4076318: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 19.680 INCHES MINIMUM AND 19.720 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, stage_number: 11, overall_length: 0.530 INCHES MINIMUM AND 0.560 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-24, FIG 139, IND 7A A.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-396-8877, 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 | 19.680 INCHES MINIMUM AND 19.720 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 11 |
| overall_length | 0.530 INCHES MINIMUM AND 0.560 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-24, FIG 139, IND 7A A |
| end_item_identification | F100/200 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | APGF AND CZBJ AND CZCJ AND ABHP AND ABMZ |
| material_document_and_classification | AMS5662 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-396-8877 |
| STAGE NUMBER | 11 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND ABHP AND ABMZ |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5662 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 19.680 INCHES MINIMUM AND 19.720 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.530 INCHES MINIMUM AND 0.560 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-24, FIG 139, IND 7A A |
| END ITEM IDENTIFICATION | F100/200 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.