BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY BLADE, design_type: COMPRESSOR, overall_width: 1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN, overall_length: 3.081 INCHES MINIMUM AND 3.090 INCHES MAXIMUM IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, material_thickness: 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-767-8334, 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 | TITANIUM ALLOY BLADE |
| design_type | COMPRESSOR |
| overall_width | 1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN |
| overall_length | 3.081 INCHES MINIMUM AND 3.090 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| material_thickness | 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN |
| end_item_identification | TF33 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 2840-00-767-8334 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| OVERALL WIDTH | 1.212 INCHES MINIMUM AND 1.222 INCHES MAXIMUM IN |
| MATERIAL | TITANIUM ALLOY BLADE |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| OVERALL LENGTH | 3.081 INCHES MINIMUM AND 3.090 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM IN |
| DESIGN TYPE | COMPRESSOR |