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PROCEDURE COMPLETED
 SPD BRK EXTEND
Indicates that one or both speed brakes are not in the stowed position.
3-132 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
ADVISORY MESSAGES
White CAS messages are advisory in nature and denote items which are considered normal during
operation of the airplane or do not normally require any pilot action. These are intended primarily to
provide feedback to the pilot regarding system status. However, some procedures are provided in
the event a white message posts at an inappropriate time or when not commanded by the pilot.
Garmin G1000 System Messages are displayed in the PFD message window and are accessed by
pressing the MSG softkey on either PFD. Additional information on these and other Garmin G1000
advisory messages can be found in the Garmin G1000 Cockpit Reference Guide.
 CABIN ALT - WHITE
This message is displayed when the pressurization system is operating in High Altitude Airfield
mode and cabin altitude exceeds 10,000 feet for less than 30 minutes.
 ENG A/I COLD L-R – WHITE
Indicates that the engine inlet temperature is below safe level for satisfactory ice protection. This
message will post in white for up to two minutes after engine anti-ice is turned on while the inlet
warms up to the normal operating temperature.
 FUEL BOOST L-R - WHITE (FUEL BOOST PUMP ON)
Indicates that the respective fuel boost pump has been activated normally.
 FUEL LO INOP L-R
Indicates that the fuel quantity signal condition is not able to determine if the fuel level is below
170 lbs. in the respective tank.
1. Refer to Abnormal Procedures, FUEL QUANTITY RED ‘X’ OR INCORRECT FUEL
INDICATION if required.
PROCEDURE COMPLETED
 FUEL TRANSFER
Indicates that the fuel transfer valve is open. In the event this message remains displayed after
the fuel transfer knob is turned OFF, refer to Abnormal Procedures, FUEL TRANSFER
MESSAGE ON WHEN TRANSFER NOT SELECTED.
510FM-07 AK 3-131.1
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 NO TIRE SPINDOWN
Indicates that the spindown feature of the antiskid system has failed. The following procedures
are required for subsequent flights.
AFTER TAKEOFF
1. ANTISKID Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
2. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY GENTLY to stop wheel rotation
3. ANTISKID Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
4. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
PROCEDURE COMPLETED
 PRESS CTRL - WHITE
(PRESSURIZATION CONTROL BACKUP MODE)
Indicates the loss of communication between the Pressurization Controller and the Garmin
system. Pressurization system will continue to function normally using built-in backup sensors;
however, it will not be possible to change the Destination Elevation.
 PRESS OFF (PRESSURIZATION OFF)
Indicates that the AIR SOURCE SELECT Knob is in either the OFF or FRESH AIR position. The
cabin will not pressurize unless switch positioned in L, BOTH, or R.
• IF CABIN PRESSURIZATION IS DESIRED
1. AIR SOURCE SELECT Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L, BOTH, or R
PROCEDURE COMPLETED
 SPD BRK EXTEND
Indicates that one or both speed brakes are not in the stowed position.
3-132 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 STALL WARN HI
Indicates that the stall warning system is set to the Icing Conditions schedule.
• IF STILL IN ICING CONDITIONS OR IT CANNOT BE VISUALLY
VERIFIED THAT THE AIRPLANE IS CLEAR OF ICE
1. Landing Performance . . . . . USE STALL WARNING-HIGH landing performance charts
PROCEDURE COMPLETED
• IF IT CAN BE VISUALLY VERIFIED THAT THE AIRPLANE IS CLEAR
OF ICE
1. PITOT-STATIC Switch. . . . . . . . . . . . . . . . . . . . . RESET STALL WARN and RELEASE
2. Landing Performance . . USE STALL WARNING-NORMAL landing performance charts
PROCEDURE COMPLETED
 SURFACE DE-ICE
Indicates that a segment of the deice boot system is inflated to a satisfactory pressure.
 W/S A/I FAIL L-R - WHITE (WINDSHIELD ANTI-ICE FAILURE)
Indicates that the windshield controller has failed for less than 5 seconds or is performing a selftest.
　
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