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CSP 700−6
Volume 2
04−10−30
AUTOPILOT - FLIGHT DIRECTOR EICAS MESSAGES
YD 1−2 FAIL
Indicates that yaw
damper 1 (2) has failed.
AFCS ENGAGE INVAL
Indicates that fault
warning computer detects
invalid autopilot
engagement.
AP PITCH TRIM FAIL
Indicates that autopilot
pitch trim is inoperative.
AP TRIM IS NU− ND
Indicates that autopilot pitch mistrim
monitor detects excessive forces.
YD OFF
Indicates that fault warning
computer detects that no
yaw damper is engaged.
AP TRIM IS LWD − RWD
Indicates that autopilot roll
mistrim monitor detects
excessive forces.
GF0410_095
AP PITCH TRIM FAIL
AP TRIM IS NU
AP TRIM IS ND
AP TRIM IS LWD
AP TRIM IS RWD
AFCS ENGAGE INVAL
YD 1 FAIL
YD 2 FAIL
YD OFF
AUTOMATIC FLIGHT CONTROL SYSTEM
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
04−10−31
AUTOPILOT - FLIGHT DIRECTOR EICAS MESSAGES (CONT'D)
AFCS 1−2 FAIL
Indicates that AFCS (one or both) functions has
failed.
YD NOT CENTERED
Indicates that the YD linear actuator is
not centered while on the ground.
AP 1−2 FAIL
Indicates that the affected autopilot
has failed.
GF0410_096
AFCS 1 FAIL
AFCS 2 FAIL
AP 1 FAIL
AP 2 FAIL
YD NOT CENTERED
AUTOMATIC FLIGHT CONTROL SYSTEM
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
04−10−32
CB - AFCS SYSTEM
GF0420_001
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
BUS
CIRCUIT BREAKER − SYSTEM 1/2
CIRCUIT BREAKER SYSTEM
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
BRT
A/T CTLR
CB − AFCS SYSTEM 1/3
AC 1 CCBP
A/T SERVOS DC 1
AP 1 SERVOS DC 1
AP 2 SERVOS DC 2
GUID PANEL CH 1 BATT
GUID PANEL CH 2 DC ESS
IN
IN
IN
IN
IN
IN
IAC 1
CB − AFCS SYSTEM 2/3
BATT
IAC 2 DC ESS
IAC 3 BATT
YD 1 BATT
YD 2 DC ESS
YD HEAT 1 DC 1
IN
IN
IN
IN
IN
IN
YD HEAT 2
CB − AFCS SYSTEM 3/3
DC 2 IN
AUTOMATIC FLIGHT CONTROL SYSTEM
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
04−20−1
AUTOMATIC FLIGHT CONTROL SYSTEM
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
04−20−2
THIS PAGE INTENTIONALLY LEFT BLANK
DESCRIPTION
General 05−10−1
APU Access and Component Location 05−10−2
APU Compartment 05−10−2
APU General Arrangement 05−10−3
APU System Schematic 05−10−3
Lubrication 05−10−4
Oil Pressure 05−10−4
Gravity Oil Fill 05−10−4
Oil Replenishment System 05−10−4
Oil Replenishment System Filling 05−10−6
Oil Replenishment Panel 05−10−7
Operation 05−10−7
Fuel Control and Indication 05−10−8
Airframe Fuel 05−10−8
Ignition 05−10−9
Start System 05−10−9
Speed Indication 05−10−9
Temperature Indication 05−10−9
Hourmeter/Cycle Counter 05−10−9
ECU Component Control Schematic 05−10−10
Control System 05−10−10
Pneumatic 05−10−10
APU System Operating Modes 05−10−11
ECU Powerup
05−10−11
Start Mode 05−10−11
Onspeed
Mode 05−10−11
Cooldown Mode 05−10−11
Shut down Mode 05−10−11
APU System Operating Sequence 05−10−11
APU Starting 05−10−11
APU Door Positioning 05−10−11
APU Loading 05−10−12
APU Shut down 05−10−12
APU Door Operation and Indication 05−10−13
Door Operation 05−10−13
Door Indication 05−10−13
AUXILIARY POWER UNIT
TABLE OF CONTENTS
CHAPTER 5
05−00−1
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
05−00−1
Page
TABLE OF CONTENTS
DESCRIPTION
APU RPM and EGT Indications 05−10−13
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