701608: DISK,TURBINE,AIRCRAFT GAS TURBIN.
DISK,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include material: ALUMINUM ALLOY OVERALL, end_item_identification: ADAPTER, FUEL, material_document_and_classification: QQ-C-465 ALLOY 442 FED SPEC SINGLE MATERIAL RESPONSE OVERALL, part_name_assigned_by_controlling_agency: PIN. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-006-2791, 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.
| material | ALUMINUM ALLOY OVERALL |
| end_item_identification | ADAPTER, FUEL |
| material_document_and_classification | QQ-C-465 ALLOY 442 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | PIN |
| NSN | 2840-00-006-2791 |
| FSC APPLICATION DATA | AIRCRAFT JET ENGINE,J57 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ROCKWELL C35-40 HARDNESS; 1.482-1.493 INCH THICKNESS; 19.825-19.835 INCH OD; 101 BLADE SLOTS EQUALLY SPACED AROUND OD; 16 0.4205-0.4235 INCH HOLES EQUALLY SPACED ON 8 INCH CENTERLINE RADIUS; 16 0.437-0.440 INCH HOLES EQUALLY SPACED ON 8.0 INCH CENTERLINE RADIUS IN |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.