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Cirrus SR2x

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SYSTEM OVERVIEW<br />

SYSTEM<br />

OVERVIEW<br />

FLIGHT<br />

INSTRUMENTS<br />

AHRS OPERATION<br />

NOTE: Aggressive maneuvering in reversionary mode can degrade AHRS accuracy.<br />

The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration<br />

calculations for the system, using GPS, magnetometer, and air data in addition to information from its internal<br />

sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate<br />

combinations of information from the external sensor inputs.<br />

EIS<br />

Y<br />

E<br />

S<br />

GPS Data Available and Reliable?<br />

N<br />

O<br />

AUDIO PANEL<br />

& CNS<br />

FLIGHT<br />

MANAGEMENT<br />

HAZARD<br />

AVOIDANCE<br />

Mag Data Available and Reliable?<br />

Y<br />

E<br />

S<br />

AHRS Normal<br />

Mode<br />

Y<br />

E<br />

S<br />

AHRS no-Mag<br />

Mode<br />

N<br />

O<br />

Air Data Available and Reliable?<br />

N<br />

O<br />

AHRS no-Mag/<br />

no-Air Mode<br />

Mag Data AND Air Data<br />

Available and Reliable?<br />

Y<br />

E<br />

S<br />

AHRS no-GPS<br />

Mode<br />

N<br />

O<br />

AHRS coast-on-gyros<br />

until invalid<br />

AFCS<br />

Heading Invalid Heading Invalid Attitude/Heading Invalid<br />

Figure 1-20 AHRS Operation<br />

ADDITIONAL<br />

FEATURES<br />

APPENDICES<br />

INDEX<br />

Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by message advisory alerts (refer<br />

to Appendix A for specific AHRS alert information). Any failure of the internal AHRS inertial sensors results<br />

in loss of attitude and heading information (indicated by red ‘X’ indications over the corresponding flight<br />

instruments).<br />

Two GPS inputs are provided to the AHRS. If GPS information from one of the inputs fails, the AHRS uses<br />

the remaining GPS input and an alert message is issued to inform the pilot. If both GPS inputs fail, the AHRS<br />

can continue to provide attitude and heading information to the PFD as long as magnetometer and airspeed<br />

data are available and valid.<br />

If the magnetometer input fails, the AHRS continues to output valid attitude information. If GPS-based track<br />

information is available while magnetometer input has failed, the HSI displays the ground track instead of<br />

heading using HSI Track Mode. In this mode, a magenta ‘TRK’ annunciation and track readout appear on the<br />

32<br />

Pilot’s Guide for the <strong>Cirrus</strong> <strong>SR2x</strong> with <strong>Cirrus</strong> Perspective by Garmin<br />

190-00820-11 Rev. A

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