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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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03/10/21

Message Overview:

Message Name:

NOSE WHEEL STEERING FAIL

Message Code:

B3-007265

Associated CAS:

NWS FAIL
(Caution)

Reporting LRU: NOSEWHEEL STEER
System Description: 32-51-00
Schematic Diagram: 32-51-00
Wiring Diagram: 32-51-01
32-51-09
32-51-13
32-51-17
32-51-25
32-51-29

Message Description:

  • The Steering Control Unit (SCU) has detected an internal fault or a fault in an LRU.
  • The SCU has detected a Nosewheel angle exceeding 65°, left or right.
  • The SCU has been powered without or with low hydraulic pressure and with at least one NWSS component out of neutral.

The Nose Wheel Steering System (NWSS) will be disabled until the system is reset using the NWS PBA located on the TAWS/LG control panel.

Depending on fault severity, the system may not work at all, NWS faults can be viewed on the nose wheel steering computer.

If there are multiple codes flashing on the 7-segment of the SCU, record the codes to troubleshoot accordingly.

Whenever there is fault code '7' flashing with another code, start with the rigging of the NWSS.

NOTE: Switching the NWS PBA to OFF or removing power from the aircraft will clear the amber 'NWS FAIL' caution CAS message and reset any fault present in the system. An '0' (No Fault) will be displayed on the SCU's 7-segment display face when the NWS PBA is set to 'ON' if no faults are detected by the power-up test.

Possible Causes:

  • Air trapped in the Nose Wheel Steering System (NWSS)
  • Rotary Variable Transducer (RVT)
  • Steering Control Handwheel (MT85)
  • Rudder Pedal Transducer (MT86)
  • Steering Manifold Electro-Hydraulic Servo Valve (EHSV) (V7)
  • Steering Control Unit (SCU) (A73)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Troubleshooting Tips: ATA 32-51-00 NOSEWHEEL STEERING SYSTEM

Quick Links:

Automatic Download of the Steering Control Unit (SCU) Non-Volatile Memory (NVM) AMM 32-51-01-970-801
Manual Download of the Steering Control Unit (SCU) Non-Volatile Memory (NVM) AMM 32-51-01-970-802
Removal of the Steering Control Unit AMM 32-51-01-000-801
Installation of the Steering Control Unit AMM 32-51-01-400-801
Operational test of the Nosewheel-Steering Control System AMM 32-51-00-710-801
Pressurize the Left and Right Hydraulic Systems AMM 29-10-00-862-801
Release Hydraulic Pressure - Left and Right Hydraulic Systems AMM 29-10-00-862-802
Rigging of the Nosewheel-Steering Control System AMM 32-51-00-820-801
Standard Practices - Continuity and Insulation Check SPM 20-12-01-05
Wiring - Maintenance Practices - ALL SPM 20-12-00-02
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02
Electrical Connectors - Maintenance Practice - ALL SPM 20-20-00-02

Troubleshooting Recommendations:

  1. Before starting any troubleshooting, it is recommended to do a download of the SCU Non-Volatile Memory (NVM) and send it to Bombardier Customer Response Center (CRC) for analysis.
  2. Make sure NWS PWR 1 (LCBP-C12) and NWS PWR 2 (RCBP-C12) Circuit Breakers are pushed in.
  3. Make sure the Handwheel, Rudder Pedals, and Nose wheel are in their neutral position (0°)
  4. Pressurize the left hydraulic system (AMM TASK 29-10-00-862-801).
    NOTE: Always establish Left Hydraulic System pressure before switching the NWS System (NWSS) to 'ON' as it may trigger and record a false 'NWS FAIL' CAS message if any NWSS component is out of its neutral position.
  5. Set the SCU PBA to 'ON' (OFF legend is extinguished).
  6. Wait 30 seconds for PBIT to finish.
  7. Carry out the Operation Test of the Nosewheel-Steering System (AMM TASK 32-51-00-710-801), doing 10 full swings of the steering system using the handwheel and then rudder pedals, or until the "NWS FAIL' caution CAS message is displayed.

    1. If the fault message is not displayed, no maintenance action is required, but:
      → It is recommended to do a download of the SCU NVM and send it to Bombardier CRC for analysis.
      → It is recommended to carry out the Rigging of the NWS (AMM TASK 32-51-00-820-801) as it may solve spurious or intermittent faults.
    2. If the 'NWS FAIL caution CAS message is displayed, record the fault code(s) indicated on the SCU front face 7-segment display.

      NOTE: If there are multiple codes flashing on the SCUs 7-segment display combined with Fault Code '1', record the codes and troubleshoot them before addressing the Fault Code '1'.
      NOTE: If Fault Code '7' is flashing with another code, carry out Fault Code '7' troubleshooting before addressing any other fault.

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