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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 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier_Global_000-Power_Plant
