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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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Quick Links

09/30/19

Message Overview:

Fault Message:

R CH B LOW TENSION IGNITN[1] RNG MA

Fault Code:

7327417RBR

Associated CAS:

None

Reporting LRU: Ignition Unit 1
System Description: 74-00-00
Schematic Diagram: 74-00-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 74-00-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

There is an open or short circuit in the low-tension circuit of Ignition System 1. The fault is found between the Engine Electronic Controller (EEC) and the Ignition Unit 1. The low-tension ignition circuits are continuously monitored by the Full-Authority Digital Engine-Controller (FADEC).

Possible Causes:

  • Ignition Unit 1
  • Right Engine Electronic Controller (EEC)
  • Secondary Power Distribution Assembly (SPDA) 3 (A15)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Connect Electrical Power to the Aircraft AMM 24-00-00-861-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Remove the Electrical Power from the Aircraft AMM 24-00-00-861-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Opening of Non-Thermal Circuit Breakers AMM 24-00-00-863-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Closing of Non-Thermal Circuit Breakers AMM 24-00-00-863-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Electrical/Electronic Safety Precautions AMM 24-00-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Engine Safety Precautions AMM 71-00-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Opening of the Cowls AMM 71-10-00-010-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Closing of the Cowls AMM 71-10-00-410-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Deactivation of the Thrust Reverser (for Maintenance) AMM 78-30-00-040-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Activation of the Thrust Reverser (for Maintenance) AMM 78-30-00-440-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Connection of Electrical Connectors EMM 70-50-01-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Engine Electronic Controller (EEC) EMM 73-21-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Engine Electronic Controller (EEC) EMM 73-21-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Ignition Units EMM 74-10-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Ignition Units EMM 74-10-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Safety Precautions - Maintenance Practices - ALL SPM 20-00-01-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

WARNING: Before touching the ignition system components, make sure of the conditions that follow:

  • Isolate the power supply (make sure the applicable circuit breakers are open)
  • After the power supply is isolated, do not touch the ignition system components before a minimum of three minutesThis must be done to make sure that the residual current decreases to a safe level. The ignition system has very high voltages which can kill.

  1. Perform a visual inspection of the ignition circuit wiring. Inspect for damage and proper installation.
    NOTE: Look specially for signs of damage adjacent to clip locations.

    1. If damage or defect is found, rectify or repair as required and do close out.
    2. If no damage or defect is found, continue with next step.

  2. Check if the CAS message R FADEC FAIL is displayed.

    1. If the CAS message R FADEC FAIL is displayed, troubleshoot the message first and continue with next step.
    2. If the CAS message R FADEC FAIL is not displayed, continue with next step.

  3. Disconnect the EEC connector (P1046) and the ignition unit 1 connector (P1055). Perform a visual inspection of the associated wiring and EEC connector (P1046) and ignition unit 1 connector (P1055).
    NOTE: Look specially for signs of chafing adjacent to clip locations, condition of connector pins and wiring kink or strain.

    1. If defects are found, repair or rectify defects as required and do close out.
    2. If no defects are found, continue with next step.

  4. Perform a continuity check as follows:

    From To Result
    P1055-2 P1046-30
    P1055-1 P1046-51

    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. Perform a insulation resistance check of the associated wiring between the EEC and the ignition unit 1 as follows:

    From To Resistance Value Result
    P1046-30 Ground 20 ΜΩ or more
    P1046-51 Ground 20 ΜΩ or more

    1. If the resistance value is less than the value specified in the table of if there is a short to ground, repair defective wiring as required and do close out.
    2. If there is no continuity or resistance value is as specified in the table, continue with next step.

  6. Remove the fixed cowl interface connector (2PB2). Check if there is 28 VDC as follows:

    From To Expected Result Result
    2JB2-7 2JB2-8 28 VDC

    1. If there is no 28 VDC, investigate the power source for SPDA 3 and do close out.
    2. If there is 28 VDC, continue with next step.

  7. Swap EEC 2 with EEC 1. Is the fault still present?

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

  8. Replace Ignition Unit 1.
  9. Do close out.
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