10/22/25
Message Overview:
Message Name:
HST MDU[CH1]/MOTOR #1/WRG FAULT
Message Code:
27662321SX
Associated CAS:
| Reporting LRU: | Motor Drive Unit (MDU) |
| System Description: | 27-40-00 - Horizontal Stabilizer |
| Schematic Diagram: | [ Global Express ] [ G5000 ] [ Global XRS ] SSM 27-41-00-101 Pitch Trim System - Horizontal Stabilizer Pitch Trim System - Electrical Schematic |
| Wiring Diagram: | [ Global Express ] [ G5000 ] [ Global XRS ] WM 27-41-00-02 - Horizontal Stabilizer Pitch System - Control Actuation [ Global Express ] [ G5000 ] [ Global XRS ] WM 27-41-00-04 - Horizontal Stabilizer Pitch System - Control Actuation |
Message Description:
There is a problem related to:
- Motor Drive Unit (MDU) fault bit status failure
- SPOST failures caused by incorrect velocity-feedback or brake-hold test-current feedback failure
- Horizontal Stab Trim (HST) Motor-Brake coil failure
Possible Causes:
- Pitch Trim Actuator Motor Drive Unit (MDU) (A184)
- Pitch-Trim Actuator (B44)
- Flight Control Unit (FCU) 1 (A65)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Full Throttle Blog/Forum Articles/Infoservice/Newsletter: None
Flight Operation Notifications Manual (FONM): None
NOTES:
- This fault may sometime be cleared by performing the flight control system reset procedure. If the message comes back more then once within 10 flight legs, troubleshooting is required.
- The status of the of the pitch trim system can verify in CAIMS:
- SYSTEM DIAG
- 27-00 FLIGHT CONTROLS
- FLIGHT CONTROL UNIT #1
- LRU TEST
- DISPLAY ADVANCED EFCS DATA
- Go to page 5 of 8
Quick Links:
| Standard Aircraft Configuration for Maintenance | [ G5000 ] [ Global Express ] [ Global XRS ] AMM12-00-00-867-801 |
| Connect Electrical Power to the Aircraft | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-861-801 |
| Electrical/Electronic Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-801 |
| Electrostatic Discharge Safety Precautions | [ G5000 ] [ Global Express ] [ Global XRS ] AMM24-00-00-910-802 |
| Removal of the Pitch Trim Actuator | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-41-09-000-801 |
| Installation of the Pitch Trim Actuator | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-41-09-400-801 |
| Removal of the Pitch Trim Actuator-Motor | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-41-13-000-801 |
| Installation of the Pitch Trim Actuator-Motor | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-41-13-400-801 |
| Removal of the Pitch-Trim Actuator-Motor Drive-Unit | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-41-17-000-801 |
| Installation of the Pitch-Trim Actuator-Motor Drive-Unit | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-41-17-400-801 |
| Removal of the Flight-Control Units | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-61-05-000-801 |
| Installation of the Flight-Control Units | [ G5000 ] [ Global Express ] [ Global XRS ] AMM27-61-05-400-801 |
Troubleshooting Recommendations:
- Interchange FCU 1 with FCU 2.
- If system checks are good, replace FCU 1. Reset FCUs latched faults and do close out.
- If fault remains, continue with next step.
- Interchange MDU Channel, if the use of the Ground Support Equipment 27X-41-09 "MDU INVERTING HARNESS" can be done to isolate the fault to the MDU or pitch trim Actuator motor.
- If system checks are good, replace defective MDU Channel and do close out.
- If fault remains, remove ground support equipment and continue with next step.
- Perform wiring checks MDU (A184) and FCU 1 (A65).
From To Result A184P3-37 A65DP1-3H A184P3-23 A65DP1-3J A184P3-6 A65DP1-6G A184P3-7 A65DP1-5K A184P3-8 A65DP1-5J A184P3-24 A65DP1-3G - If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Interchange pitch trim actuator motors. Is the fault still present?
- If NO, replace pitch trim actuator motor 1 and do close out.
- If YES, continue with next step
- Perform wiring checks between MDU (A184) and HSTA (B44).
From To Result A184P2-A B44P1-A A184P2-B B44P1-B A184P2-C B44P1-C A184P3-1 B44P2-34 A184P3-2 B44P2-26 A184P3-3 B44P2-12 A184P3-4 B44P2-11 A184P3-10 B44P2-32 A184P3-25 B44P2-33 A184P3-19 B44P2-14 A184P3-20 B44P2-13 - If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Perform wiring checks between FCU 1(A65) and HSTA (B44)
From To Result A65EP1-14J B44P2-8 A65EP1-15J B44P2-9 A65BP1-14C B44P2-6 A65BP1-15C B44P2-5 NOTE: Make sure wiring checked for short circuit to ground or shield. If high resistance is measured, check all disconnects along the link for bent, damaged or unlocked pins.
- If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Replace MDU and do close out.