Garmin G2000 Pilot’s Guide for the Cessna T240
190-01263-01 Rev. A
36
SyStem overview
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toucHScreen controller Failure
If the Touchscreen Controller fails, the MFD continues to display what was shown prior to the failure of the
Touchscreen Controller. Most functions normally performed exclusively on the Touchscreen Controller will be
unavailable.
The PFD Controller is used to control communications and navigation radios, fl ight planning functions, and
procedure selection and activation on the PFD. Refer to the Audio and CNS and Flight Management sections
for information on using the PFD controller to perform these functions.
aHrS operation
note:
Refer to Appendix A for specifi c AHRS alert information.
note:
Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy.
In addition to using internal sensors, the GRS 77 AHRS uses GPS information, magnetic fi eld data and air
data to assist in attitude/heading calculations. In normal mode, the AHRS relies upon GPS and magnetic fi eld
measurements. If either of these external measurements is unavailable or invalid, the AHRS uses air data
information for attitude determination. Four AHRS modes of operation are available (see Figure 1-28) and
depend upon the combination of available sensor inputs. Loss of air data, GPS, or magnetometer sensor inputs
is communicated to the pilot by system message alerts.
AHRS no-GPS
Mode
AHRS coast-on-gyros
until invalid
AHRS Normal
Mode
AHRS no-Mag
Mode
AHRS no-Mag/
no-Air Mode
Heading Invalid
Heading Invalid
Attitude/Heading Invalid
YES
YES
YES
NO
NO
NO
Air Data Available and Reliable?
Mag Data Available and Reliable?
YES
NO
Mag Data AND Air Data
Available and Reliable?
GPS Data Available and Reliable?
Figure 1-28 AHRS Operation
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