Garmin G5000 - ADC 1 FAULT or ADC 2 FAULT; Loss of ATC Altitude Reporting; PFD Failure

Model 560XL Section III – Operating Procedures
Abnormal Procedures
190-02313-03 Rev. 8 Textron Aviation Citation 560XL
FAA Approved 3-41
 LOSS OF ATC ALTITUDE REPORTING
1. Verify selected transponder is in AUTO, TA ONLY, or ALT mode.
NOTE
When transponder is in ALT mode, TCAS will be in standby. No traffic will be displayed,
and no TAs or RAs will be issued.
 IF ATC DOES NOT RECEIVE AIRCRAFT’S ALTITUDE
2. Transponder Control (GTC) – SELECT other transponder.
Procedure completed
 ADC 1 FAULT OR ADC 2 FAULT
ADC 1 FAULT ADC 2 FAULT CAS message displayed
Indicates loss of altitude (static source) error correction in the affected air data computer.
1. PFD Softkeys: Sensors – ADC Settings – SELECT the unaffected ADC.
2. Altitude – MAINTAIN using ADC with error correction.
3. With loss of redundancy of primary altimetry systems, perform appropriate RVSM contingency
procedures for the loss of primary altimetry systems.
Procedure completed
 PFD FAILURE
PFD failure is indicated by a complete loss of image on a display. If only individual elements of the
display are failed, refer to appropriate procedures for the individual failures.
NOTE
At the time of PFD failure, if the flight director is selected to the side with the failed PFD,
the autopilot will immediately disconnect.
If the flight director is selected to the side with the operative PFD, the autopilot will remain
engaged.
1. CPL button (AFCS Mode Control Panel) – SELECT Operating PFD if required.
2. Autopilot and Yaw Damper – RE-ENGAGE if required.
3. AFCS Mode Control Panel – RE-SELECT desired modes.
4. With possible loss of autopilot, consider appropriate RVSM contingency procedures for the loss of
autopilot.
 TO SELECT REVERSIONARY DISPLAY OF BOTH COMPOSITE PRIMARY FLIGHT
INSTRUMENTS AND ENGINE INSTRUMENTS ON THE MFD
5. MFD Knob (DISPLAY FORMAT Panel) – REV If Desired
NOTE
When display reversion mode is selected, the MFD may initially present a non-SVT (blue
sky over solid brown ground) display. SVT will be presented on the backup display
within 20 seconds if it was enabled on the PFD when display backup was selected.
Procedure completed