07/30/19
Message Overview:
| DDG Reference: | CAS - 42 |
| Pilot Action (QRH): | AVNC 02-26 |
| System Description: | 34-33-00 |
| Schematic Diagram: | 34-33-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 34-33-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
There is a missing or invalid input of defog set point label from the Head-up Flight Display Computer (HFDC) to the Enhanced Vision System (EVS) heater controller when the EVS infrared sensor unit (ISU) is selected on.
Possible Causes:
- Head-Up Display (HUD) Computer (A250)
- LH Engine P20/T20 Temperature Sensor (TAT 1)
- RH Engine P20/T20 Temperature Sensor (TAT 2)
- Total Air Temperature (TAT) Probe 3
- EVS Heater Controller (A315)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
NOTE: CAIMS message 3000142IN - DEFOG FAULT/EVSHC/WRG may display when the CAS message is active.
Quick Links:
| Removal of the Data Acquisition Units (DAU) | AMM 31-42-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Data Acquisition Units (DAU) | AMM 31-42-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the MASTER WARNING/CAUTION Panel | AMM 31-52-13-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the MASTER WARNING/CAUTION Panel | AMM 31-52-13-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the Head-Up-Display (HUD) Computer | AMM 34-32-01-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the Head-Up-Display (HUD) Computer | AMM 34-32-01-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Access to CAIMS Bus Reader | AMM 45-45-00-970-824 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of EVS Infrared Window (IRW) | AMM 53-62-03-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of EVS Infrared Window (IRW) | AMM 53-62-03-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Access the PMAT CAIMS BUS Reader (from the PMAT Start Menu). Add the following signals:
- Micro Air Data Computer 1 - WSP 9 - STATIC AIR TEMPERATURE
- Micro Air Data Computer 2 - WSP 9 - STATIC AIR TEMPERATURE
- Micro Air Data Computer 3 - WSP 9 - STATIC AIR TEMPERATURE
- If there is a Static air temperature displayed for all three MADC and the values are the same or very close, go to step 3.
- If one of the values is missing or out of range, continue with next step.
- Perform a wiring check between the affected MADC and its associated TAT probe. Repair defective wiring if required or replace TAT probe.
- MADC 1 = P20/T20 on LH engine intake
- MADC 2 = P20/T20 on RH engine intake
- MADC 3 = TAT 3 on RH FWD fuselage
- Perform a wiring check between the HUD computer (A250) and the Master Warning/Caution panel (AP15) and the EVS Heater Controller (A315) as follows:
From To Result A250DP1-D3 AP15P2-D A315P1-W AP15P2-F NOTE: Make sure to check for short circuit to ground also on these wires.
- If wiring defects are found, repair defective wiring as required and do close out.
- If no defects are found, continue with next step.
- Perform a wiring check between the HUD computer (A250) and DAU 4 (A31) as follows:
From To Result A250EP1-G6 A31CP1-B2 A250EP1-H6 A31CP1-C2 - If wiring defects are found, repair defective wiring as required and do close out.
- If no defects are found, continue with next step.
- Perform a wiring check between the HUD computer (A250) and the MADCs as follows:
MADC 1
From To Result A250BP1-J1 A27P1-68 A250BP1-K1 A27P1-69 MADC 2
From To Result A250EP1-E1 A28P1-68 A250EP1-E2 A28P1-69 MADC 3
From To Result A250EP1-E4 A29P1-66 A250EP1-F4 A29P1-67 A250BP1-E6 A29P1-63 A250BP1-F6 A29P1-64 - If wiring defects are found, repair defective wiring as required and do close out.
- If no defects are found, continue with next step.
- Perform a wiring check between the EVS Heater Controller and the Infrared Window (IRW).
From To Result A315P1-BB A320P1-G A315P1-KK A320P1-C A315P1-a A320P1-A A315P1-Z A320P1-B A315P1-Y A320P1-J A315P1-X A320P1-K - If wiring defects are found, repair defective wiring as required and do close out.
- If no defects are found, continue with next step.
- Swap DAU 4 with DAU 2. Is the fault still present?
- If YES, continue with next step.
- If NO, replace defective DAU.
- Replace the IRW. Is the fault still present?
- If YES, continue with next step.
- If NO, do close out.
- Replace the EVS Heater Controller.Is the fault still present?
- If YES, continue with next step.
- If NO, do close out.
- Replace the HUD computer.
- Do close out.