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5  FUEL TRANSFER
2 AA 510CLEAP-07
A
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
WHITE CAS MESSAGES
TABLE OF CONTENTS
CABIN ALT - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A1
ENG A/I COLD L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A2
FUEL BOOST L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A3
FUEL LO INOP L-R- - - - - - - - - - - - - - - - - - - - - - - - - - - - - A4
FUEL TRANSFER - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A5
NO TIRE SPINDOWN- - - - - - - - - - - - - - - - - - - - - - - - - - - A6
PRESS CTRL- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A7
PRESS OFF- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A8
SPD BRK EXTEND- - - - - - - - - - - - - - - - - - - - - - - - - - - - - A9
STALL WARN HI - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B1
SURFACE DE-ICE - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B2
W/S A/I FAIL L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B3
W/S O’HEAT L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B4
510CLEAP-07 AK 1.1
WHITE CAS
MESSAGES
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
WHITE CAS 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 G1000 advisory messages
can be found in Garmin G1000 Cockpit Reference Guide.
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.
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.
Indicates that the respective fuel boost pump has been activated
normally.
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 Emergency/Abnormal Procedures, FUEL
QUANTITY RED “X” OR INCORRECT FUEL QUANTITY
INDICATION; Tab D7.
PROCEDURE COMPLETED
Indicates that the fuel transfer valve is open. In the event that this
message remains posted after the fuel transfer knob is turned OFF,
refer to Emergency/Abnormal Procedures, FUEL TRANSFER
MESSAGE ON WHEN TRANSFER NOT SELECTED; Tab E2.
1  CABIN ALT – WHITE
2  ENG A/I COLD L-R – WHITE
3  FUEL BOOST L-R - WHITE (FUEL BOOST PUMP
ON)
4  FUEL LO INOP L-R
5  FUEL TRANSFER
2 AA 510CLEAP-07
A
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
Indicates that the MFD temperature is below -20°C. Engine start
should be delayed until this CAS message clears. The MFD is warmed
and operational when the individual display elements such as letters
and cursors change without blurring or streaking. Engines may be
started when engine instrument numerical values are legible on the
MFD.
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
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.
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.
1. AIR SOURCE SELECT Knob- - - - - - - - - - L, BOTH, OR R
PROCEDURE COMPLETED
Indicates that one or both speed brakes are not in the stowed position.
　
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