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G500 Q

ARMIN

ADC Failure

Indications - Complete loss of the Air

Data Computer (ADC) is indicated

by a red X and yellow text over the

airspeed, altimeter, vertical speed,

TAS and OAT displays. True airspeed

and wind calculations are also lost.

Pilot Action - Use standby airspeed

indicator and altimeter for speed

and altitude data. There is no backup

for the VSI, but known pitch attitudes

using the attitude indicator, power

settings, and airspeeds produce

consistent descent rates.

UICK

EFERENCE

continued...

Electrical Failure

Indication - In the event of a total loss of electrical

power, the G500 system will be inoperative / dark.

The STBY PWR button on the standby attitude

indicator will begin blinking indicating it will turn off

in one minute.

Pilot Action - For attitude reference, press the "STBY

PWR" button on the standby attitude indicator

while blinking to operate using its integral

emergency battery. If the red warning flag appears

on the standby attitude instrument face, the unit is

powered off or inoperative and must not be used.

Use the standby airspeed, altimeter, compass, and

GNS430 for remaining flight data.

AHRS Failure

Indications - Failure of the Attitude

and Heading Reference System (AHRS)

is indicated by a removal of the sky/

ground presentation, a red X across

the Attitude Indicator, and a yellow

"ATTITUDE FAIL" and "HDG" messages

on the PFD. Rate-of-turn information

will not be available.

Pilot Action - Use standby attitude

indicator for attitude info and a

combination of the magnetic compass

and Garmin GNS 430 for heading. The

CDI will function normally.

Heading Failure

Indications - A complete Heading

Failure (magnetometer and GPS

ground track failure) is indicated by

the digital heading presentation

being replaced with a red X and

the compass rose digits being

removed.

Pilot Action - Use the magnetic

compass and the GNS 430s for

heading information.