OPERATIONS MANUAL

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Simulator Handling Instructor > Preferences > USB: • Through the combo boxes on the right-hand side, assign simulator functions to USB inputs. • When running multiple Precision Simulators on one computer, the USB on checkbox should be deselected on all Precision Simulators but one. Otherwise, every USB input will by multiplied through the network inside this computer and cause input errors. • When running multiple Precision Simulators on different computers, each Precision Simulator may be assigned to any USB functions. However, be sure to assign pilot seat specific functions like the PTT and stabilizer trim switches to the respective onside controls of the captain and first officer. • For each axis and slider, enter a value in the associated Neutral edit field that keeps the input stable when the control is not moved. • The function Aileron and tiller acts as a gear steering tiller when the groundspeed is above 0 and below 40 kt, otherwise it acts as an aileron control wheel. — Page 92 — For preview only. Not for sale. Many pages are intentionally removed.
Simulator Handling Instructor > About/Quit: • The AIRAC cycle currently used in this simulator is indicated after “Navigation data by ...” • The current Java specifications used on this computer are displayed in the white box. — Page 93 — 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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Page 67 and 68: Simulator Handling Instructor > Net
Page 69 and 70: Simulator Handling Network Examples
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Page 91 and 92: Aircraft General Aircraft General
Page 93 and 94: Aircraft General Main Panel Lightin
Page 95 and 96: 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
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
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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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Some pages are intentionally remove
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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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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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