OPERATIONS MANUAL

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Fuel System Defueling Panel: Toggle switch directions are aircraft specific; the OFF and CLOSE functions may be in the upper or in the lower position. Center tank scavenge pump switch (guarded) (this switch is installed only on aircraft equipped with an electric scavenge pump) ON Pump is commanded to run. Auxiliary tank transfer switch (guarded) (this switch is installed only on aircraft equipped with an auxiliary tank) ON Fuel transfer is commanded to run. Reserve 2 & 3 transfer switch (guarded) (this switch is located in the middle of the panel if no electric scavenge pump and no auxiliary tank are installed) OPEN Valves are commanded to open. — Page 435 — For preview only. Not for sale. Many pages are intentionally removed.
Fuel System Transfer and Jettison Panels: Transfer main 1 & 4 switch (guarded) ON Valves are commanded to open to allow gravity transfer into main tanks 2 & 3. Fuel-to-remain selector Rotate Selects a total fuel value at which jettison will automatically stop. Value is indicated on EICAS when system is armed. Jettison nozzle valve switches ON Valve is commanded to open. VALVE LIGHT Valve unpowered or position disagreement. Jettison control selector OFF System is disarmed. A, B System is armed. MLW Fuel-to-remain is set for maximum landing weight. — Page 436 — 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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Air Systems Air Conditioning Contro
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Air Systems Air Conditioning Contro
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Automatic Flight System Overview: A
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Automatic Flight MCP: Vertical navi
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Automatic Flight MCP: Bank limit se
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Automatic Flight MCP: Altitude wind
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Automatic Flight Takeoff Operation:
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Auxiliary Power APU Control: Batter
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Communications ACP: (continued) Pus
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Communications RTP: (continued) HF
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Communications Cockpit Voice Record
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Communications Cabin Interphone Sys
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Communications ACARS - Basics: The
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Communications ACARS - Flight Plan
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Communications ACARS - OOOI Status
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Electrical Bus Tie System: (continu
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Electrical Battery Busses and Hot B
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Electrical Main Instrument Panel: A
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Electrical Overhead Panel: Bus tie
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Electrical APU Standby Bus System w
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Electrical DC Bus 2 - Equipment Lis
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Electrical DC Bus 3 - Equipment Lis
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Electrical Main Hot Battery Bus - E
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Electrical Main Standby Bus - Equip
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Electrical Ground Service Bus - Equ
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Electrical EICAS Messages: CAUTION
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Emergency Equipment Overhead Panel:
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Fire Protection Dual Loop Detectors
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Fire Protection Maintenance Panel:
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Fire Protection Fire and Overheat T
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Flight Controls Maintenance Panel:
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Flight Controls Aisle Stand: (In th
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Flight Controls Surface Position In
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Flight Controls Stabilizer Trim: Th
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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
Page 249 and 250: FMS RTE Page: (continued) 1L 2L 3L
Page 251 and 252: FMS RTE Page: (continued) 2L 3L 3R
Page 253 and 254: FMS DEP/ARR INDEX Page: 1L 3L 6L 1R
Page 255 and 256: FMS ARRIVALS Page (Active Route): 1
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Page 259 and 260: FMS LEGS Page: (continued) 6L Valid
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Page 263 and 264: FMS LEGS Page: (continued) Map view
Page 265 and 266: FMS LEGS Page: (continued) Direct-t
Page 267 and 268: FMS RTE DATA Page: 1L 2L 3L 4L 5L 6
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Page 271 and 272: FMS VNAV CLB Page: (continued) 3R 4
Page 273 and 274: FMS VNAV CRZ Page: (continued) 2L 3
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Page 277 and 278: FMS DESCENT FORECAST Page: 1L 2L 3L
Page 279 and 280: FMS OFFPATH DES Page: 1L 2L 3L 4L 5
Page 281 and 282: FMS INDEX Page: 1L 2L 3L 4L 5L 6L I
Page 283 and 284: FMS LOG Page: 1L 2L 3L 4L 5L 6L 1R
Page 285 and 286: FMS Sent REPORT Page (Message to Co
Page 287 and 288: FMS EMERGENCY REPORT Page: 1L 2L 3L
Page 289 and 290: FMS VERIFY EMERGENCY Page: Access:
Page 291 and 292: FMS ALT REQUEST Page (Message to Co
Page 293 and 294: FMS OFFSET REQUEST Page (Message to
Page 295 and 296: FMS VERIFY REQUEST Page for Navigat
Page 297 and 298: FMS WHEN CAN WE EXPECT Page (Messag
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Page 303 and 304: Fuel System EICAS Fuel Synoptics: F
Page 305 and 306: Fuel System Fuel Pumps: Main boost
Page 307 and 308: Fuel System EICAS Interface: The fu
Page 309 and 310: Fuel System Stabilizer Tank Operati
Page 311 and 312: Fuel System EICAS Messages: >FUEL A
Page 315 and 316: Hydraulics EICAS Hydraulic Synoptic
Page 317 and 318: Hydraulics EICAS Messages: CAUTION
Page 319 and 320: Ice & Rain Protection System Overvi
Page 321 and 322: Ice & Rain Protection Anti-Ice with
Page 323 and 324: Ice & Rain Protection EICAS Message
Page 325 and 326: Landing Gear Landing Gear — Page
Page 327 and 328: Landing Gear System Overview: (cont
Page 329 and 330: Landing Gear Autobrakes: The select
Page 331 and 332: Landing Gear Primary EICAS Gear Ind
Page 335 and 336: Navigation Systems Inertial Referen
Page 337 and 338: Navigation Systems Inertial Referen
Page 339 and 340: Navigation Systems Weather Radar Sy
Page 341 and 342: Navigation Systems ATC Transponder
Page 343 and 344: Navigation Systems DME System: Two
Page 345 and 346: Navigation Systems VOR and Marker B
Page 347 and 348: Navigation Systems EICAS Messages:
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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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