6895382: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL BLADE, design_type: COMPRESSOR, overall_length: 7.030 INCHES MINIMUM AND 7.040 INCHES MAXIMUM IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: TF41 ENG, engine_section_location: LOW PRESSURE COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-064-8521, 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 BLADE |
| design_type | COMPRESSOR |
| stage_number | 2 |
| overall_length | 7.030 INCHES MINIMUM AND 7.040 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| end_item_identification | TF41 ENG |
| engine_section_location | LOW PRESSURE COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | EMS73168 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 2840-01-064-8521 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | EMS73168 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| OVERALL LENGTH | 7.030 INCHES MINIMUM AND 7.040 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF41 ENG |
| MATERIAL | STEEL BLADE |
No substitute or cross-reference records for this part.