DISK,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, fsc_application_data: AIRCRAFT JET ENGINE,J57, engine_section_location: COMPRESSOR, material_document_and_classification: AMS 6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-006-5308, 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 | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| fsc_application_data | AIRCRAFT JET ENGINE,J57 |
| engine_section_location | COMPRESSOR |
| material_document_and_classification | AMS 6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-00-006-5308 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| MATERIAL | STEEL OVERALL |
| FSC APPLICATION DATA | AIRCRAFT JET ENGINE,J57 |
| SPECIAL FEATURES | STEEL,AMS 6415,ROCKWELL C35-40 HARDNESS,3.210-3.221 IN. THK,19.825-19.835 IN. OD,6.995-7.005 IN. ID,27 BLADE SLOTS EQUALLY SPACEDAROUND OD,SIXTEEN 0.437-0.440 IN. HOLES EQUALLY SPACED ON 8.000 IN.CENTERLINE RADIUS,THIRTY-TWO 0.101-0.113 IN. HOLES EQUALLY SPACED ON7.260 IN. CENTERLINE RADIUS,THIRTY-TWO SCALLOPS EQUALLY SPACED ON 7.260IN. CENTERLINE RADIUS IN |
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |