G600 MU-2B Checklist Changes 190-00601-20 Rev. 1
Page 3 of 5
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) 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]
Autopilot .......................................................................................... DISCONNECT
Aircraft Controls .................................... INITIATE MAXIMUM POWER CLIMB
Airspeed ........................................................... BEST ANGLE OF CLIMB SPEED
After warning ceases:
Power ......................................................................... MAXIMUM CONTINUOUS
Altitude .......................................... 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:
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.
2) Emergency Expanded Checklist
No changes required.
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