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Require immediate crew attention. These messages are accompanied by flashing master warning, triple chime attenson with or without voice message or dedicated tone. Require immediate crew awareness and future crew action may be required in the form of alternate system selection or performance limitation. These message are accompanied by flashing master caution and a single chime. Indicate safe or normal system operation which require crew awareness, over and above the dark cockpit philosophy. Indicate minor failures or reduction in systems capability, which require no crew action.

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01/14/20

Message Overview:

Fault Message:

H STAB MOT DR UNIT [CH2]/WRG FAULT

Fault Code:

27661262SX

Associated CAS Message:

STAB TRIM
(Caution)

SPLRS STAB BIT
(Advisory)

STAB CH1 FAIL
(Advisory)

Reporting LRU: Flight Control Unit (FCU) 2
System Description: 27-40-00
Schematic Diagram: 27-41-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 27-41-04 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

There is a Horizontal Motor Drive Unit failure or the interface wiring is defective between the Flight Control Unit (FCU) 2 and the Motor Drive Unit (MDU).

Possible Causes:

  • Pitch Trim Actuator Motor Motor Drive Unit (MDU) (A184)
  • Flight Control Unit (FCU) 2 (A66)
  • Pitch Trim Actuator (B44)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

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.

Quick Links:

Removal of the Pitch Trim Actuator AMM 27-41-09-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Pitch Trim Actuator AMM 27-41-09-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Pitch-Trim Actuator-Motor Drive-Unit AMM 27-41-17-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Pitch-Trim Actuator-Motor Drive-Unit AMM 27-41-17-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Flight-Control Units AMM 27-61-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Flight-Control Units AMM 27-61-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Swap FCU 2 with FCU 1 and check for the failure transfer over to Channel 1?

    1. If YES, replace FCU 2. Reset FCUs latched faults and do close out.
    2. If NO, continue with next step.

  2. Use Ground Support Equipment 27X-41-09 'MDU INVERTING HARNESS' if available. Confirm the failure with the inverting harness installed. If the MDU INVERTING HARNESS is not available, continue with step 3.

    1. If the fault is now on Channel 1, it means that the MDU CH 2 is defective. Replace the MDU and do close out.
    2. If the fault remains on Channel 2, the failure could be with the HSTA motor or the wiring interface. Continue with next step.

  3. Disconnect FCU 2 connector A66DP1 and A66BP1. Disconnect MDU connector A184P7. Perform a continuity check as follows:

    From To Result
    A66DP1-3H A184P7-37
    A66DP1-3J A184P7-23
    A66DP1-6G A184P7-6
    A66DP1-5K A184P7-7
    A66DP1-5J A184P7-8
    A66DP1-3G A184P7-24
    A66BP1-14F A184P7-28
    A66BP1-14E A184P7-29
    A66BP1-15F A184P7-16
    A66BP1-15E A184P7-17

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  4. Disconnect MDU connectors A184P7 and A184P6. Disconnect Pitch Trim Actuator connectors B44P4 and B44P3. Perform a continuity check as follows:

    From To Result
    A184P6-A B44P3-A
    A184P6-B B44P3-B
    A184P6-C B44P3-C
    A184P7-20 B44P4-13
    A184P7-19 B44P4-14
    A184P7-3 B44P4-12
    A184P7-4 B44P4-11
    A184P7-2 B44P4-26
    A184P7-1 B44P4-34
    A184P7-10 B44P4-32
    A184P7-25 B44P4-33

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  5. Swap HSTA motor 2 with motor 1. Is the fault still present on the same side?

    1. If YES, continue with next step.
    2. If NO, replace defective motor and do close out.

  6. Replace the MDU.
  7. Replace the Pitch Trim Actuator.
  8. Do close out.
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