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Garmin G5000 - Page 70

Garmin G5000
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Model 560XL Section III – Operating Procedures
Abnormal Procedures
Textron Aviation Citation 560XL 190-02313-03 Rev. 8
3-28 FAA Approved
GPS Approach – Downgrade ................................................................................................................... 3-45
GPS Approach – Loss of Navigation ....................................................................................................... 3-45
Audio (GMA) Failure ................................................................................................................................ 3-46
Loss of COM Radio Tuning Functions ..................................................................................................... 3-46
Failed Airspeed, Altitude, and/or Vertical Speed ..................................................................................... 3-47
Failed Attitude and/or Heading ................................................................................................................ 3-48
Engine Indication System (EIS) Failure ................................................................................................... 3-48
ENG DISPLAY FAULT ............................................................................................................................. 3-50
PFD 1 FAULT ........................................................................................................................................... 3-50
MFD FAULT ............................................................................................................................................. 3-51
PFD 2 FAULT ........................................................................................................................................... 3-51
Loss of VOR / ILS / LOC / GS Deviation Indicators ................................................................................. 3-52
BOTH ON ADC1 or BOTH ON ADC2 ...................................................................................................... 3-52
BOTH ON ATT/HDG1, BOTH ON ATT/HDG2 ......................................................................................... 3-53
BOTH ON GPS1, BOTH ON GPS2 ......................................................................................................... 3-53
TRANSPONDER STANDBY .................................................................................................................... 3-53
TRANSPONDER FAIL 1-2 ....................................................................................................................... 3-54
AVIONICS FAULT .................................................................................................................................... 3-54
AOA FAIL ................................................................................................................................................. 3-54
ADS-B Out Transmission Fail .................................................................................................................. 3-55
Synthetic Vision Displays Inconsistent with Primary Flight Instrumentation ............................................ 3-55
TAWS or GPWS Caution ......................................................................................................................... 3-55
TAWS or GPWS Flap Override ................................................................................................................ 3-55
CHECK RUNWAY SurfaceWatch Alert (During Takeoff) ........................................................................ 3-56
CHECK RUNWAY SurfaceWatch Alert (During Landing) ....................................................................... 3-56
SURFACEWATCH INHIBITED ................................................................................................................ 3-57
SURFACEWATCH FAIL .......................................................................................................................... 3-57
No Surfacewatch Runway Position Data ................................................................................................. 3-57

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