OPERATIONS MANUAL

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Electrical APU Standby Bus System without Alternate EFIS Selector: APU STBY BUS XFR RELAY APU START RELAY BAT SWITCH OFF AUTO BAT APU HOT BAT J6 APU INV XFR RELAY REMOTE ON/OFF (GND=OFF) STATIC INV APU B26 APU STBY C1 FMC L J5 XFR CAPT A8 F13 PFD L F12 ND L OFF AUTO BAT J4 APU STBY BUS VOLTAGE SENSE BAT SWITCH FMC ND PFD STBY BUS STATIC INV XFR CAPT XFR RELAY BATTERY SWITCH FLIGHT MANAGEMENT COMPUTER NAVIGATION DISPLAY PRIMARY FLIGHT DISPLAY STANDBY BUS STATIC INVERTER (28V DC TO 115V AC) TRANSFER BUS OF CAPTAIN TRANSFER RELAY BUS WITH AC (115V) BUS WITH DC (28V) AUTO OFF BAT SWITCH ELEMENT OF STANDBY POWER SELECTOR CIRCUIT BREAKER (CB) ON P7 PANEL CIRCUIT BREAKER (CB) ON P6 PANEL REMOTE CONTROL CIRCUIT BREAKER (RCCB), CONTROLLED ON P6 — Page 201 — For preview only. Not for sale. Many pages are intentionally removed.
Some pages are intentionally removed. This document is for preview only. 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
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Aircraft General Aircraft General
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Aircraft General Main Panel Lightin
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Aircraft General Glareshield Panel
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Page 99 and 100: Air Systems Air Conditioning Contro
Page 101 and 102: 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
Page 111 and 112: Automatic Flight MCP: Bank limit se
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
Page 141 and 142: Electrical Battery Busses and Hot B
Page 143 and 144: Electrical Main Instrument Panel: A
Page 145 and 146: Electrical Overhead Panel: Bus tie
Page 149: Electrical APU Standby Bus System w
Page 153 and 154: Electrical DC Bus 2 - Equipment Lis
Page 155 and 156: Electrical DC Bus 3 - Equipment Lis
Page 157 and 158: Electrical Main Hot Battery Bus - E
Page 159 and 160: Electrical Main Standby Bus - Equip
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
Page 193 and 194: Flight Controls EICAS Messages: AIL
Page 195 and 196: Flight Instruments Integrated Displ
Page 197 and 198: Flight Instruments IDU Controls: Se
Page 199 and 200: 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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