| CRITICALITY CODE JUSTIFICATION | CBBL |
| FUNCTIONAL DESCRIPTION | RECEIVES SIGNALS FROM VARIOUS ACFT COMPONENTS; PROVIDES PERFORMANCE SIGNALS TO ECS, OBIGGS, AND APU CONTROLLERS PROVIDES STATUS SIGNALS TO THE WCC,CAWS, AND MMP; DETECTS AND STORES FAULT DATA |
| END ITEM NAME | CARGO AIRCRAFT |
| END ITEM SOURCE | 88277 |
| FEATURES PROVIDED | ELECTROSTATIC SENSITIVE |
| JOINT ELECTRONICS TYPE DESIGNATION SYSTEM ITEM NAME | CONTROLLER,MANIFOLD FAILURE DETECTION |
| JOINT ELECTRONICS TYPE DESIGNATION SYSTEM ITEM TYPE NUMBER | DCU-283/A |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROLLER,MANIFOLD FAILURE DETECTION |
| PROPRIETARY CHARACTERISTICS | PACS |
| SPECIAL FEATURES | POWER-28 VDC; MOUNTING-ARINC 404A; INSTALLATION-AIRBORNE |
| UNPACKAGED UNIT LENGTH | 14.170 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 7.620 INCHES NOMINAL |
| USAGE DESIGN | DETECTION OF LEAKS IN PNEUMATIC DUCTING |