P203P07: VANE,COMPRESSOR,AIRCRAFT GAS TUR.
VANE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F110-14, FIG 62, blade_attachment_method: PIN, end_item_identification: F110 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: HIGH PRESSURE COMPRESSOR, criticality_code_justification: CZBJ AND CZCJ AND BGLW AND FEAT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-435-8550, 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.
| design_type | AXIAL COMPRESSOR |
| stage_number | 3 |
| special_features | T.O. 2J-F110-14, FIG 62 |
| blade_attachment_method | PIN |
| end_item_identification | F110 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | HIGH PRESSURE COMPRESSOR |
| criticality_code_justification | CZBJ AND CZCJ AND BGLW AND FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME ON DWG VANE,COMPRESSOR STATOR |
| NSN | 2840-01-435-8550 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND CZCJ AND BGLW AND FEAT |
| BLADE ATTACHMENT METHOD | PIN |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F110-14, FIG 62 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME ON DWG VANE,COMPRESSOR STATOR |
| END ITEM IDENTIFICATION | F110 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.