Attitude Fail And/Or Hdg; Both On Adc1 Or Adc2; Both On Ahrs1 Or Ahrs2; Using Adc1 Or Adc2 - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

SECTION 3 CESSNA
ABNORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000

ATTITUDE FAIL AND/OR HDG

This message indicates a loss of pitch, roll, and/or heading information
from AHRS. Refer to Garmin G1000 Cockpit Reference Guide for
additional information. Interference from GPS repeaters operating
inside nearby hangars can cause an intermittent loss of attitude and
heading displays while the airplane is on the ground. This is usually
accompanied by a BOTH ON GPS1 or GPS2 message. Moving the
airplane more than 100 yards away from the source of the interference
should alleviate the condition.

BOTH ON ADC1 OR ADC2

This message is displayed on both PFDs and indicates that both pilot's
and copilot's PFDs are displaying data from the same Air Data
Computer. Normally the pilot's side displays ADC1 and the copilot's
side displays ADC 2. Refer to Garmin G1000 Cockpit Reference Guide
for additional information.
BOTH ON AHRS 1 OR AHRS2
This message is displayed on both PFDs and indicates that both pilot's
and copilot's PFDs are displaying data from the same Attitude Heading
Reference System. Normally the pilot's side displays AHRS 1 and the
copilot's side displays AHRS 2. Refer to Garmin G1000 Cockpit
Reference Guide for additional information.

USING ADC1 OR ADC2

This message is displayed on both PFDs and indicates that both PFDs
are displaying data from the opposite side Air Data Computer. Normally
the pilot's side displays ADC1 and the copilot's side displays ADC2.
Refer to Garmin G1000 Cockpit Reference Guide for additional
information.

USING AHRS1 OR AHRS2

This message is displayed on both PFDs and indicates that both PFDs
are displaying data from the opposite side Attitude Heading Reference
System (AHRS). Normally the pilot's side displays AHRS1 and the
copilot's side displays AHRS2. Refer to Garmin G1000 Cockpit
Reference Guide for additional information.
FAA APPROVED
3-100 U.S. 208BPHCUS-00