4070851: VANE,COMPRESSOR,AIRCRAFT GAS TUR.
VANE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: TITANIUM ALLOY VANE, design_type: AXIAL COMPRESSOR, overall_length: 8.827 INCHES NOMINAL IN, special_features: T.O. 2J-F100-54, blade_attachment_method: LOCK, end_item_identification: F100PW0229 AIRCRAFT ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-321-0701, 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 VANE |
| design_type | AXIAL COMPRESSOR |
| stage_number | 1 |
| overall_length | 8.827 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-54 |
| blade_attachment_method | LOCK |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE VANE |
| NSN | 2840-01-321-0701 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | LOCK |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE VANE |
| OVERALL LENGTH | 8.827 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY VANE |
No substitute or cross-reference records for this part.