OPERATIONS MANUAL

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Electrical Standby Busses: The devices that are most important are powered by standby busses. There is a main standby bus and an APU standby bus. Each standby system can use power from one of three independent sources. Effectively, these are, in the order of their priority: • AC bus 3 • AC bus 1 • Battery The power source selection is automatic when the standby power selector on the overhead panel is set to AUTO, which is assumed in the following description: When the main standby system cannot use AC bus 3, it uses power from the main battery charger; battery chargers are powered by AC bus 1 when available via the ground service bus (which, on the ground, may also use external or APU power). If the main battery charger is unusable either, the main standby system uses the main battery. The APU standby system uses AC bus 3 via the captain’s transfer bus which transfers to AC bus 1 on its own when necessary. If the captain’s transfer bus provides no power at all, the APU standby system uses the APU battery. At this stage the APU battery charger is already inoperative as the charger requires AC bus 1 power (if the ground service bus is not powered otherwise).—The APU standby bus powers the left FMC and the captain’s EFIS instruments. Some aircraft are fitted with an alternate EFIS selection system; when the selector is set to F/O, the APU standby system uses the first officer’s transfer bus instead of the captain’s, and redirects the APU standby power to the first officer’s instruments. Each standby bus system includes a static inverter that converts the 28 V DC from the battery or battery charger to 115 V AC. The static inverter of the APU standby system is switched off during APU start; this means, when AC bus 1 and 3 are not available, the respective instruments will be inoperative until the APU N2 RPM rises above circa 40%. This takes about 15 seconds. When the batteries are the only power sources in flight, they will provide power for at least 30 minutes. This is approximately the time required to glide from a high cruise altitude down to sea level. (In the simulator, discharged batteries can be promptly recharged on Instructor > Situation > Service with the button Service batteries.) — Page 188 — For preview only. Not for sale. Many pages are intentionally removed.
Electrical Main Instrument Panel: Alternate EFIS selector CAPT Powers the captain’s flight instruments and depowers the first officer’s flight instruments when the APU standby bus is powered by the APU hot battery bus. F/O Powers the first officer’s flight instruments and depowers the captain’s flight instruments when the APU standby bus is powered by the APU hot battery bus. Standby EFIS selector The standby EFIS selector functions in the same way as the alternate EFIS selector. — Page 189 — For preview only. Not for sale. Many pages are intentionally removed.
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® OPERATIONS MANUAL VERSION 10 For
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Simulator Handling Introduction: Pr
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Simulator Handling End User License
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Simulator Handling Starting the Sim
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Simulator Handling Java Look & Feel
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Simulator Handling User Files - Ove
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Simulator Handling Mouse - How to D
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Simulator Handling Mouse - How to Z
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Simulator Handling Mouse - How to A
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Simulator Handling Mouse - How to M
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Simulator Handling Mouse - How to T
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Simulator Handling Keyboard - Impor
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Simulator Handling Keyboard - Summa
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Simulator Handling Instructor > Sit
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Simulator Handling Instructor > Mod
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Simulator Handling Instructor > Mod
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Simulator Handling Instructor > Ana
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Simulator Handling Instructor > Lay
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Simulator Handling Instructor > Lay
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Simulator Handling Instructor > Net
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Simulator Handling Network Examples
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Simulator Handling Boost Server: Th
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Simulator Handling Instructor > Pre
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Simulator Handling Instructor > Abo
Page 91 and 92: Aircraft General Aircraft General
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Page 99 and 100: Air Systems Air Conditioning Contro
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Page 105 and 106: Automatic Flight System Overview: A
Page 109 and 110: Automatic Flight MCP: Vertical navi
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Page 113 and 114: Automatic Flight MCP: Altitude wind
Page 115 and 116: Automatic Flight Takeoff Operation:
Page 119 and 120: Auxiliary Power APU Control: Batter
Page 123 and 124: Communications ACP: (continued) Pus
Page 127 and 128: Communications RTP: (continued) HF
Page 129 and 130: Communications Cockpit Voice Record
Page 131 and 132: Communications Cabin Interphone Sys
Page 133 and 134: Communications ACARS - Basics: The
Page 135 and 136: Communications ACARS - Flight Plan
Page 137 and 138: Communications ACARS - OOOI Status
Page 139 and 140: Electrical Bus Tie System: (continu
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Page 145 and 146: Electrical Overhead Panel: Bus tie
Page 149 and 150: Electrical APU Standby Bus System w
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Page 155 and 156: Electrical DC Bus 3 - Equipment Lis
Page 157 and 158: Electrical Main Hot Battery Bus - E
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Page 161 and 162: Electrical Ground Service Bus - Equ
Page 163 and 164: Electrical EICAS Messages: CAUTION
Page 167 and 168: Emergency Equipment Overhead Panel:
Page 171 and 172: Fire Protection Dual Loop Detectors
Page 173 and 174: Fire Protection Maintenance Panel:
Page 177 and 178: Fire Protection Fire and Overheat T
Page 181 and 182: Flight Controls Maintenance Panel:
Page 183 and 184: Flight Controls Aisle Stand: (In th
Page 187 and 188: Flight Controls Surface Position In
Page 189 and 190: Flight Controls Stabilizer Trim: Th
Page 191 and 192: Flight Controls Rudder Control: Fla
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Flight Controls EICAS Messages: AIL
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Flight Instruments Integrated Displ
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Flight Instruments IDU Controls: Se
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Flight Instruments IDU Switching: (
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Flight Instruments Instrument Sourc
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Flight Instruments Instrument Sourc
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Flight Instruments Altitude Indicat
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Flight Instruments ND Symbology: (c
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Flight Instruments ND Symbology: (c
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Flight Instruments ND VOR Mode: In
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Flight Instruments ND Plan Mode - V
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Flight Instruments ND Position Chec
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Flight Instruments ND Test & Failur
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Flight Instruments Standby Attitude
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Flight Instruments Integrated Stand
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Flight Instruments Clock: Chronogra
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FMS IRS LEGS Page: 1L 2L 3L 4L 5L 6
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FMS ALTN NAV RADIO Page: 1L 2L 3L A
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FMS SELECT DESIRED WPT Page: 1L 2L
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FMS PROGRESS 2/3 Page: 1L 2L 3L 4L
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FMS NAV RADIO Page: 1L 2L 3L 1R 2R
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FMS FIX INFO Page: 1L 2L 3L 4L 5L 6
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FMS TAKEOFF REF Page: 1L 2L 3L 4L A
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FMS APPROACH REF Page: 1L 3L 4L 6L
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FMS MAINTENANCE INDEX Page: 1L 2L 3
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FMS RTE Page: 1L 3L 6L 1R 2R 3R 6R
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FMS RTE Page: (continued) 1L 2L 3L
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FMS RTE Page: (continued) 2L 3L 3R
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FMS DEP/ARR INDEX Page: 1L 3L 6L 1R
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FMS ARRIVALS Page (Active Route): 1
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FMS ARRIVALS Page (Active Route): (
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FMS LEGS Page: (continued) 6L Valid
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FMS LEGS Page: (continued) Single l
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FMS LEGS Page: (continued) Map view
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FMS LEGS Page: (continued) Direct-t
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FMS RTE DATA Page: 1L 2L 3L 4L 5L 6
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FMS VNAV CLB Page: (continued) 3R 4
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FMS VNAV CRZ Page: (continued) 2L 3
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FMS VNAV DES Page: Page title 1L 2L
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FMS DESCENT FORECAST Page: 1L 2L 3L
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FMS OFFPATH DES Page: 1L 2L 3L 4L 5
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FMS INDEX Page: 1L 2L 3L 4L 5L 6L I
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FMS LOG Page: 1L 2L 3L 4L 5L 6L 1R
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FMS Sent REPORT Page (Message to Co
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FMS EMERGENCY REPORT Page: 1L 2L 3L
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FMS VERIFY EMERGENCY Page: Access:
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FMS ALT REQUEST Page (Message to Co
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FMS OFFSET REQUEST Page (Message to
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FMS VERIFY REQUEST Page for Navigat
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FMS WHEN CAN WE EXPECT Page (Messag
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Fuel System Transfer and Jettison P
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Fuel System EICAS Fuel Synoptics: F
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Fuel System Fuel Pumps: Main boost
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Fuel System EICAS Interface: The fu
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Fuel System Stabilizer Tank Operati
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Fuel System EICAS Messages: >FUEL A
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Hydraulics EICAS Hydraulic Synoptic
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Hydraulics EICAS Messages: CAUTION
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Ice & Rain Protection System Overvi
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Ice & Rain Protection Anti-Ice with
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Ice & Rain Protection EICAS Message
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Landing Gear Landing Gear — Page
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Landing Gear System Overview: (cont
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Landing Gear Autobrakes: The select
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Landing Gear Primary EICAS Gear Ind
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Navigation Systems Inertial Referen
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Navigation Systems Inertial Referen
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Navigation Systems Weather Radar Sy
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Navigation Systems ATC Transponder
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Navigation Systems DME System: Two
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Navigation Systems VOR and Marker B
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Navigation Systems EICAS Messages:
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Power Plant Power Plant — Page 49
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Power Plant Forward Thrust Levers a
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Power Plant Electronic Engine Contr
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Power Plant Electronic Engine Contr
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Power Plant Ignition Control - GE M
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Power Plant Ignition Control - RR M
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Power Plant Primary EICAS Display -
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Power Plant Primary EICAS Display -
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Power Plant Secondary Engine Displa
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Power Plant Compact Engine Indicati
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Warning Systems EICAS Messages: (co
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Warning Systems EICAS Messages: (co
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Warning Systems EGPWS: The aircraft
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Warning Systems EGPWS - Mode 2: 245
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Warning Systems EGPWS - Terrain Cle
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Warning Systems EGPWS - Terrain Ale
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Warning Systems EGPWS - Aural Messa
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Limitations Approved low visibility
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Procedures Two Engines Inoperative
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Procedures Normal Procedures (Examp
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Procedures First Officer - Cockpit
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Abnormal Lists Air Systems: — Pag
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OPERATIONS MANUAL

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