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1. Engine Sync- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
2. ENGINE ANTI-ICE Switch (affected engine) - - - - - - - - - - - - - - - - - - - OFF
3. RAT Indication on PFD - - - - - - - - - - - - - - - - - - - - - - - - VERIFY decrease
4. Exit icing conditions as soon as practical
5. Monitor for ice accumulation.
• IF ICING INTENSITY IS TRACE OR LESS
Go to Step 8 prior to descent.
• IF ICING INTENSITY IS GREATER THAN TRACE
6. Engine Anti-Ice Circuit Breaker (affected engine) - - - - - - - - - - - - - PULL
7. Exit icing conditions as soon as possible.
PRIOR TO DESCENT
8. Engine Anti-Ice Circuit Breaker- - - - - - - - - - - - - - - - - - - - - - - - - - -RESET
9. ENGINE ANTI-ICE Switches - - - - - - - ON until RAT indications are normal
and icing conditions are exited
PROCEDURE COMPLETED
1. Control Wheel - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - GRIP
2. Autopilot - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DISCONNECT
(high aileron control forces possible)
3. AILERON TRIM Switch - - - - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED
4. Autopilot - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ENGAGE as desired
PROCEDURE COMPLETED
3  UNCOMMANDED REDUCTION IN ENGINE POWER DURING
ICING CONDITIONS
4  AILERON MISTRIM (AIL OR AIL  ANNUNCIATION PFD)
510CLEAP-07 AA 61
R
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
Indicates a mistrim of the elevator while the autopilot is engaged. The autopilot will
normally trim automatically as required. However, during rapid acceleration,
deceleration, or configuration changes momentary illumination of this message may
occur accompanied by minor fluctuations in flight path. If the autopilot is disconnected
while this message is displayed, high elevator control forces are possible. In the event
of a sustained illumination, the following procedure should be followed:
1. Control Wheel- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - GRIP
2. Autopilot- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DISCONNECT
(high elevator control forces possible)
3. Elevator Trim - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
4. Autopilot- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ENGAGE as desired
PROCEDURE COMPLETED
1. Rudder Pedals - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - HOLD FIRMLY
2. AP/TRIM DISC Button - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - PRESS
(high rudder control forces possible)
3. RUDDER TRIM Switch - - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
4. Autopilot and Yaw Damper - - - - - - - - - - - - - - - - - - - - ENGAGE as desired
PROCEDURE COMPLETED
This message is displayed when the G1000 detects a difference of 200 feet or greater
between the pilot and copilot’s altitude information (displayed in the upper right of the
PFD.) Refer to GARMIN G1000 Cockpit Reference Guide for additional information.
1. Altimeter Settings - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VERIFY
both pilot and copilot have the correct altimeter setting
• IF ANNUNCIATION DOES NOT CLEAR
2. ATC- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ADVISE
of non-RVSM status, if required
3. Pilot and Copilot Altitude - - - - - - - - - - - - - - - - - - - - - - - - - -COMPARE
with Standby Altimeter
WARNING
The Standby Altimeter uses the same pitot-static sources as the pilot’s
side air data computer (ADC1). Do not use Standby Altimeter as sole
source in determining correct altitude.
(Continued Next Page)
1  ELEVATOR MISTRIM (ELE OR ELE  ANNUNCIATION PFD)
2  RUDDER MISTRIM (RUD OR RUD  ANNUNCIATION PFD)
3  ALT MISCOMP (ALTITUDE MISCOMPARE)
62 AA 510CLEAP-07
S
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
 ALT MISCOMP (ALTITUDE MISCOMPARE) (Continued)
 IF COPILOT PFD AND STANDBY ALTIMETER AGREE (PILOT PFD
DIFFERS)
4. SENSOR Softkey (pilot PFD) - - - - - - - - - - - - - - - - - - - - - - -PRESS
5. ADC2 Softkey- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -PRESS
6. PFD ADI Displays - - - - - - - - - - - - - - CONFIRM “BOTH ON ADC2”
is displayed on both PFDs
PROCEDURE COMPLETED
 IF PILOT PFD AND STANDBY ALTIMETER AGREE (COPILOT PFD
DIFFERS)
4. Compare indicated altitude to GPS altitude on MFD AUX-GPS
　
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