740809: DISK,TURBINE,AIRCRAFT GAS TURBIN.
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 part is cataloged in the U.S.
Government catalog under NSN 2840-00-005-6777, 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 | 2840-00-005-6777 |
| 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 | STEEL,AMS 6415,ROCKWELL C35-40 HARDNESS,1.354-1.365 IN. THK,20.017-20.027 IN. OD,11.995-12.005 IN. ID,103 BLADE SLOTS EQUALLYSPACED AROUND OD,SIXTEEN 0.437-0.440 IN. HOLES EQUALLY SPACED ON 8.000IN. CENTERLINE RADIUS,32 SCALLOPS EQUALLY SPACED ON 7.260 IN.CENTERLINE RADIUS,THIRTY-TWO 0.108-0.113 IN. HOLES EQUALLY SPACED ON7.260 IN. CENTERLINE RADIUS IN |
| MATERIAL | STEEL OVERALL |