414210: DISK,COMPRESSOR,AIRCRAFT GAS TUR.
DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 21.034 INCHES MINIMUM AND 21.044 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, hardness_rating: 35.0 ROCKWELL C MINIMUM AND 40.0 ROCKWELL C MAXIMUM OVERALL, special_features: ORIGINAL NAME DISK,AXIAL COMPRESSOR,TURBINE ENGINE, end_item_identification: ACFT ENG TF33. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-806-7721, 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 | 21.034 INCHES MINIMUM AND 21.044 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| hardness_rating | 35.0 ROCKWELL C MINIMUM AND 40.0 ROCKWELL C MAXIMUM OVERALL |
| special_features | ORIGINAL NAME DISK,AXIAL COMPRESSOR,TURBINE ENGINE |
| end_item_identification | ACFT ENG TF33 |
| engine_section_location | COMPRESSOR |
| material_document_and_classification | AMS 6304 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-00-806-7721 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| HARDNESS RATING | 35.0 ROCKWELL C MINIMUM AND 40.0 ROCKWELL C MAXIMUM OVERALL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6304 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 21.034 INCHES MINIMUM AND 21.044 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME DISK,AXIAL COMPRESSOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |
| MATERIAL | STEEL OVERALL |