曝光台 注意防骗
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detected by the anti--ice and leak
detection controller.
ANTI--ICE
DUCT
BLEED
AIR DUCT
L or R BLEED DUCT warning (red)
Indicates a bleed air leak has been
detected by the anti--ice and leak
detection controller in the respective
engine bleed ducting.
ANTI--ICE DUCT caution (amber)
Indicates bleed shutdown after bleed leak
detected and system not selected off.
L or R BLEED DUCT caution (amber)
Indicates respective bleed shutdown
after bleed leak detected and system
has not been reconfigured.
Primary Page
Vol. 1 19--30--4
PNEUMATIC
Bleed Air Leak Detection Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
Bleed Air Leak Detection --- Loop EICAS Indication <1001>
Figure 19---30---3
L COWL LOOP
R COWL LOOP
L BLEED LOOP
R BLEED LOOP
L (R) BLEED LOOP Caution (amber)
Indicates a loss of both left or right engine bleed
air leak detection loops during power--up test.
ANTI--ICE LOOP caution (amber)
Indicates loss of both wing anti--ice leak
detection loops during power--up test.
L (R) COWL LOOP Caution (amber)
Indicates a loss of both left or right cowl bleed
air leak detection loops during power--up test.
DUCT MON FAULT status (white)
Indicates a loss of redundancy in
bleed leak detection system.
Primary Page
ANTI--ICE LOOP
Status Page
Vol. 1 20--00--1
POWER PLANT
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
CHAPTER 20 --- POWER PLANT
Page
TABLE OF CONTENTS 20--00
Table of Contents 20--00--1
INTRODUCTION 20--10
Introduction 20--10--1
THRUST CONTROL 20--20
Thrust Control 20--20--1
Thrust Levers 20--20--1
Full Authority Digital Electronic Control 20--20--3
Automatic Power Reserve 20--20--6
High Power Schedule 20--20--7
N1 and N2 Synchronization 20--20--7
Engine Overspeed Protection 20--20--8
Engine N2 Indications When Using Wing Anti--ice 20--20--8
System Circuit Breakers 20--20--11
STARTING AND IGNITION SYSTEMS 20--30
Starting and Ignition Systems 20--30--1
Starting System 20--30--1
Ignition System 20--30--2
Start Protection 20--30--2
System Circuit Breakers 20--30--5
OIL SYSTEM 20--40
Oil System 20--40--1
Oil Replenishing System 20--40--6
System Circuit Breakers 20--40--7
FUEL SYSTEM 20--50
Fuel System 20--50--1
INTERTURBINE TEMPERATURE (ITT) MONITORING 20--55
Interturbine temperature (ITT) Monitoring 20--55--1
VIBRATION MONITORING 20--60
Vibration Monitoring 20--60--1
System Circuit Breakers 20--60--4
REVERSE THRUST 20--70
Reverse Thrust 20--70--1
System Circuit Breakers 20--70--4
Vol. 1 20--00--2
POWER PLANT
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
LIST OF ILLUSTRATIONS
INTRODUCTION
Figure 20--10--1 Power Plant -- Cross--section 20--10--2
THRUST CONTROL
Figure 20--20--1 Thrust Control -- Thrust Levers 20--20--1
Figure 20--20--2 Thrust Control -- Throttle Quadrant Settings 20--20--2
Figure 20--20--3 Thrust Control -- N1 & N2 Readout Scale and Pointer 20--20--2
Figure 20--20--4 FADEC/FMU Interface 20--20--4
Figure 20--20--5 Thrust Control N1 Reference Bug and Readout 20--20--5
Figure 20--20--6 Thrust Control Automatic Performance Reserve 20--20--6
Figure 20--20--7 High Power Schedule Pushbutton 20--20--7
Figure 20--20--8 Engine Synchronization Switch --
Engine/Micscellaneous Test Panel 20--20--8
Figure 20--20--9 Thrust Control Engine Overspeed Warning 20--20--9
Figure 20--20--10 Thrust Control APR CDM Set Caution 20--20--10
STARTING AND IGNITION SYSTEMS
Figure 20--30--1 Starting and Ignition Systems Block Diagram 20--30--1
Figure 20--30--2 Starting and Ignition System -- Controls 20--30--2
Figure 20--30--3 Primary Page -- ITT Readout Scale and Pointer 20--30--3
Figure 20--30--4 L or R Start Abort and Ignition EICAS Messages 20--30--4
OIL SYSTEM
Figure 20--40--1 Oil Distribution System -- Schematic 20--40--2
Figure 20--40--2 Oil System -- Oil Temp and Pressure EICAS Indications 20--40--3
Figure 20--40--3 Oil System -- Oil Test and Oil Levels Controls
and Indications 20--40--4
Figure 20--40--4 Oil System -- EICAS Indications 20--40--5
Figure 20--40--5 Oil Replinishment System <1213> 20--40--6
FUEL SYSTEM
Figure 20--50--1 Fuel system -- EICAS Indications 20--50--2
Figure 20--50--2 Fuel Distribution System -- Schematic 20--50--3
INTERTURBINE TEMPERATURE (ITT) MONITORING
Figure 20--55--1 Interturbine Temperature (ITT)
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