Garmin Part 23 AML STC Checklist Changes Sheet
Contents
1. Delete the procedure Alternative Flight Instruments USE by drawing a line through the text with permanent marker Write STC SA02153LA D next to the deleted text Emergency Expanded Checklist No changes required Page 3 of 5 190 00601 20 Rev 1 3 Abnormal Abbreviated Checklist Add a page to the existing checklist at the beginning of the Abnormal Abbreviated section that states the following G600 Abnormal Abbreviated Checklist STC SA02153LA D Loss of Electrical Power to G600 System For installations with a Mid Continent Electric Standby Attitude Instrument STBY PWR on Standby Attitude Instrument ee eeeeeneeeneceeeeeees PRESS ATTITUDE FAILURE Attitude Red X ATTITUDE FAIL annunciation Attitude Source Use Standby Attitude Instrument and Magnetic Compass Seek VFR Conditions or land as soon as practical AIRSPEED FAILURE Airspeed Red X AIRSPEED FAIL annunciation Airspeed SOUECE e tuei E EA Use Standby Airspeed Instrument Seek VFR Conditions or land as soon as practical ALTITUDE FAILURE Altitude Red X ALTITUDE FAIL annunciation Altitude S OUNCE ag gists stay E e R E O le EAR Use Standby Altimeter Seek VFR Conditions or land as soon as practical HEADING FAILURE Heading Red X Heading Source Use GPS Ground Track or Magnetic Compass GPS POSITION FAILURE NO GPS POSITION annunciation Navigation Source Selection If dual GPS press the G600 1 2 softke2. MU 2B Checklist Changes Required for the Installation of a Garmin G600 PFD MFD System The following describe a list of changes to the MU 2B approved checklist that must be accomplished by the installer during the installation of a Garmin G600 PFD MFD system under STC SA02153LA D These changes have been accepted by the Kansas City Aircraft Evaluation Group in accordance with SFAR 108 1 2 G600 MU 2B Checklist Changes Emergency Abbreviated Checklist Add a page to the existing checklist at the beginning of the Emergency Abbreviated section that states the following G600 Emergency Abbreviated Checklist STC SA02153LA D TAWS WARNING Red annunciator and aural PULL UP if installed Autopilote i es Pata geese ee RD Nanas dae a Ardea aces DISCONNECT Aircraft Controls i5 2 sssccseisecasesesaetodess INITIATE MAXIMUM POWER CLIMB Alts pe d 25 enei toma ee at teesucs cams wean eaten BEST ANGLE OF CLIMB SPEED After warning ceases POWER eeni a bt th esa atihs iene MAXIMUM CONTINUOUS ASUS ss ccsctscsdianisetenctedeoetuareencn CLIMB AND MAINTAIN SAFE ALTITUDE Advise ATC of Altitude Deviation if appropriate For the INVERTER FAIL ANNUNCIATOR CYCLES ON OFF procedure Delete the procedure Alternative Flight Instruments USE by drawing a line through the text with permanent marker Write STC SA02153LA D next to the deleted text For the INVERTER FAIL ANNUNCIATOR ILLUMINATED procedure
3. y TAWS CAUTION Terrain Obstacle Ahead Sink Rate Don t Sink if installed When a TAWS CAUTION occurs take corrective action until the alert ceases Stop descending or initiate either a climb or a turn or both as necessary based on analysis of all available instruments and information 4 Abnormal and Normal Expanded Checklist Add a page to the existing checklist at the beginning of the Abnormal Expanded section that states the following For Garmin G600 PFD MFD System Abnormal and Normal Expanded procedures see the Airplane Flight Manual Supplement for the Garmin G600 System and Garmin G600 Cockpit Reference Guide G600 MU 2B Checklist Changes 190 00601 20 Rev 1 Page 4 of 5 5 Normal Abbreviated Checklist No changes required G600 MU 2B Checklist Changes 190 00601 20 Rev 1 Page 5of 5
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