2840PL0696903: VANE,COMPRESSOR,AIRCRAFT GAS TUR.
VANE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: TITANIUM ALLOY VANE, design_type: AXIAL COMPRESSOR, overall_length: 4.721 INCHES MINIMUM AND 4.733 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-54; 4-9TH STAGES; 58UNITS PER ASSY; REAR COMPRESSOR,VARIABLE INLET, surface_treatment: NICKEL VANE, blade_attachment_method: PIN.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-321-4455, 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 |
| overall_length | 4.721 INCHES MINIMUM AND 4.733 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-54; 4-9TH STAGES; 58UNITS PER ASSY; REAR COMPRESSOR,VARIABLE INLET |
| surface_treatment | NICKEL VANE |
| blade_attachment_method | PIN |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| material_document_and_classification | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE VANE |
| surface_treatment_document_and_classification | AMS2433 ASSN STD SINGLE TREATMENT RESPONSE VANE |
| NSN | 2840-01-321-4455 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | AMS2433 ASSN STD SINGLE TREATMENT RESPONSE VANE |
| DESIGN TYPE | AXIAL COMPRESSOR |
| BLADE ATTACHMENT METHOD | PIN |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE VANE |
| OVERALL LENGTH | 4.721 INCHES MINIMUM AND 4.733 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-54; 4-9TH STAGES; 58UNITS PER ASSY; REAR COMPRESSOR,VARIABLE INLET |
| SURFACE TREATMENT | NICKEL VANE |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY VANE |
No substitute or cross-reference records for this part.