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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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09/19/19

Message Overview:

Fault Message:

FADEC [OVERSPEED CIRCUIT 1]

Fault Code:

4960250APU

Associated CAS:

APU FAULT
(Advisory)

Reporting LRU: Full-Authority Digital Engine-Controller (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:

The Full-Authority Digital Engine-Controller (FADEC) has detected a loss of redundant overspeed protection. The FADEC has detected an internal failure to its overspeed protection circuitry.

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.

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 during
i) start
ii) on-speed operation
FIRE EMERG * Fire signal is received by the FADEC
REVERSE FLOW * T2 temp. limit (176.6°C/350°F) has been exceeded for 5 secs
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 seconds)
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 secs
NO CRANK rpm does not rise above 5% within:
a) 2 secs when oil temp is warmer than minus 23°C, or
b) 50 secs when oil temp is minus 23°C or lower
INLET DOOR Inlet door position indicates closed 30 secs 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 cutout
APU GCU HIGH OIL TEMP * APU Generator oil temperature above 215°C

Possible Causes:

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

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

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 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. Inspect the wiring and connectors to the speed sensor for any damage.

    1. If system checks are not good, repair or replace defective wiring as required and do close out.
    2. If system checks are good, continue with next step.

  2. Inspect the speed sensor for condition and check that the resistance within speed senor as follows:

    From To Expected Result Result
    MT4P1-A MT4P1-B 54.08 - 81.12 Ohms

    1. If system checks are not good, replace speed sensor and do close out.
    2. If system checks are good, continue with next step.

  3. Re-rack FADEC and verify connector A108AP1-G11, A108AP1-H11, A108AP1-J11 and A108AP1-K11 for damage or FOD, verify if fault is still present.
  4. Perform continuity check between APU firewall and the speed sensor connector. The resistance should measure as follows:

    From To Expected Result Result
    P802-13 MT4P1-A <1 ohm
    P802-14 MT4P1B <1 ohm

    1. If measurements are not good, repair defective wiring as required and do close out.
    2. If measurements are good, continue with next step.

  5. Perform wiring check between APU firewall and the APU FADEC connector. The resistance should measure as follows:

    From To Expected Result Result
    J802-13 A108AP1-G11 <3 ohms
    J802-14 A108AP1-H11 <3 ohms

    1. If measurements are not good, repair defective wiring as required and do close out.
    2. If measurements are good, continue with next step.

  6. Replace the APU FADEC.
  7. Do close out.
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