| GENERAL CHARACTERISTICS ITEM DESCRIPTION | THE OPERATING TEMPERATURE RANGE FOR THE TRANSDUCER SHALL BE -65F TO 160F |
| MATERIAL | STEEL AND ALUMINUM |
| III FUNCTIONAL DESCRIPTION | TRANSDUCER IS A PART OF THE FLIGHT CONTROL SYSTEM OF THE V-22 AIRCRAFT AND PROVIDES THE BASIC POSITION INPUTS TO THE FLIGHT CONTROL COMPUTER. THERE ARE 4 TRANSDUCERS IN EACH OF THE 4 AIRCRAFT CONTROL AXES |
| III PART NAME ASSIGNED BY CONTROLLING AGENCY | COCKPIT CONTROL POSITION TRANSDUCER |
| III SUPPLEMENTARY FEATURES | ALUMINUM ALLOYS USED IN CONSTRUCTION OF UNIT SHALL CONFORM TO REQUIREMENTS OF SD-572-1,PREFERRED ALLOY FOR ALL STRESSED ALUMINUM PARTS SHALL BE 7075-T73, HEAT TREATMENTS SHALL BE IAW MIL-H-6088 AND BAC 5602 |
| PROPRIETARY CHARACTERISTICS | PACS |
| OVERALL HEIGHT | 1.30 INCHES MAXIMUM |
| OVERALL LENGTH | 8.20 INCHES NOMINAL |
| SPECIAL FEATURES | STEEL ALLOYS USED IN CONSTRUCTION OF THE UNIT SHALL CONFORM TO THE REQUIREMENTS SD-572-1, HEAT TREATMENT SHALL BE IAW MIL-H-6875,BAC 5617 OR BAC 5619, CADMIUM PLATING SHALL CONFORM TO SPECIFICATION QQ-P-416,TYPE II,CLASS 2 |
| VOLTAGE IN VOLTS AND CURRENT TYPE | 0.24 AC |
| SURFACE TREATMENT | CADMIUM |