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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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09/13/19

Message Overview:

Fault Message:

APU SHUT DOWN - OVERSPEED

Fault Code:

4960125APU

Associated CAS:

APU OVERSPEED
(Warning)

Reporting LRU: Full Authority Digital Engine (Electronic) Control (FADEC)
System Description: 49-60-00
Schematic Diagram: 49-61-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 49-12-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]
49-61-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

An Auxiliary Power Unit (APU) shut-down occurred, because of over speed. APU speed was greater than 106%. Automatic shut-down will occur on ground or in flight.

Fault See * below Description
FADEC FAILURE ECU internal failure (CPU, watchdog timer, O/S circuit failure, loss of O/S protection, etc.).
O/SPD (Hardware/Software) overspeed circuits tripped (at 106%).
LOSS OF SPEED Both monopoles failed.
LOSS OF O/SPD FADEC overspeed circuit/FCU fuel output solenoid failed.
OVERTEMP * EGT limit exceeded duringi) startii) on-speed operation
FIRE EMERG * Fire signal is received by the FADEC.
REVERSE FLOW * T2 temperature limit (176.6 °C/350 °F) has been exceeded for 5 seconds.
HIGH OIL TEMP * Oil temp limit of >148.9 °C exceeded for 10 seconds.
LOW OIL PRESS * Oil pressure has fallen below lower limit of 30 psig for 15 seconds, with RPM >95%.
LOSS OF EGT DETECTION * Both EGT thermocouples have failed.
NOTE: In Essential Mode, FADEC programs an EGT of 260 °C to maintain the APU running.
NO FLAME EGT rise has not been detected within 17 seconds of fuel solenoid being commanded open by FADEC, or RPM >18% for 5 seconds.
NO ACCEL Acceleration is <0.05% of the prescheduled rate (normal acceleration is 2.5% per second).
SLOW SPEED Starter timer expired - APU RPM >5% and less than starter cut-out for 30 seconds.
UNDER SPEED * Speed has reached 100%, then drops below 80% for 5 seconds.
NO CRANK RPM does not rise above 5% within:a) 2 seconds when oil temp is warmer than minus 23 °C, orb) 50 seconds when oil temp is minus 23 °C or lower.
INLET DOOR Inlet door position indicates closed 30 seconds before starter engagement, or 600 msecs. after starter engagement.
LOSS OF DC POWER Loss of 28 VDC power for 200 milliseconds.
LOP SW FAIL * Oil pressure switch has failed open when RPM is <7%.
NOTE: This switch is normally closed during prestart BITE.
FALLBACK APU drop below 25% RPM after starter cut-out
APU GCU HIGH OIL TEMP * APU Generator oil temperature above 215 °C

NOTE: An asterisk mark (*) in any row above means that the automatic protection shut-down on that row is inhibited if the associated fault occurs in flight. The respective CAS message, or an advisory message reading APU FAULT will be displayed in the CAS window and the APU will not shut down automatically in flight. However the pilot may select to shut-down the APU manually by placing the APU control switch to "OFF".

Possible Causes:

  • Auxiliary Power Unit (APU) Full-Authority Digital Engine-Controller (FADEC) (A108)
  • Fuel Control Unit (FCU) (A3)
  • Speed Sensor (MT4)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Access to Active Faults AMM 45-45-00-970-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to Stored Faults AMM 45-45-00-970-803 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to System Diagnostics AMM 45-45-00-970-804 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Engine Branched Wiring-Harness AMM 49-12-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Engine Branched Wiring-Harness AMM 49-12-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Fuel Control Unit AMM 49-30-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Fuel Control Unit AMM 49-30-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Full-Authority Digital Engine-Controller (FADEC) AMM 49-61-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Full-Authority Digital Engine-Controller (FADEC) AMM 49-61-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Speed Sensor AMM 49-61-17-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Speed Sensor AMM 49-61-17-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Remove APU FADEC and perform a visual inspection of the FADEC rack, pins and sockets for damage or FOD.

    1. If damages are found, repair as required and do close out.
    2. If damages are not found, continue with next step.

  2. Disconnect the MPE1P1 connector from the LCV and inspect for contamination and damage.

    1. If contamination or damage found, repair as required and do close out.
    2. If contamination or damage not found, re-connect MPE1P1 connector and continue with next step.

  3. Disconnect the A3P1 connector from the FCU (A3) and inspect for contamination and damage.

    1. If contamination or damage found, repair as required and do close out.
    2. If contamination or damage not found, re-connect A3P1 connector and continue with next step.

  4. Disconnect the MT4P1 connector from the APU Speed Sensor (MT4) and inspect for contamination and damage.

    1. If contamination or damage found, repair as required and do close out.
    2. If contamination or damage not found, re-connect MT4P1 connector and continue with next step.

  5. Perform a continuity check between APU FADEC connector A108AP1 and ground as follows:

    From To Expected Result Result
    A108AP1-F2 Ground 33 Ω to 41 Ω
    A108AP1-G2 Ground 33 Ω to 41 Ω

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

  6. Perform a continuity check between APU FADEC connector and ground (this is the FCU shut-off solenoid) as follows:

    From To Expected Result Result
    A108BP1-A1 Ground 18 Ω to 33 Ω
    A108BP1-B1 Ground 18 Ω to 33 Ω

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

  7. Perform a continuity check between APU FADEC connector A108AP1and ground (this is the speed sensor (dual channel)) as follows:

    From To Expected Result Result
    A108AP1-G11 Ground ≈24 Ω
    A108AP1-H11 Ground ≈24 Ω
    A108AP1-J11 Ground ≈33.9 Ω
    A108AP1-K11 Ground ≈33.9 Ω

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

  8. Re-rack APU FADEC.

    1. If system checks are good, do close out.
    2. If fault remains continue with next step.

  9. Access CAIMS/System Diagnostics/ATA 49/FADEC/LRU TEST/APU DATA STATUS page 1 and read EGT DATA. Back out and go to APU DATA STATUS page 2 and read EGT data. Compare the two and ensure they are the same or close to the same value (Page 1 is channel 1, Page 2 is channel 2). Compare the rest of the data on these two pages to current conditions and ensure it is accurate. If possible read this data with, and without the APU running to have as much data as possible. If you suspect a sensor; remember what you are reading is real time (give or take 5 seconds), so have an assistant change the sensor physically (temp/ pressure) and verify the changes in CAIMS.
  10. Swap speed sensor.

    1. If system checks are good, replace defective speed sensor and do close out.
    2. If fault remains, continue with next step.

  11. Replace the APU FADEC.
  12. Do close out.
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