9531M67G01: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 31.902 INCHES NOMINAL IN, material: STEEL OVERALL, overall_length: 2.088 INCHES MINIMUM AND 2.098 INCHES MAXIMUM IN, special_features: WAS CASE,TURBINE ROTOR,TURBINE ENGINE, material_thickness: 0.120 INCHES MINIMUM AND 0.130 INCHES MAXIMUM IN, end_item_identification: ACFT ENG F110. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-192-7479, 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.
| diameter | 31.902 INCHES NOMINAL IN |
| material | STEEL OVERALL |
| overall_length | 2.088 INCHES MINIMUM AND 2.098 INCHES MAXIMUM IN |
| special_features | WAS CASE,TURBINE ROTOR,TURBINE ENGINE |
| material_thickness | 0.120 INCHES MINIMUM AND 0.130 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG F110 |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-192-7479 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 31.902 INCHES NOMINAL IN |
| OVERALL LENGTH | 2.088 INCHES MINIMUM AND 2.098 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| MATERIAL THICKNESS | 0.120 INCHES MINIMUM AND 0.130 INCHES MAXIMUM IN |
| SPECIAL FEATURES | WAS CASE,TURBINE ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.