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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 Lock-Out 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
Auto-Relight 18.10.66
Quick Relight 18.10.66
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
18.00.2 CSP 700.5000.6
POWER PLANT
TABLE OF CONTENTS
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
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
POWER PLANT
TABLE OF CONTENTS
THIS PAGE INTENTIONALLY LEFT BLANK
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
POWER PLANT
GENERAL
The Global 5000 airplane is powered by two BMW.Rolls Royce BR 700.710A2.20 engines, each mounted on a pylon on either side of the rear fuselage.
The engine is an axial flow, dual shaft turbofan, with a 4.0:1 bypass ratio, rated at 14,750 lbs of thrust at sea level to ISA +20.
The BR 700.710A2.20 engine contains two main rotating assemblies (spools), a single stage low pressure (LP) fan driven by a two stage turbine and a ten stage high pressure (HP) compressor, driven by a two stage turbine. The HP spool provides an external drive for the accessories mounted on the accessory gearbox.
The engine is made up of eight modules as follows:
.
Fan assembly.
.
Fan case.
.
Intermediate case.
.
HP Compressor.
.
HP Turbine and combustion chamber.
.
LP Turbine and shaft.
.
Accessory Gearbox (AGB).
.
Bypass duct.
Each engine provides bleed air extraction, from either the 5th stage or the 8th stage of compression, for Air Conditioning and Pressurization, Cowl and Wing anti-icing and/or engine starts.
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