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STATUS page to aid in determining which primary system is most
accurate.
o IF ABLE TO IDENTIFY ACCURATE ALTITUDE SOURCE
5. Use SENSOR REVERSION to select most accurate ADC on
both PFDs.
6. Land as soon as practical.
PROCEDURE COMPLETED
o IF UNABLE TO IDENTIFY ACCURATE ALTITUDE SOURCE
5. Land as soon as practical. Consider diversion to visual
conditions.
6. Maintain altitudes based on LOWEST indicated altitude.
7. ATC- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ADVISE
of inability to verify correct altitude
8. If unable to descend into visual conditions, plan ILS approach
with course intercept well outside the Final Approach Fix (FAF).
9. Once glideslope is intercepted, determine most accurate altitude
source when crossing FAF.
10. Reference ILS Decision Height to most accurate altimeter based
on FAF crossing.
WARNING
TAWS alerts are based on GPS altitude and position information and are
independent of ADC data. If a TAWS alert is received, it should be
considered valid and appropriate terrain avoidance action should be
taken.
PROCEDURE COMPLETED
• IF ANNUNCIATION CLEARS
PROCEDURE COMPLETED
510CLEAP-07 AA 63
S
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
This message is displayed when the G1000 detects a difference of 7 KIAS or greater
between the pilot’s and copilot’s airspeed information (10 KIAS difference during
takeoff or landing roll). Refer to GARMIN G1000 Cockpit Reference Guide for
additional information.
1. Pilot and Copilot Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - -COMPARE
with Standby Airspeed Indicator
WARNING
The Standby Airspeed Indicator uses the same pitot-static sources as the
pilot’s side Air Data Computer (ADC1). Do not use Standby Airspeed
indicator as sole source in determining correct airspeed.
• IF STANDBY AIRSPEED AND COPILOT PFD AGREE (PILOT PFD
DIFFERS)
2. SENSOR Softkey (pilot PFD) - - - - - - - - - - - - - - - - - - - - - - - - - PRESS
3. ADC2 Softkey - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - PRESS
4. PFD ADI Displays- - - - - - - - - - - - - - - - - CONFIRM “BOTH ON ADC2”
is displayed on both PFDs
PROCEDURE COMPLETED
• IF PILOT PFD AND STANDBY AIRSPEED AGREE (COPILOT PFD
DIFFERS)
2. Pilot and Copilot ALTITUDE- - - - - - - - - - - - - - - - - - - - - - - - - - - NOTE
 IF ALTITUDES AGREE
3. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - 120 KIAS MINIMUM
on slowest indicator
4. Monitor all three airspeed indicators during changes in power setting
or altitude to determine which indicators are inaccurate.
Indications of inaccurate airspeed include:
a. No change in indicated airspeed when power
changed and altitude maintained.
b. Indicated airspeed increases when climbing or
decreases when descending.
5. Use SENSOR REVERSION to select most accurate ADC on the
affected PFDs.
6. Airspeed - - - - - - - - - - - - - - - - - - - - RESUME NORMAL SPEEDS
PROCEDURE COMPLETED
 IF ALTITUDES DO NOT AGREE
3. Refer to ALT MISCOMP (Altitude Miscompare) procedure; Tab S3, to
determine most accurate ADC.
PROCEDURE COMPLETED
1  IAS MISCOMP (AIRSPEED MISCOMPARE)
64 AA 510CLEAP-07
T
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
This message is displayed when the G1000 detects a difference between the pilot and
copilot’s attitude or heading information (displayed in the upper right of the PFD). Refer
to GARMIN G1000 Cockpit Reference Guide for additional information.
• PITCH OR ROLL MISCOMP INDICATION
1. Refer to STANDBY ATTITUDE indicator to determine which AHRS is
providing the most accurate data.
2. Use SENSOR REVERSION to select the most accurate AHRS on the
affected PFD.
• HEADING MISCOMP
1. L/R WINDSHIELD ANTI-ICE Switches - - - - - - - - - - - - - - - - - - - - - OFF
2. COCKPIT FAN- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
3. AIR SOURCE SELECT Knob - - - - - - - - - - - - - - - - L, BOTH, R or OFF
(Any position other than FRESH AIR)
4. Refer to Magnetic Compass to determine which AHRS is providing the
most accurate heading information.
5. Use SENSOR REVERSION to select the most accurate AHRS on the
affected PFD.
6. L/R WINDSHIELD ANTI-ICE Switches - - - - - - - - - - - - - AS REQUIRED
7. COCKPIT FAN- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AS DESIRED
8. AIR SOURCE SELECT Knob - - - - - - - - - - - - - - - - - - -AS REQUIRED
PROCEDURE COMPLETED
　
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