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VALVE OVERFLOW
CONTAINER
GROUND SERVICE
SUCTION
GROUND SERVICE
PRESSURE
TEMPERATURE
TRANSDUCER
PRESSURE
FILTER
PRESSURE
MANIFOLD
P
T
S S
T
CHECK
VALVE
Vol. 1 14--30--3
HYDRAULIC POWER
System 3 REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
A. AC Motor Pumps
Hydraulic system No. 3 AC motor pumps (ACMPs) are controlled by switches on the
hydraulic control panel. ACMP 3A runs continuously to maintain normal system
pressure. ACMP 3B operates during takeoffs and landings. The ADG bus
automatically powers ACMP 3B when the ADG is deployed (independent of the flight
compartment 3B switch setting).
Hydraulic Control Panel
Figure 14---30---2
AC Motor Pump 3A
Used to control the operation
of AC motor pump 3A.
ON -- Pump will operate at
3000 psi output.
OFF -- Pump inoperative.
Hydraulic Pump Panel
Overhead Panel
AC Motor Pump 3B
Used to control the operation
of AC motor pump 3B. Pump
will operate irrespective of
switch position when ADG is
deployed.
ON -- Pump will operate at
3000 psi output.
OFF -- Pump inoperative.
AUTO -- Pump will operate
in AUTO position, when
flaps are greater than
0--degrees and either
IDG 1 or IDG 2 is operating.
Vol. 1 14--30--4
HYDRAULIC POWER
System 3 Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
Hydraulic Synoptic Page
Figure 14---30---3
Green -- Sufficient
Blank -- Insufficient
Reservoir Output Line
quantity ( 5 ).
quantity ( 5 ).
BRT
System Distribution Table
Displays status of
corresponding airplane
systems.
White -- Adequate
pressure to operate
( 1800 psi).
Amber -- Hydraulic supply
to system inadequate
( 1800 psi).
Half--intensity magenta --
Invalid data.
Hydraulic Pressure
Displays hydraulic pressure
(in 100 psi increments).
Normal operating pressure
is 2800 to 3200 psi.
White -- Hydraulic
pressure 3200 psi.
Green -- Hydraulic
pressure 1800 psi and
3200 psi.
Amber -- Hydraulic
pressure 1800 psi.
Amber dashes -- Invalid
data.
Pump Output and
Pressure Manifold Lines
Green -- Pressure
1800 psi.
Amber -- Low pressure
( 1800 psi).
quantity 45 and
Amber dashes -- Invalid
Hydraulic Quantity
Displays reservoir fluid
quantity (in 5 increments).
Normal quantity is 45 to 85
percent.
White -- Hydraulic quantity
45 or 85 .
Green -- Hydraulic
85 .
data.
Hydraulic Temperature
Displays reservoir fluid
temperature (in 1 C
increments).
Amber -- Pump output low.
Pump
Displays pump status.
White -- Pump not
operating and selected off.
Green -- Pump output
normal.
Half--intensity magenta --
Invalid data.
Hydraulic Page
Vol. 1 14--30--5
HYDRAULIC POWER
System 3 Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
Hydraulic EICAS Indications <1001>
Figure 14---30---4
HYD PUMP 3A or 3B caution (amber)
Indicates that corresponding AC motor pump
has a low pressure output ( 1800 psi).
HYD 3 HI TEMP caution (amber)
Indicates that corresponding system has a
fluid temperature of 96 C (205 F) or greater.
HYD 3 LO PRESS caution (amber)
Indicates that corresponding system
pumps (both AC motor pumps) have a low
pressure output ( 1800 psi).
BRT
Primary Page
Vol. 1 14--30--6
HYDRAULIC POWER
System 3 Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
B. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Pumps
HYD SYST AC
PUMP CONT
3A
DC BUS 2 2 F14
Hydraulic
System 3
HYD SYST AC
PUMP CONT
3B
DC BUS 1
1
F11
Indication HYD SYST
IND 3
BATTERY
BUS
L8
Vol. 1 15--00--1
ICE AND RAIN PROTECTION SYSTEM
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
CHAPTER 15 --- ICE AND RAIN PROTECTION SYSTEM
Page
TABLE OF CONTENTS 15--00
Table of Contents 15--00--1
INTRODUCTION 15--10
Introduction 15--10--1
ICE DETECTION SYSTEM 15--20
Ice Detection System 15--20--1
System Circuit Breakers 15--20--5
WING ANTI-ICE SYSTEM 15--30
Wing Anti--Ice System 15--30--1
System Circuit Breakers 15--30--6
　
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