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has occurred, other
than an overspeed or
over temperature.
APU OIL LO QTY
Indicates that the APU
oil level has reached
3.5 quarts ( 2 quarts
low).
APU BLEED DISABLED
Indicates that the LCV
command has been
received and either:
The inlet pressure is
less than 3.3 psia
(35,000 ft).
The 60 second
warm−up period (on
ground only) is in
progress.
APU IN BITE
Indicates that RUN is
selected and the
prestart BITE is in
progress.
APU BLEED ON
Indicates that the APU
BLEED switch is in the
ON position and the
load control valve is
open.
APU FAULT
Indicates a failure in
one of the following:
Single speed
sensor.
EGT thermocouple.
Fuel solenoid (failed
to close).
Fuel/oil filters in
impending by−pass.
Low oil pressure
switch has failed
(in flight).
APU FADEC FAIL
Indicates that no data
is received by the DAU.
APU NOT AVAILABLE
Indicates that when
START or RUN is
selected,
checks/testing is in
progress.
APU BLEED OFF
Indicates that the APU
BLEED switch is in the
OFF position and the
load control valve is
closed.
APU FADEC FAIL
APU OIL LO QTY
APU NOT AVAILABLE
APU BLEED DISABLED
APU SHUTDOWN
APU FAULT
APU IN BITE
APU BLEED ON
APU BLEED OFF
AUXILIARY POWER UNIT
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
05−10−23
AUXILIARY POWER UNIT
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
05−10−24
THIS PAGE INTENTIONALLY LEFT BLANK
CB - APU SYSTEM
GF0520_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
BRT
FIRE
FLIGHT CONTROLS
FUEL
APU DOOR
CB − APU SYSTEM 1/1
APU BATT ASCA
APU FADEC PWR 1 BATT
APU FADEC PWR 2 AV BATT DCPC
APU OIL HEAT AC 4
APU START BATT
APU START CONTACT APU BATT ASCA
IN
IN
IN
IN
IN
IN
AUXILIARY POWER UNIT
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
05−20−1
AUXILIARY POWER UNIT
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
05−20−2
THIS PAGE INTENTIONALLY LEFT BLANK
DESCRIPTION
General 06−10−1
Interphone Communication 06−10−1
Flight Compartment Speakers 06−10−1
Flight Crew Intercom 06−10−1
Service Intercom Panels 06−10−2
Forward External Services Panel Interphone Station 06−10−2
Aft External Services Panel Interphone Station 06−10−3
Aft Equipment Bay Interphone Station 06−10−3
Avionics Bay Interphone Station 06−10−3
Control Wheel Radio Key / Control Wheel Toggle Switch (If Installed) 06−10−4
Audio Control Panel 06−10−4
Audio Control Panel Input Schematic 06−10−4
Audio Control Panel Switch Operation 06−10−5
Transmit/Emer 06−10−5
Microphone Selection 06−10−5
Speaker/Headphone 06−10−5
Radio Communication System 06−10−6
VHF 1 and 2 Communications Systems 06−10−6
VHF 3 Communications System (On airplanes with SB 700-23-002
incorporated) 06−10−6
Integrated Radio System 06−10−7
Integrated Radio System Schematic 06−10−7
Radio Management Unit (RMU) Display 06−10−8
Radio Management System 06−10−9
General Colour Philosophy 06−10−10
Transfer Keys 06−10−11
Line Select Keys 06−10−11
Function Keys and Tuning Knobs 06−10−11
Function Keys 06−10−12
Direct COM Tuning 06−10−18
COM Memory 06−10−19
High Frequency (HF) Communication System 06−10−20
RMU HF Display 06−10−20
HF Preset and Direct Tuning Modes 06−10−21
HF Fault Annunciation 06−10−21
Menu Page 06−10−22
COMMUNICATIONS
TABLE OF CONTENTS
CHAPTER 6
06−00−1
　
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