OPERATIONS MANUAL

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Flight Controls EICAS Messages: CAUTION MESSAGES (accompanied by caution light and beeper sound) FLAPS CONTROL FLAPS DRIVE FLAPS PRIMARY SPEEDBRAKE EXT STAB TRIM UNSCHD alternate flaps control activated OR all RVDTs are unpowered OR all FCUs have failed any flap drive has failed in secondary mode [message inhibited by FLAPS CONTROL] leading edge flap pneumatic drive failure OR trailing edge flap hydraulic drive failure [message inhibited by FLAPS CONTROL or FLAPS DRIVE] speedbrake lever is out of ARM position AND radio altitude is above 15 ft AND { at least two thrust levers are out of idle by 5° or more OR landing flaps are set OR radio altitude is below 800 ft } unscheduled stabilizer trim motion is detected AILERON LOCKOUT >FLAP RELIEF >FLT CONT VLVS RUD RATIO DUAL RUD RATIO SNGL SPEEDBRAKE AUTO >STAB GREENBAND >STAB TRIM () >YAW DAMPER () VALVE CLOSED LIGHT INOP LIGHT ADVISORY MESSAGES aileron lockout disagrees with commanded position flap load relief function has retracted the flaps any flight control shutoff valve is closed upper and lower rudder ratio systems have failed one rudder ratio system has failed autospeedbrake disagrees with commanded position nose gear oleo pressure switch disagrees with FMC selected takeoff trim data hydraulic system (2 or 3) stabilizer drive failure causing the stabilizer trim rate to be reduced by 50% yaw damper (LWR or UPR) failure — Page 269 — For preview only. Not for sale. Many pages are intentionally removed.
Flight Controls EICAS Messages: AILERON LOCKOUT ELEVATOR FEEL FLAP CONTROL () FLAP LOAD RELIEF FLAP SYS MONITOR LE MULT DRIVE LE SINGLE DRIVE MACH/SPEED TRIM RUDDER RATIO RUD TRIM CTR SPEEDBRAKE AUTO STAB AUTO CUTOUT STAB AUTO TRIM STAB GREENBAND STAB SPEED TRIM STAB TRIM STAB TRIM UNSCHD TE FLAPS YAW DAMPER () INOP LIGHT STATUS MESSAGES aileron lockout disagrees with commanded position excessive disagreement between left and right elevator feel system [message inhibited when hydraulic system 2 or 3 pressure is below 1200 psi] FCU (L, C, or R) failure flap load relief function failure FCU failure or sensor fault multiple leading edge flap drives have failed one leading edge flap drive has failed speed trim and Mach trim function has failed [freighter] upper or lower rudder ratio function failure fault detected in rudder trim autocentering control autospeedbrake disagrees with commanded position automatic stabilizer cutout function has failed stabilizer autotrim function has failed nose gear oleo pressure switch disagrees with FMC selected takeoff trim data speed trim function has failed [passenger & combi aircraft] hydraulic system (2 or 3) stabilizer drive failure causing the stabilizer trim rate to be reduced by 50% unscheduled stabilizer trim motion is detected trailing edge flap system failure yaw damper (LWR or UPR) failure — Page 270 — 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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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: Flight Controls Rudder Control: Fla
Page 195 and 196: Flight Instruments Integrated Displ
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Page 199 and 200: Flight Instruments IDU Switching: (
Page 201 and 202: Flight Instruments Instrument Sourc
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Page 207 and 208: Flight Instruments Altitude Indicat
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Page 215 and 216: Flight Instruments ND VOR Mode: In
Page 217 and 218: Flight Instruments ND Plan Mode - V
Page 219 and 220: Flight Instruments ND Position Chec
Page 221 and 222: Flight Instruments ND Test & Failur
Page 223 and 224: Flight Instruments Standby Attitude
Page 225 and 226: Flight Instruments Integrated Stand
Page 227 and 228: Flight Instruments Clock: Chronogra
Page 229 and 230: FMS IRS LEGS Page: 1L 2L 3L 4L 5L 6
Page 231 and 232: FMS ALTN NAV RADIO Page: 1L 2L 3L A
Page 233 and 234: FMS SELECT DESIRED WPT Page: 1L 2L
Page 235 and 236: FMS PROGRESS 2/3 Page: 1L 2L 3L 4L
Page 237 and 238: FMS NAV RADIO Page: 1L 2L 3L 1R 2R
Page 239 and 240: FMS FIX INFO Page: 1L 2L 3L 4L 5L 6
Page 241 and 242: 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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