9531M95G18: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include material: TITANIUM ALLOY OUTER CASE, design_type: AXIAL COMPRESSOR, overall_length: 21.310 INCHES MINIMUM AND 21.320 INCHES MAXIMUM IN, special_features: GOES ON THE FAN STATOR, end_item_identification: F110GE129 AIRCRAFT ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-322-6271, 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 OUTER CASE |
| design_type | AXIAL COMPRESSOR |
| overall_length | 21.310 INCHES MINIMUM AND 21.320 INCHES MAXIMUM IN |
| special_features | GOES ON THE FAN STATOR |
| end_item_identification | F110GE129 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS4928 ASSN STD 1ST MATERIAL RESPONSE AND AMS4935 ASSN STD 2ND MATERIAL RESPONSE OUTER CASE |
| NSN | 2840-01-322-6271 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD 1ST MATERIAL RESPONSE AND AMS4935 ASSN STD 2ND MATERIAL RESPONSE OUTER CASE |
| OVERALL LENGTH | 21.310 INCHES MINIMUM AND 21.320 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | GOES ON THE FAN STATOR |
| END ITEM IDENTIFICATION | F110GE129 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY OUTER CASE |