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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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02/26/21

Message Overview:

Message Name:

FLAP RUNAWAY

Message Code:

B3-006688

Associated CAS:

FLAPS FAIL
(Caution)

Reporting LRU: FLAP CTRL UNIT
System Description: 27-51-00
Schematic Diagram: 27-52-00
Wiring Diagram: 27-52-33

Message Description:

Flap Control Unit (FCU) detected a runaway in the Flap System. Check mechanical driveline for symmetric disconnect. (If OB Actuator is disconnected or replaced, flaps must be rigged).

Possible Causes:

  • Mechanical Driveline
  • Flap Power Unit (FPU) (A123)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

  • AW300-27-0058 - Flap Control Unit - CAS Messages Reset procedure (20501 to 20999)

Forum Articles/Infoservice/Newsletter: None

In the MDC system parameters, an FPU PRESS XDCR SIGNAL showing 3740 PSI indicates the FCU have detected a malfunction in the system and do not send the excitation signal to the FPU pressure transducer.

MDC REPORT: SYSTEM PARAMETERS
FILENAME:
DATE:
...
FLAP SURFACE ANGLE - 3.74 DEG
FPU PRESS XDCR SIGNAL - 3740 PSI
APU HOURS - 1116.75 HRS

Source of the problem still has to be found.

Quick Links:

Removal of the Flap Control Unit (FCU) AMM 27-51-05-000-801
Installation of the Flap Control Unit (FCU) AMM 27-51-05-400-801
Operational Test of the Flap Control Unit (FCU) AMM 27-51-05-710-801
Electrical Rigging of the Flap System AMM 27-52-00-820-801
Mechanical Rigging of the Flap System AMM 27-52-00-820-802
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. Perform a General Visual Inspection of the Flap system per AMM (Verify integrity of driveline by pulling and pushing on the flap panel and by attempting to rotate the driveline by hand, verify integrity of AGB, and actuators to ensure that they are not loose or do not have stripped gears.).

        1. Replace any defective component per AMM.
        2. Continue with next step.

      2. Reset the following circuit breakers.

        1. If system checks are good, do close out.
        2. If fault remains, continue with next step.
        FLAP R IND CB2-B12
        FLAP L IND CB1-B13
        FLAP CTRL CB1-B14

      3. Reset the FCU by pressing the FCU reset button on the MAINTENANCE TEST control-panel. If unable to reset, engage the Alternate Flaps button with the left hydraulic system pressurized, and attempt another reset using the Flap Reset switch on the left galley.

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

      4. Perform a Flap Power Unit solenoid resistance check as follow.

        1. If values are not within specifications, replace FPU per AMM.
        2. If system checks are good, do close out.
        Connector Part Coil Resistance: Values:
        A123J1 POB Solenoid Pins 4-5 = Normally around 58 Ω
        A123J1 Solenoid #2 Pins 1-2 = Normally around 58 Ω
        A123J1 EHSV Pins 7-8 = Normally around 500 Ω
        A123J2 Solenoid #1 Pins 1-2 = Normally around 58 Ω

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