FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS
190-01754-01 Rev. 4
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3.3 Attitude Aligning / Keep Wings Level
If the “
ALIGNING KEEP WINGS LEVEL
” indication occurs during flight, the G3X Touch has detected
an invalid attitude solution and will not display any attitude information.
1. Use standby instruments to maintain 1
o
nose up pitch and wings level flight. The system will
display attitude when internal accuracy tolerances have been met.
2. Limit aircraft attitude to +10
o
bank, +5
o
pitch, 200 KTAS or less.
3. If attitude does not return, continue to use the standby flight instruments for aircraft attitude
control.
3.4 AHRS ALIGN
This annunciation indicates that the AHRS is beginning to fail and the internal sensors are trying to
realign themselves. The attitude presentation behind the annunciation is still valid but should be
crosschecked using the standby instruments.
3.5 Autopilot Abnormal Disconnect
Red
AP
or
AFCS
flashing on PFD, Continuous high-low aural tone
1. Aircraft Attitude -------------------------------------------------- MAINTAIN/REGAIN AIRCRAFT CONTROL
2. FD Mode Bar on PFD ----------------------------------------------------------------------------------------- PRESS
(to cancel disconnect tone and extinguish annunciator)
3.6 G3X Touch Altimeter Barometric Window Cyan
If a G5 Standby Flight Instrument is installed and the G3X Touch Altimeter Barometric Setting window
is cyan and the digits are changing without the pilot manually adjusting the Barometric Altimeter setting
knob on the G5, disable the G5 / G3X Touch Baro synchronization as follows:
1. Press MENU, MENU
2. Scroll down to SETTINGS and Select.
3. Scroll down to PFD and Select.
4. Scroll down to
‘SFD Baro Sync’ and Select.
5. Change the selection from ENABLED to DISABLE.
6. Press and hold the BACK button to return to a normal PFD display.
7. Adjust the G3X Touch Altimeter Barometric Setting to the current local setting.
8.
Disregard the G5 Standby Instruments altimeter display and use the G3X Touch’s.
3.7 EIS Failure
EIS failure is indicated by the loss of displayed information on the EIS, including a blank, frozen, red
‘X’ over the display, or unresponsive display of EIS parameters.
1. Position engine controls to ensure operation within engine limitations.
