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speed mode activated
SPEED
VMO LIMIT
Green – Steady
Amber – Flashing
ATS protecting VMO limit,
speed mode activated
MSD Error Messages
The following MSD error messages may be displayed, with only one error message displayed at a
time. If multiple error conditions exist, that error condition must be corrected in order to display the
next message.
If an amber fail message is displayed, the ATS pushbutton can be pressed and held until a fail
fault message is displayed, to help in troubleshooting the failure.
The following table describes the error messages and color logic, but does not cover the definition
of each message due to the complexity of interface between components and systems
configuration. Reference should be obtained from the Aircraft Maintenance Manual for message
definition description.
Mode Status Display Error Messages
MESSAGE COLOR/STATE
ADC ERR Amber – Steady
AFCS ERR Amber – Steady
AOA ERR Amber – Steady
ATS COMM FAIL Green – Steady
Amber – Steady
BRAKE ERR Amber – Steady
FCC ERR Amber – Steady
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−73
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
AUTOTHROTTLE SYSTEM (CONT'D)
MESSAGE COLOR/STATE
FLAPS ERR Amber – Steady
FMC ERR Amber – Steady
GEAR ERR Amber – Steady
IRS ERR Amber – Steady
PFD ERR Amber – Steady
SERVO ERR Amber – Steady
SW ERR Amber – Steady
EICAS MESSAGES
MESSAGE MEANING AURAL WARNING (IF ANY)
AFCS MSGS FAIL No valid AFCS messages received from either IAPS
side.
WARNING
“Triple Chime”
CONFIG AP Autopilot is engaged with the aircraft in takeoff mode. “CONFIG AUTOPILOT”
AP TRIM IS LWD Autopilot is engaged with a left wing down out-of-trim condition.
AP TRIM IS ND Autopilot is engaged with a nose down out-of-trim condition.
AP TRIM IS NU Autopilot is engaged with a nose up out-of-trim condition.
AP TRIM IS RWD Autopilot is engaged with a right wing down out-of-trim condition.
AP PITCH TRIM Autopilot pitch trim function has failed.
YAW DAMPER Both yaw damper channels are disengaged or failed.
AFCS 1 INOP
The respective automatic flight control system is inoperative.
AFCS 2 INOP
FD 1 FAIL
Respective flight director is inoperative.
FD 2 FAIL
IAPS DEGRADED One or more IAPS quadrant(s) failed, with either WOW or both PSEU channel
invalid.
IAPS OVERTEMP Overtemperature condition in one or more IAPS quadrant(s).
YD 1 INOP Respective yaw damper channel is off or failed and the other channel is engaged
YD 2 INOP and not failed.
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−74
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY
SYSTEM SUB-SYSTEM CB NAME BUS BAR
CB
PANEL
CB LOCATION NOTES
Integrated Avionics
Processor System
Left IAPS L IAPS AFCS 2
FMS 1
DC BUS 1 1 M2
L IAPS AFCS 1
MDC
DC BATT 1 Q4
L IAPS FAN DC BATT 1 Q5
AFCS 2 DC BUS 1 1 K4
Right IAPS R IAPS AFCS 2
FMS 2
DC BUS 2 2 K3
R IAPS AFCS 1
FMS 3
DC ESS 4 D3
R IAPS FAN DC ESS 4 D2
AUTOMATIC FLIGHT CONTROL SYSTEM
Summary
Vol. 2 04−20−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
AUTOMATIC FLIGHT CONTROL SYSTEM
Summary
Vol. 2 04−20−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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