07/17/19
Message Overview:
| DDG Reference: | None |
| Pilot Action (QRH): | ABNORM 8-4 |
| System Description: | 27-41-00 |
| Schematic Diagram: | 27-41-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 27-41-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
FCU does not receive the Mach data. The Mach trim function is lost and will not adjust the pitch when there is Mach changes. On ground, this message also occurs with the failure of two pitch-trim position-transducers.
Possible Causes:
- At least two MADCs are defective
- Mach data is invalid (Mach Transducer or IESI defective)
- HST control angle is invalid (electrical or mechanical failure of one HST RVDT)
- Pitch-Trim Actuator Electrical-Module
- One FCU is defective
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter:To support a NFF technical investigation please fill out this Questionaire and send it to your FSR if you are replacing an Flight Control Unit (FCU).
Quick Links:
| Removal of FCU | AMM 27-61-05-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of FCU | AMM 27-61-05-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of Pitch Trim Actuator | AMM 27-41-09-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of Pitch Trim Actuator | AMM 27-41-09-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of Micro Air Data Computers | AMM 34-11-09-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of Micro Air Data Computers | AMM 34-11-09-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair | SPM 20-12-10 [ Global Express ] [ G5000 ] [Global XRS ] |
Troubleshooting Recommendations:
- Select related CAIMS message below: