CAS Advisory Message
Meaning, Effects and Possible Actions
FMS Synch Error
FMS1 and FMS2 are operating independently (not
synchronized). Non-coupled FMS will not receive any
changes made to the flight plan. See Section 7-33,
, for a description of how to synchronize
FMS1 and FMS2.
*
Gear Control Fault
Indicates loss of redundancy in landing gear control system,
such as a stuck landing gear selector position switch. Gear
will still function normally with a single fault.
Takeoff Config
Takeoff configuration incorrect. Correct prior to takeoff.
*
Pusher Safe Mode
Stick pusher computer has gone into pusher safe mode. Stall
warning trigger thresholds operate at the 0° flap position
settings irrespective of the flap position.
*
*
*
LH OAT Fail
RH OAT Fail
LH+RH OAT Fail
Loss of total and static air temperature from ADAHRS
Channel A or B or A and B. Refer to Section 3,
for more information.
*
*
*
LH PFD CTRL Fail
RH PFD CTRL Fail
LH+RH PFD CTRL Fail
Cross check PFD data with Electronic Standby Instrument
System (ESIS). Use Touch Screen Controller / MF Controller
to operate Radio window. Use PFD knob on serviceable PFD
Controller to set up both Pilot and Copilot PFD.
(In Flight Only)
FLT CTRL Ch A Fail
FLT CTRL Ch B Fail
FLT CTRL Ch A+B Fail
Single channel failure has no effect.
Dual channel failure results in loss of AP/FD/YD.
*
*
*
GPS 1 Fail
GPS 2 Fail
GPS 1+2 Fail
GPS has no satellite signal reception or GPS unit failed. If
CAS message does not clear after approx. 2 mins:
For Single GPS installation: Use remaining operational
navigation equipment as required.
For Dual GPS installation: If single GPS fail, the FMS will
automatically select the alternate GPS. If needed, select
alternate GPS on Sensors page.
For Dual GPS installation: If dual GPS fail: Use remaining
operational navigation equipment as required.
Open the circuit breaker of the failed GPS (GPS 1 Standby
Bus
L
V3 and/or GPS 2 Avionic 2 Bus
R
X1), wait 5 seconds
then close the circuit breaker.
Note
The FMS will use ADAHRS data to dead reckon, based
on the previously known GPS position prior to the failure.
Traffic Fail
Loss of TCAS.
TAWS Fail
Loss of TAWS.
Terr Inhib Active
Terrain alerting Inhibit selected.
Terr Inhib not Avail
Terrain alerting visual and aural inhibit is not available.
No Altitude Reporting
XPDR not transmitting altitude. Select TA on Radio window
or ALT if no TCAS system is installed.
Flameout
Indicates an uncommanded engine flameout has been
detected.
Section 3A - Abnormal Procedures (EASA Approved)
CAS Advisories
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 3A-2-3
12-C-A15-48-0302-00A-014A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY