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entries may be made.
1. Press the FUEL key until the FUEL FLOW page is accessed.
2. Check the fuel flow displays for reasonableness.
3. Enter manual fuel flows if necessary.
4. Update the fuel used values manually if required.
Messages
2423sv602 11
Change 1
FUEL FLOW SELFTEST FAIL - Self test of the fuel flow
measurement circuitry has failed.
FUEL NOT CONFIRMED – The FMS was started up in the Standby
mode and the fuel has not been confirmed on FUEL page 1.
GPIR # DESELECT - The sensor monitor has determined that the
specified GPS data is unreasonable and has deselected the GPS
portion of the sensor for use in navigation. The message will be
removed after it is displayed once.
GPIRS # DIFFERENCE > xxNM - The sensor “Watchdog" has
sensed that the latitude/longitude position as determined by the GPS
portion of the GPIR# (1, 2 or 3) differs from the FMS best computed
position by an amount that warrants pilot attention. "xx" can be 6,
12, 18 or 24 NM.
GPIR # FAILED - A Fail status has been determined for the GPS
portion of the indicated GPIRS, because the position data is missing
or invalid or the status label indicates a FAIL status exists.
1. Press The DATA key to access DATA 2/4.
2. Check the sensor status.
GPIR # GPS NOT NAV - GPS portion of the GPIRS has change a
not navigational (neither Nav nor Alt) condition. GPS status page
will show the cause of the change.
GPS # DESELECT - The sensor monitor has determined that the
specified GPS data is unreasonable and has deselected the sensor
for use in navigation. The message will be removed after it is
displayed once.
GPS # DIFFERENCE > xxNM - The sensor "watchdog" has sensed
that the latitude/longitude position as determined by GPS# (1, 2, or
3) differs from the FMS best computed position by an amount that
warrants pilot attention. "xx" can be 6, 12, 18 or 24 NM.
Messages
12 2423sv602
Change 1
GPS # FAILED - A Fail status has been determined for the indicated
GPS, because the position data is missing or invalid or the status
label indicates a FAIL status exists.
1. Press The DATA key to access DATA 2/4.
2. Place cursor over sensor to access the SENSOR STATUS page
3. Check the sensor status.
GPS # NOT NAV - GPS has changed to a not navigational (neither
Nav nor Alt) condition for more than 3 minutes. GPS status page will
show the cause of the change.
GPS ONLY NAVIGATION - Displayed if a non-RAIM GPS is the
only position sensor available. Message is displayed 60 seconds
after condition exists and remains as long as condition exists.
Message is suppressed on the ground or while operating in the FIAS
‘GPS only’ mode.
GPS POS ALARM - GPS error is outside of phase of flight limits for
specified time.
HEADING REF FAIL - The AC reference for the Analog Heading
input has failed.
HIGH GNDSPD FOR HOLDING - In holding mode, the current
groundspeed is excessive for holding airspace. This may be due to
either high winds or high TAS. The pilot should lower airspeed if
feasible.
ILLEGAL FACILITY TYPE - The entered facility is of an invalid type
for this approach.
ILLEGAL WAYPOINT - A waypoint that is more than 6° from being
on the inbound course has been entered into the first optional
waypoint position in the approach definition pages.
INSIDE LOA - The aircraft is inside a defined LORAN Operating
Area (LOA). This message will be removed after it is displayed.
INVALID ARINC VERSION - Two ARINC circuit boards are installed
which do not have the same software version number.
Messages
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Change 1
INVALID CONFIGURATION - The FMS configuration is unknown.
This message can only occur on the ground.
INVALID FUEL CONFIG - The fuel flow sensor configuration is
invalid or incomplete. The fuel flow function will be disabled.
IC600L HEADING FAIL – In the Cessna Bravo, Cessna Ultra, or
Embraer 145, the heading source has failed while in use.
IC600R HEADING FAIL – In the Cessna Bravo, Cessna Ultra, or
Embraer 145, the heading source has failed while in use.
IC600-L BUS FAIL - In the Cessna Bravo, Cessna Ultra, or Embraer
145 configuration, label 371 does not have a valid SSM, or is not
detected on the left bus.
IC600-R BUS FAIL - In the Cessna Bravo, Cessna Ultra, or Embraer
145 configuration, label 371 does not have a valid SSM, or is not
detected on the right bus.
IRS # ALIGN - The specified IRS is in the alignment mode. The
aircraft must stay stationary.
IRS # ATTITUDE - The specified IRS is in the attitude reference
　
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