6869693: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL CORROSION RESISTING BLADE, design_type: COMPRESSOR, hardness_rating: 34.0 BRINELL MINIMUM AND 38.0 BRINELL MAXIMUM BLADE, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: TF41 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-883-6020, 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 CORROSION RESISTING BLADE |
| design_type | COMPRESSOR |
| hardness_rating | 34.0 BRINELL MINIMUM AND 38.0 BRINELL MAXIMUM BLADE |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| end_item_identification | TF41 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | EMS59035 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 2840-00-883-6020 |
| DESIGN TYPE | COMPRESSOR |
| HARDNESS RATING | 34.0 BRINELL MINIMUM AND 38.0 BRINELL MAXIMUM BLADE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | EMS59035 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF41 AIRCRAFT ENGINE |
| MATERIAL | STEEL CORROSION RESISTING BLADE |
No substitute or cross-reference records for this part.