INCHES MINIMUM AND 19.740 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.360 INCHES MINIMUM AND 0.390 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-24, FIG 138, IND 13A A |
| END ITEM IDENTIFICATION | F100/200 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.