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ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 FAILED AIRSPEED, ALTITUDE, AND/OR VERTICAL SPEED
(RED "X" ON PFD AIRSPEED, ALTITUDE, AND/OR VERTICAL
SPEED INDICATORS)
This indicates a loss of valid air data system information to the respective system. If either
primary altitude indication is affected, the airplane is no longer RVSM capable.
• IF BOTH SIDES
1. Airspeed and Attitude . . . . . . . . . . . . . . . . . . . . . MONITOR using standby instruments
2. Land as soon as practical.
PROCEDURE COMPLETED
• IF ONE SIDE ONLY
1. Affected PFD SENSOR Softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
2. Affected PFD ADC1/2 Softkey . . . . . . . . . . . . . . . . . . . . . . SELECT opposite side ADC
3. PFD ADI Displays . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM "BOTH ON ADC1 or 2"
is displayed on both PFDs
PROCEDURE COMPLETED
3-102 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 FAILED ATTITUDE AND/OR HEADING (ATTITUDE FAIL AND/
OR RED “X” OVER HEADING DISPLAY ON PFD)
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 aircraft is on the ground. This is usually accompanied by a BOTH ON GPS1/2
message. Moving the aircraft more than 100 yards away from the source of the interference
should alleviate the condition.
• IF BOTH SIDES
1. Attitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR using standby attitude gyro
2. COCKPIT FAN Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. AIR SOURCE SELECT Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L, R, BOTH, or OFF
(Any position other than FRESH AIR)
4. L/R WINDSHIELD ANTI-ICE Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
NOTE
With windshield heat OFF, fog or frost will form on the inside surface of the
windshield. The windshield heat should be turned off only long enough to reference
magnetic compass or the pilot should descend to a warmer altitude if terrain, fuel, and
endurance permit.
5. Heading. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR using magnetic compass
6. Land as soon as practical.
NOTE
• The autopilot will disconnect and may not be re-engaged.
• Reference the GPS track on MFD/PFD map to improve situational awareness.
GPS will continue to display correct GPS based map, position, and track.
• Magnetic compass is influenced by windshield heat, cockpit fan, and fresh air fan.
These items must be off prior to referencing magnetic compass heading then may
be reselected on. The items must then be reselected off prior to each referencing
of the magnetic compass.
PROCEDURE COMPLETED
• IF ONE SIDE ONLY
1. Standby Attitude Gyro . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
2. Affected PFD SENSOR softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
3. Affected PFD AHRS1/2 softkey . . . . . . . . . . . . . . . . . . . SELECT opposite side AHRS
4. PFD ADI Displays . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM “BOTH ON AHRS1 or 2"
is displayed on both PFDs
5. Flight Director . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TRANSFER
(XFR button) to functional side
NOTE
The autopilot will disconnect and may not be re-engaged.
PROCEDURE COMPLETED
510FM-07 AA 3-103
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 LOSS OF NAVIGATION DATA (LATERAL DEVIATION BAR NOT
PRESENT AND/OR GLIDESLOPE INDEX CLEARS)
This indicates a loss of data from the selected NAV source. Refer to GARMIN G1000 Cockpit
Reference Guide for additional information.
1. Opposite NAV Source. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT
2. PFD HSI Displays. . . . . . . . . . . . . CONFIRM OPPOSITE “LOC1/LOC2" or “VOR1/VOR2"
is displayed on both PFDs.
PROCEDURE COMPLETED
 STALL WARN FAIL (STALL WARNING FAILURE)
This message is displayed when the stall warning and/or low speed awareness functions are
　
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