ADC AND COPILOT ALTIMETER FAILURE
1. Airspeed and Altitude - Refer to Standby Airspeed/Altimeter.
2. LAND AS SOON AS PRACTICAL.
NOTE
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CAUTION: DEPENDING ON THE CAUSE OF THE FAILURE, THE PRESSURIZATION CONTROLLER MAY BE IN BAROMETRIC MODE.
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The flight director will not display. The autopilot will engage in basic pitch and roll mode. Transponder altitude reporting will be inoperative.