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VFLC Vertical navigation mode, FMS VNAV is valid and flight level change overspeed mode is
active (flashes).
VGP Vertical navigation mode and glide path are captured.
VPATH Vertical navigation mode − capturing/tracking a vertical path.
VPTCH Vertical navigation mode selected and pitch mode is active..
VNAV Vertical navigation mode, and FMS VNAV is invalid (annunciated in the vertical arm
field).
VS Vertical speed mode − active.
VVS Vertical navigation mode selected and vertical speed mode is active.
YD Both yaw damper channels are disengaged or have failed.
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−52
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
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 04−10−53
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−54
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY
SYSTEM SUB-SYSTEM CB NAME BUS BAR
CB
PANEL
CB LOCATION NOTES
Integrated Avionics
Processing System
Left IAPS
L IAPS AFCS 2
FMS 1
DC BUS 1
1
K4
L IAPS AFCS 1
MDC DC BATT
Q4
L IAPS FAN Q5
Right IAPS
R IAPS AFCS 2
FMS 2
DC BUS 2 2 K3
R IAPS AFCS 1
DC ESS 4
D3
L IAPS FAN D2
AUTOMATIC FLIGHT CONTROL SYSTEM
Summary
Vol. 2 04−20−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
AUTOMATIC FLIGHT CONTROL SYSTEM
Summary
Vol. 2 04−20−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
DESCRIPTION APU 100E
General 05−10−1
APU Enclosure 05−10−1
Power Section and Accessory Gearbox 05−10−2
Description 05−10−2
Components and Operation 05−10−2
Generator Adapter 05−10−4
Description 05−10−4
Components and Operation 05−10−4
Air Intake and Exhaust 05−10−6
Description 05−10−6
Components and Operation 05−10−6
APU Fuel Distribution 05−10−8
Description 05−10−8
Components and Operation 05−10−8
Start and Ignition 05−10−12
Description 05−10−12
Components and Operation 05−10−12
Pneumatic Supply 05−10−20
Description 05−10−20
Components and Operation 05−10−20
Controls and Indicators 05−10−22
EICAS Messages 05−10−24
DESCRIPTION APU 150
General 05−15−1
APU Enclosure 05−15−1
Power Section and Accessory Gearbox 05−15−2
Description 05−15−2
Components and Operation 05−15−2
Generator Adapter 05−15−4
Description 05−15−4
Components and Operation 05−15−4
Air Intake and Exhaust 05−15−6
Description 05−15−6
AUXILIARY POWER UNIT
Table of Contents
Vol. 2 05−00−1
REV 76, Jul 17/09
CHAPTER 5 - AUXILIARY POWER UNIT
05−00−1
CL−604 Operating Manual
　
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