OPERATIONS MANUAL

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FMS LEGS Page: Access: • LEGS key • 6L on RTE DATA General: Provides tools to build and modify route legs for lateral and vertical guidance. Leg line titles (all in small font) Each line title on the left-hand side indicates the respective leg type, for example: 13.9 ARC R Aircraft follows a right-turn DME arc at radius 13.9 nm. 042° Aircraft follows a 042° course of an airway or of any other geographically fixed, lateral path. 044°TRK Aircraft flies a track of 044° (without course correction). 220°HDG Aircraft flies a constant heading of 220° (not a course). ---° Undefined direction. PROC TURN Procedure turn. HOLD AT Holding pattern. A course, heading, or track refers to true north when the indication has a T-suffix, otherwise it refers to magnetic north. In the middle of the page, the line title indicates the computed length of the leg if applicable, or ROUTE DISCONTINUITY if there is a gap. The line title on the right-hand side indicates the glide path (GP) angle if the leg belongs to a final approach; for example, GP 3.00°. Leg lines The left-hand side indicates in large font how a leg will be terminated, for example: PERLY Identifier of a geographically fixed waypoint; the leg terminates when the aircraft flies by or over this waypoint. ( 480) Conditional waypoint; the leg terminates when the aircraft has climbed to 480 ft. (INTC) Conditional waypoint; the leg terminates when the aircraft intercepts the course of the next leg. JFK/03 Conditional waypoint; the leg terminates when the distance between the aircraft and the JFK DME is 3 nm. JFK180 Conditional waypoint; the leg terminates when the aircraft crosses the 180° radial of the JFK VOR. VECTORS The crew has to terminate the leg manually by entering the next or any other waypoint into the first line. (when instructed by ATC). (continued next page) — Page 375 — For preview only. Not for sale. Many pages are intentionally removed.
FMS LEGS Page: (continued) 6L Valid entries in 1R to 5R Step climb advisory on a cruise leg: XXXS FLXXXS Altitude constraint (-1005 to 45100 ft) on a departure or arrival leg: XXXA XXXXB XXXXXAXXXXXB FLXXX Speed constraint (IAS 100 to 399 kt) if altitude constraint is already entered: XXX/ Speed constraint/altitude constraint: XXX/XXX XXX/XXXXA XXX/FLXXX Speed constraints must be combined with altitude constraints.—Mach constraints are invalid. 6L
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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 > 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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Page 207 and 208: Flight Instruments Altitude Indicat
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Page 211 and 212: Flight Instruments ND Symbology: (c
Page 213 and 214: Flight Instruments ND Symbology: (c
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
Page 243 and 244: FMS APPROACH REF Page: 1L 3L 4L 6L
Page 245 and 246: FMS MAINTENANCE INDEX Page: 1L 2L 3
Page 247 and 248: 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
Page 257: FMS ARRIVALS Page (Active Route): (
Page 261 and 262: FMS LEGS Page: (continued) Single l
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
Page 271 and 272: FMS VNAV CLB Page: (continued) 3R 4
Page 273 and 274: FMS VNAV CRZ Page: (continued) 2L 3
Page 275 and 276: FMS VNAV DES Page: Page title 1L 2L
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
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Page 301 and 302: Fuel System Transfer and Jettison P
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
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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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