Garmin G5000 - MFD Failure; Single GTC (Touch Screen Controller) Failure

Model 560XL Section III – Operating Procedures
Abnormal Procedures
Textron Aviation Citation 560XL 190-02313-03 Rev. 8
3-42 FAA Approved
 MFD FAILURE
MFD failure is indicated by a complete loss of image on the center display. If only individual elements
of the display are failed, refer to appropriate procedures for the individual failures.
To select reversionary display of composite primary flight instruments and engine instruments on PFD
1 and/or PFD 2:
1. PFD 1 and/or PFD 2 Knob (DISPLAY FORMAT Panel) – REV.
Procedure completed
 SINGLE GTC (TOUCH SCREEN CONTROLLER) FAILURE
If either GTC is failed, TOLD data must be verified using the AFM or other alternate approved source.
 IF GTC 1 FAIL
1. TOUCH CTRL 1 (PRIM) Circuit Breaker (LH Panel – AVIONICS) – IN.
TOUCH CTRL 1 (SEC) Circuit Breaker (RH Panel – AVIONICS) – IN.
 IF GTC 2 FAIL
1. TOUCH CTRL 2 Circuit Breaker (RH Panel – AVIONICS) – IN.
 IF GTC FAILURE REMAINS:
2. IF GTC 1 FAIL
a. TOUCH CTRL 1 (PRIM) Circuit Breaker (LH Panel – AVIONICS) – PULL.
b. TOUCH CTRL 1 (SEC) Circuit Breaker (RH Panel – AVIONICS) – PULL.
IF GTC 2 FAIL
a. TOUCH CTRL 2 Circuit Breaker (RH Panel – AVIONICS) – PULL.
3. Use the operative GTC:
 Use the Pilot and Copilot tabs to control both pilot’s radio, mic, and audio source
selections.
 All four MFWs can be controlled via pane selection on the operative GTC.
 If desired, the remote PFD controller (GCU) can be used to tune the radios and
control other functions.
Procedure completed