Cockpit Reference Guide for the Cirrus SR2x with Perspective Touch+ by Garmin
190-02954-01 Rev. A
Warnings, Cautions & Notes
NOTE:
When operating the system with the magnetic sensor uncoupled from the
AHRS, the displayed heading and heading information used by some system compo-
nents (e.g. traffic system, AFCS, and weather radar) will be different from the heading
calculated by the AHRS. The difference is an amount equal to the difference between
the current Magnetic Field Variation Database (MV DB) value, and the MV DB value
when the magnetic sensor was uncoupled. Due to the convergence of isogonic lines,
this condition is most noticeable at or near the north and south magnetic poles.
NOTE:
Interference from GPS repeaters operating inside nearby hangars can cause an
intermittent loss of attitude and heading displays while the aircraft is on the ground.
Moving the aircraft more than 100 yards away from the source of the interference
should alleviate the condition.
NOTE:
Operate G2000 system power through at least one cycle in a period of four
days of continuous operation to avoid an autonomous system reboot.
NOTE:
The purpose of this Cockpit Reference Guide is to provide the pilot a resource
with which to find operating instructions on the major features of the system more
easily. It is not intended to be a comprehensive operating guide. Complete operating
procedures for the system are found in the Pilot’s Guide for this aircraft.
