1522M85G01: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include diameter: 30.180 INCHES MINIMUM AND 30.220 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 2.475 INCHES NOMINAL IN, blade_attachment_method: SLOT, end_item_identification: ACFT ENG F110. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-347-0820, 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 | 30.180 INCHES MINIMUM AND 30.220 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 1 |
| overall_length | 2.475 INCHES NOMINAL IN |
| blade_attachment_method | SLOT |
| end_item_identification | ACFT ENG F110 |
| engine_section_location | LOW PRESSURE TURBINE |
| material_document_and_classification | AMS 5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-347-0820 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| BLADE ATTACHMENT METHOD | SLOT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 30.180 INCHES MINIMUM AND 30.220 INCHES MAXIMUM IN |
| OVERALL LENGTH | 2.475 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| MATERIAL | STEEL OVERALL |