DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: GLASS FIBER AND PLASTIC EPOXY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 1.000 INCHES NOMINAL IN, overall_height: 0.094 INCHES NOMINAL IN, overall_length: 2.880 INCHES NOMINAL IN, special_features: CUSHION IS BUNA NITRILE PER MIL-R-6855 CLASS A GRADE 70; WIPERS ARE BRONZE PER ASTM B584 ALLOY C93200; FIRST STAGE. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-590-6955, 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 | GLASS FIBER AND PLASTIC EPOXY OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_width | 1.000 INCHES NOMINAL IN |
| overall_height | 0.094 INCHES NOMINAL IN |
| overall_length | 2.880 INCHES NOMINAL IN |
| special_features | CUSHION IS BUNA NITRILE PER MIL-R-6855 CLASS A GRADE 70; WIPERS ARE BRONZE PER ASTM B584 ALLOY C93200; FIRST STAGE |
| style_designator | FLAT, RECTANGULAR |
| end_item_identification | LGM-118A PEACEKEEPER A |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | MIL-P-18177, TYPE GEB MIL SPEC SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-00-590-6955 |
| SPECIAL FEATURES | WAS DISK,AXIAL COMPRESSOR,TURBINEENGINE |
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J-75 AIRCRAFT ENGINE |