DESCRIPTION
General 18−10−1
Engine Assembly and Airflow 18−10−2
Engine Modules 18−10−3
Engine Bleed Air System 18−10−4
Engine Oil System 18−10−5
Engine Oil Heat Management System 18−10−6
Oil Replenishment System 18−10−7
Oil Replenishment Panel 18−10−8
Oil Replenishment Schematic 18−10−9
Operation 18−10−9
Engine Fuel System 18−10−10
Fuel System Schematic 18−10−11
Full Authority Digital Engine Control (FADEC) 18−10−12
Engine Electronic Controller (EEC) 18−10−13
Engine Indications 18−10−15
Engine Pressure Ratio (EPR) 18−10−16
EPR Control 18−10−17
EPR Indication 18−10−17
EPR Rating Mode Selection 18−10−18
SYNC Mode Selection 18−10−18
FMS Selection (EPR) 18−10−19
N1 (Fan) 18−10−20
N1 Control 18−10−21
N1 Indication 18−10−21
Inter Turbine Temperature (ITT) 18−10−22
ITT Indication 18−10−23
N2 (HP Compressor) 18−10−24
N2 Indication 18−10−25
Fuel Flow 18−10−25
Fuel Flow Indication 18−10−26
Oil Temperature 18−10−26
Oil Temperature Indication 18−10−26
Oil Pressure 18−10−26
Oil Pressure Indication 18−10−26
Engine Vibration Monitoring System (EVMS) 18−10−27
EVMS Indication 18−10−27
POWER PLANT
TABLE OF CONTENTS
CHAPTER 18
18−00−1
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
18−00−1
Page
TABLE OF CONTENTS
DESCRIPTION
Thrust Management 18−10−28
Thrust Levers 18−10−30
Autothrottle System 18−10−32
Autothrottle Data Sources 18−10−33
Limiting 18−10−33
Monitoring 18−10−33
A/T 1 or 2 Select 18−10−34
A/T Engagement/Disengagement 18−10−34
A/T Mode Operation 18−10−37
Takeoff
Thrust Control Mode 18−10−38
Takeoff
Thrust Hold Control Mode 18−10−38
Flight Level Change Thrust Control Mode 18−10−39
Airspeed Control Mode 18−10−40
Retard Mode 18−10−41
Go Around Thrust Control Mode 18−10−41
Electronic Thrust Trim System (ETTS) 18−10−42
N1 SYNC ON 18−10−42
N2 SYNC ON 18−10−43
EPR CMD SYNC ON 18−10−43
N1, N2, EPR CMD SYNC OFF 18−10−44
SYNC Annunciation 18−10−44
Thrust Reverser System 18−10−45
Thrust Reverser 18−10−46
Reverse Thrust Operation 18−10−47
Reverser Components 18−10−48
Isolation Control Unit 18−10−48
Directional Control Unit 18−10−48
Reverse Thrust Levers 18−10−50
Reverser System LockOut
18−10−51
Starting and Ignition 18−10−52
Starter Air Valve (SAV) 18−10−54
Air Turbine Starter (ATS) 18−10−54
Ignition System 18−10−55
Engine Run Switches 18−10−56
Engine Starting 18−10−58
Engine Shutdown 18−10−63
Dry Cranking 18−10−64
Wet Cranking 18−10−64
Starting Anomalies 18−10−65
AutoRelight
18−10−66
Quick Relight 18−10−66
POWER PLANT
TABLE OF CONTENTS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
18−00−2
Page
DESCRIPTION
Engine Fire Detection System 18−10−67
Engine Limit Exceedance Display 18−10−68
Power Plant EICAS Messages 18−10−69
EMS CIRCUIT PROTECTION
CB − Engine System 18−20−1
CB − Oil System 18−20−2
CB − Thrust Rev System 18−20−3
POWER PLANT
TABLE OF CONTENTS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
18−00−3
Page
POWER PLANT
TABLE OF CONTENTS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
18−00−4
THIS PAGE INTENTIONALLY LEFT BLANK
GENERAL
The Global 5000 airplane is powered by two BMW−Rolls Royce BR 700−710A2−20 engines, each
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：Bombardier_Global_000-Power_Plant
