4082850: VANE,COMPRESSOR,AIRCRAFT GAS TUR.
VANE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 2.218 INCHES MINIMUM AND 2.308 INCHES MAXIMUM IN, overall_length: 10.540 INCHES MINIMUM AND 10.600 INCHES MAXIMUM IN, special_features: FRONT STATOR;VARIABLE INLET, end_item_identification: F100PW100 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-431-1568, 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 OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_width | 2.218 INCHES MINIMUM AND 2.308 INCHES MAXIMUM IN |
| overall_length | 10.540 INCHES MINIMUM AND 10.600 INCHES MAXIMUM IN |
| special_features | FRONT STATOR;VARIABLE INLET |
| end_item_identification | F100PW100 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | APGF AND CZBJ AND ABMK AND ABHP AND FEAT |
| material_document_and_classification | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-431-1568 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND ABMK AND ABHP AND FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 10.540 INCHES MINIMUM AND 10.600 INCHES MAXIMUM IN |
| OVERALL WIDTH | 2.218 INCHES MINIMUM AND 2.308 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | FRONT STATOR;VARIABLE INLET |
| END ITEM IDENTIFICATION | F100PW100 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.