1476AS232-1: LEVER,REMOTE CONTROL.
The LEVER,REMOTE CONTROL is a the manufacturer industrial component. Key specifications include material: STEEL, style_designator: OFFSET, CLEVIS LINK END, link_end_thickness: 0.450 INCHES NOMINAL IN, end_item_identification: T400-CP400 FOR H1 HELICOPTER, material_document_and_classification: QQ-S-7863, CLASS 304 FED SPEC SINGLE MATERIAL RESPONSE, part_name_assigned_by_controlling_agency: LEVER ENGINE CONTROL,TIE ROD ASSYTURBOSHAFT ENGINE TEST SYSTEM. This part is cataloged in the U.S.
Government catalog under NSN 3040-01-443-8488, 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 | STEEL |
| style_designator | OFFSET, CLEVIS LINK END |
| link_end_thickness | 0.450 INCHES NOMINAL IN |
| end_item_identification | T400-CP400 FOR H1 HELICOPTER |
| material_document_and_classification | QQ-S-7863, CLASS 304 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | LEVER ENGINE CONTROL,TIE ROD ASSYTURBOSHAFT ENGINE TEST SYSTEM |
| center_to_center_distance_between_link_and_shaft_holes | 2.000 INCHES NOMINAL IN |
| NSN | 3040-01-443-8488 |
| LINK END THICKNESS | 0.450 INCHES NOMINAL IN |
| STYLE DESIGNATOR | OFFSET, CLEVIS LINK END |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-S-7863, CLASS 304 FED SPEC SINGLE MATERIAL RESPONSE |
| CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.000 INCHES NOMINAL IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | LEVER ENGINE CONTROL,TIE ROD ASSYTURBOSHAFT ENGINE TEST SYSTEM |
| END ITEM IDENTIFICATION | T400-CP400 FOR H1 HELICOPTER |
| MATERIAL | STEEL |
No substitute or cross-reference records for this part.