OPERATIONS MANUAL

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Power Plant Secondary Engine Display – RR Model: Fuel-on indicator (shows minimum N2 at which the fuel control switch should be set to RUN during start; blanks when set to RUN). X-BLD flag is shown in flight when windmilling start is not possible and cross-bleed air is required for starter motor. Current N2 Oil pressure in psi (caution range in amber, operating limit in red) Oil temperature in °C (caution range in amber, operating limit in red) Current N3 N3 operating limit Maximum N3 Current N3 Fuel flow in: kg x 1000 / hour lb x 1000 / hour Oil quantity in liters or US quarts (magenta when abnormal) Highest vibration level and the related source: • FAN (fan vibration) • LPT (N1 rotor vibration) • N2 (N2 rotor vibration) • N3 (N3 rotor vibration) • BB (broadband, source unknown) — Page 516 — For preview only. Not for sale. Many pages are intentionally removed.
Power Plant Compact Engine Indications – GE Model: Shown when only one IDU is available for EICAS displays, and the secondary engine display is manually or automatically selected. Some important limit markers are replaced by digital indications: • A digital EGT start limit indication (red) replaces the EGT start limit marker. • A digital fuel-on indication (magenta) replaces the fuel-on marker; and X-BLD, if indicated, is replaced by XB. — Page 517 — 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
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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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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
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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
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Page 335 and 336: Navigation Systems Inertial Referen
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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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Page 351 and 352: Power Plant Forward Thrust Levers a
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Page 357 and 358: Power Plant Ignition Control - GE M
Page 359 and 360: Power Plant Ignition Control - RR M
Page 361 and 362: Power Plant Primary EICAS Display -
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Page 365: Power Plant Secondary Engine Displa
Page 369 and 370: Warning Systems EICAS Messages: (co
Page 371 and 372: Warning Systems EICAS Messages: (co
Page 373 and 374: Warning Systems EGPWS: The aircraft
Page 375 and 376: Warning Systems EGPWS - Mode 2: 245
Page 377 and 378: Warning Systems EGPWS - Terrain Cle
Page 379 and 380: Warning Systems EGPWS - Terrain Ale
Page 381 and 382: Warning Systems EGPWS - Aural Messa
Page 385 and 386: Limitations Approved low visibility
Page 387 and 388: Procedures Two Engines Inoperative
Page 389 and 390: Procedures Normal Procedures (Examp
Page 391 and 392: Procedures First Officer - Cockpit
Page 395 and 396: Abnormal Lists Air Systems: — Pag
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OPERATIONS MANUAL

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