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(WARNING)
RED MESSAGE
(CAUTION)
AMBER MESSAGE
(ADVISORY)
CYAN MESSAGE
(STATUS)
WHITE MESSAGE
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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04/26/21

Message Overview:

Message Name:

HEADING FLAG (Caution)

Identifier: 342OBS004
Effectivity: AIRCRAFT 20501 - 20999
System: Navigation
Associated CAS: None
System Description: 34-21-00
Schematic Diagram: None
Wiring Diagram: 34-21-01
34-21-05

Message Description:

The amber 'HDG' caution flag identifies that the IRS heading is split or the IRSs can not cross compare to each other.

  • Inaccurate heading information can be caused by a flux valve, flux valve wiring failure, or magnetic field disruption around the flux valve.
  • The IRS calibration may need to be re-accomplished, or the IRS unit may be drifting. Checking the aircraft on a compass rose or know heading (aircraft runway lineup) to determine the inaccurate side assists trouble shooting.
  • Cross comparator problems could be associated with a bad IOC, IRS Computer or Data bus failure.

    MDC troubleshooting information may help isolate data validity, prior to component replacement and data bus ring-out.

flux_detector_unit

Possible Causes:

  • Flux Valve
  • Magnetic Field Disruption around the Flux Valve.

    • Inertial Reference System (IRS) Calibration

    • Input/Output Concentrator (IOC) (A4-IOC)

    • Inertial Reference Unit 1 (IRS 1) (A233)

    • Inertial Reference Unit 2 (IRS 2) (A232)

    • Data Bus Failure

    • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Removal of the Input/Output Concentrator Unit (IOC) AMM 31-45-05-000-801
Installation of the Input/Output Concentrator Unit (IOC) AMM 31-45-05-400-801
Operational Test of the Input/Output Concentrator Unit (IOC) AMM 31-45-05-710-801
Operational Test of the Inertial Reference System (IRS) AMM 34-45-00-710-801
Removal of the Inertial Reference Unit (IRU) AMM 34-45-01-000-801
Installation of the Inertial Reference Unit (IRU) AMM 34-45-01-400-801
Wiring - Maintenance Practices - ALL SPM 20-12-00-02
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02

Troubleshooting Recommendations:

The IRS system is susceptible to splits (Compass headings disagree by more than 5°) in or around hangars or on the tarmac where underground plumbing or electrical wiring runs. Taxi the aircraft away from these areas, select the "slew" switch to either L or R with the system still in slave, this will "quick align" the IRS system to the flux valve input.

  • If the system does not match up, check the area around the flux valves for magnetic hardware.
  • If no magnetic hardware is found around the flux valves, the system will require a compass swing, perform the compass swing IAW AMM TASK 34-21-00-820-802.

45_current_faults

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