2RMX IOM - Flight Simulation Company...B737-700 Full Flight Simulator Instructor’s Operating...

18 Jan 2006 TPD XXXXX

B737-700 Full Flight Simulator

Instructor’s Operating Manual

Instructor’s Operating Manual Safety Precautions

Safety Precautions18 Jan 2006

Page i

Safety Precautions

The following general safety notices supplement the specific warnings and cautions appearing elsewhere in this manual. There are recommended precautions that must be understood and applied during operation and maintenance of the equipment covered herein. Should situations arise that are not covered by safety precautions given consult the proper local authority.

(1) Under no circumstances should a person operate or maintain this equipment without theimmediate presence or assistance of another person capable of rendering aid.

(2) Personnel working with or near high voltages must be familiar with modern methods ofresuscitation. In the event of electrical shock, always:

(a) Remove power.

(b) Administer first aid treatment.

(c) Summon assistance.

(3) In the event of fire, carry out the procedures provided in your local fire code.

(4) All operation and maintenance personnel should be familiar with the location andfunction of the emergency shutdown switches. They should also be familiar with theemergency procedures needed to remove power from damaged equipment.

(5) The simulator has voltages that are dangerous and may be fatal if contacted byoperation or maintenance personnel.

(6) Do not energize equipment unless safety grounds have been established; failure to doso may result in electrical shock to the operator.

(7) Do not place a finger over a leak to determine the extent of a leakage. High pressurespray can puncture the skin and enter the bloodstream. High pressure spray ispotentially explosive.

(8) Spilled hydraulic fluid is a safety hazard and must be wiped up immediately.

(9) Before starting the motion system, ensure that the area around the simulator envelope isclear of personnel and that all loose objects are secured.

(10) If, at any time, a safety hazard is detected, it is the responsibility of the individual toreport the hazard to ensure it is corrected.

(11) All personnel in the flight compartment are to be fastened with seat belts.

(12) Do not adjust the seat(s) when the motion system is on.

Instructor’s Operating Manual List of Effective Pages

List of Effective Pages18 Jan 2006

Page iii

List of Effective Pages

Insert the latest changed pages and dispose of the superseded pages in accordance with the applicable amendment instructions and regulations:

NOTE: On a changed page, the text affected by the latest change is indicated by a vertical line in the page margin. Changes to illustrations and tables are indicated by miniature pointing hands or vertical lines.

Page No. Change No.

Title ................................................................0 i to xvii ............................................................0 1-1..................................................................02-1 to 2-3........................................................0 3-1 to 3-3........................................................0 4-1 to 4-5........................................................0 5-1..................................................................06-1 to 6-6........................................................0 7-1 to 7-219....................................................0

Zero in the Change No. column indicates an original page.

Instructor’s Operating Manual Table of Contents

Table of Contents18 Jan 2006

Page v

Table of Contents

Section/Title Page

List of Effective Pages........................................................................................................................iii

Table of Contents ............................................................................................................................... v

List of Illustrations...............................................................................................................................ix

List of Tables ......................................................................................................................................xi

List of Terms and Abbreviations ......................................................................................................xiii

General ............................................................................................................................................1-1 1. Introduction............................................................................................................................1-1

1.1 Reference................................................................................................................1-1 1.2 Main Sections .........................................................................................................1-1

Safety Features ...............................................................................................................................2-1 2. Introduction............................................................................................................................2-1

2.1 Emergency Cutoff Switches ...................................................................................2-1 2.1.1 Motion System Cutoff Switches........................................................................2-1 2.1.2 Electrical Power System Emergency Cutoff ....................................................2-1

2.2 Crew Access ...........................................................................................................2-1 2.2.1 Emergency Operation of Accessway ...............................................................2-1

2.3 Rope Ladder ...........................................................................................................2-2 2.4 Smoke and Heat Detection System .......................................................................2-2 2.5 Emergency Lighting ................................................................................................2-3 2.6 Emergency Power Source......................................................................................2-3 2.7 Fire Suppression System (Optional) ......................................................................2-3

Instructor Station Configuration.......................................................................................................3-1 3. Introduction............................................................................................................................3-1

3.1 Instructor Station Hardware Configuration .............................................................3-2

Full Flight Simulator Instructor’s Operating Manual

Table of Contents 18 Jan 2006 Page vi

Startup and Shutdown.....................................................................................................................4-1 4. Introduction............................................................................................................................4-1

4.1 Daily Site Inspections..............................................................................................4-1 4.2 Startup.....................................................................................................................4-2

4.2.1 Control Loading System Startup ......................................................................4-2 4.2.2 Motion System Startup .....................................................................................4-2 4.2.3 Instructor Operating Station Touch Screen......................................................4-3

4.3 Shutdown ................................................................................................................4-4 4.3.1 Control Loading System Shutdown..................................................................4-4 4.3.2 Motion System Shutdown.................................................................................4-4 4.3.3 Instructor Operating Station Touch Screen......................................................4-6

Flight Readiness..............................................................................................................................5-1 5. Introduction............................................................................................................................5-1

5.1 Preflight Checks......................................................................................................5-1 5.1.1 Panel 1: Emergency Shutdown.......................................................................5-1 5.1.2 Panel 2: Communications Facility ...................................................................5-1 5.1.3 Panel 3: Lighting Control .................................................................................5-1 5.1.4 Panel 4: Accessway Control............................................................................5-1 5.1.5 Panel 5: Temperature Control .........................................................................5-1

5.2 Postflight Checks ....................................................................................................5-1 5.2.1 Reset.................................................................................................................5-1 5.2.2 Motion and Control Loading .............................................................................5-1

Instructor Station Panel Description................................................................................................6-1 6. Introduction............................................................................................................................6-1

6.1 Panel 1: Emergency Shutdown .............................................................................6-1 6.2 Panel 2: Communications Facility .........................................................................6-3 6.3 Panel 3: Lighting Control .......................................................................................6-4 6.4 Panel 4: Accessway Control..................................................................................6-5 6.5 Panel 5: Temperature Control ...............................................................................6-6

LCD Page System...........................................................................................................................7-1 7 Introduction.............................................................................................................................7-1

7.1 LCD Page Input/Output Types ...............................................................................7-2 7.2 LCD Pages Color Logic ..........................................................................................7-3

7.2.1 Regular and Lesson Page Color Logic ............................................................7-3 7.2.2 Malfunction Pages Color Logic.........................................................................7-3 7.2.3 Map Color Logic................................................................................................7-4 7.2.4 Approach Plots Color Logic ..............................................................................7-4 7.2.5 Runway Plots Color Logic ................................................................................7-4

7.3 Map Symbology ......................................................................................................7-5

Instructor’s Operating Manual Table of Contents

Table of Contents18 Jan 2006

Page vii

7.4 LCD Pages..............................................................................................................7-6 7.5 Footer Pages ..........................................................................................................7-7

7.5.1 Footer No. 1 ......................................................................................................7-7 7.5.2 Recall Last Capture ........................................................................................7-10 7.5.3 Footer No. 2 ....................................................................................................7-11

7.6 Index Pages ..........................................................................................................7-14 7.6.1 Master Index ...................................................................................................7-14 7.6.2 Malfunction Index............................................................................................7-17 7.6.3 Lesson Plan Index ..........................................................................................7-18

7.7 Control Pages .......................................................................................................7-20 7.7.1 Aircraft Set (737-800) .....................................................................................7-20 7.7.2 Doors (737-800)..............................................................................................7-24 7.7.3 Fuel Set...........................................................................................................7-26 7.7.4 A/C Config Quick Set (Metric & Imperial) - (737-800)....................................7-28 7.7.5 Position Set.....................................................................................................7-30 7.7.6 Runways .........................................................................................................7-38 7.7.7 Destination Airport ..........................................................................................7-39 7.7.8 Destination Runways......................................................................................7-41 7.7.9 ALT/IAS/HDG Set ...........................................................................................7-42 7.7.10 Position Slew ............................................................................................7-44 7.7.11 Hold/Taxi...................................................................................................7-46 7.7.12 Airport Repos/Lighting ..............................................................................7-48 7.7.13 Environment Set .......................................................................................7-49 7.7.14 Time of Day ..............................................................................................7-58 7.7.15 Airport Lighting..........................................................................................7-60 7.7.16 Runway Lights ..........................................................................................7-63 7.7.17 TCAS ........................................................................................................7-64 7.7.18 Ground Traffic...........................................................................................7-68 7.7.19 Surface Wind ............................................................................................7-70 7.7.20 Runway Conditions...................................................................................7-73 7.7.21 Weather Effects ........................................................................................7-76 7.7.22 Microburst .................................................................................................7-78 7.7.23 Microburst Description..............................................................................7-80 7.7.24 Predictive Windshear................................................................................7-81 7.7.25 Non-Predictive Windshears......................................................................7-85 7.7.26 Turbulence................................................................................................7-88 7.7.27 Icing...........................................................................................................7-90 7.7.28 Simulator Controls ....................................................................................7-92 7.7.29 Resets/Freezes.........................................................................................7-95 7.7.30 Aircraft Upset ..........................................................................................7-104 7.7.31 Communications.....................................................................................7-105 7.7.32 FMS Memory Save/Recall......................................................................7-109 7.7.33 Title Designation: Save...........................................................................7-111 7.7.34 Recall ......................................................................................................7-112 7.7.35 Delete Selected Item ..............................................................................7-113 7.7.36 Clear All Temporary................................................................................7-114 7.7.37 Fail Summary..........................................................................................7-115


Table of Contents 18 Jan 2006 Page viii

7.7.38 Controls Not In Agreement (CNIA).........................................................7-118 7.7.39 Crash Status ...........................................................................................7-120 7.7.40 Radio Station Index ................................................................................7-122 7.7.41 Failed Stations ........................................................................................7-124 7.7.42 ATIS ........................................................................................................7-126 7.7.43 ATIS - Weather Type..............................................................................7-130 7.7.44 ATIS - Clouds .........................................................................................7-131 7.7.45 Approach.................................................................................................7-133 7.7.46 Arrival Runway........................................................................................7-134 7.7.47 ATIS - Departure Runway ......................................................................7-135 7.7.48 ATIS - Runway Conditions .....................................................................7-136 7.7.49 ATIS - Braking Action .............................................................................7-138 7.7.50 Remarks TBD .........................................................................................7-139 7.7.51 ATC Message Pages..............................................................................7-140 7.7.52 Air Carriers..............................................................................................7-148 7.7.53 Hand-Off Controller ................................................................................7-149 7.7.54 Destination Type.....................................................................................7-150

7.8 Map Pages..........................................................................................................7-151 7.8.1 Map Status....................................................................................................7-153 7.8.2 Scale .............................................................................................................7-156 7.8.3 Map To Airport ..............................................................................................7-157 7.8.4 Symbol Suppress..........................................................................................7-159 7.8.5 Station Fail ....................................................................................................7-160 7.8.6 Storm Clouds ................................................................................................7-163 7.8.7 Approach Plot Pages....................................................................................7-172 7.8.8 Non-Precision Approach Plot .......................................................................7-173 7.8.9 ILS Approach Plot.........................................................................................7-174 7.8.10 Runway Plot............................................................................................7-176 7.8.11 Tail Clearance.........................................................................................7-177

7.9 Malfunction Pages ..............................................................................................7-178 7.9.1 Typical Malfunction Page .............................................................................7-178 7.9.2 Preselect .......................................................................................................7-179 7.9.3 Preselect Criteria ..........................................................................................7-182

7.10 Lesson Plan Pages.............................................................................................7-185 7.10.1 Sample Lesson Plan...............................................................................7-187

7.11 Maintenance Pages ............................................................................................7-189 7.11.1 Initial Conditions and FMC Performance ...............................................7-189 7.11.2 Engine Fails ............................................................................................7-190 7.11.3 ATM Reposition ......................................................................................7-191 7.11.4 Flight Situation Capture/Recall...............................................................7-200 7.11.5 Flight Situation Transfer .........................................................................7-203 7.11.6 Delete All Captures.................................................................................7-205 7.11.7 Flight Situation – Capture Recall Details................................................7-206 7.11.8 Flight Situation –Stored Recall Details...................................................7-208

7.12 Help Pages..........................................................................................................7-210

Instructor’s Operating Manual List of Illustrations

List of Illustrations18 Jan 2006

Page ix

List of Illustrations

Figure/Title Page

Figure 3-1 Forward Facing IOS ..............................................................................................3-3

Figure 6-1 Emergency Shutdown Panel .................................................................................6-1 Figure 6-2 Communications Facility Panel .............................................................................6-3 Figure 6-3 Lighting Control Panel ...........................................................................................6-4 Figure 6-4 Accessway Control Panel......................................................................................6-5 Figure 6-5 Temperature Control Panel ...................................................................................6-6

Figure 7-1 LCD Layout............................................................................................................7-1 Figure 7-2 Numeric Keypad and Slider...............................................................................7-211 Figure 7-3 Alphanumeric Keypad .......................................................................................7-211 Figure 7-4 Typical Malfunction Selection Pop-Up Menu.....................................................7-215

Instructor’s Operating Manual List of Tables

List of Tables18 Jan 2006

Page xi

List of Tables

Table/Title Page

Table 4-1 Control Loading System Startup Procedure ...........................................................4-2 Table 4-2 Motion System in Normal Mode Startup Procedure (IOS)......................................4-3 Table 4-3 Control Loading System Shutdown Procedure (IOS) .............................................4-4 Table 4-4 Motion System Shutdown Procedure (IOS)............................................................4-6

Table 7-1 Map Symbology ......................................................................................................7-5

Instructor’s Operating Manual List of Terms and Abbreviations

List of Terms and Abbreviations18 Jan 2006

Page xiii

List of Terms and Abbreviations

ac alternating currentACARS Aircraft Communications Addressing and Reporting System ACIP ac InputACOP ac OutputADC Analog-to-Digital ConverterADF Automatic Direction Finder ADIO Analog/Digital Input/OutputAI Analog InputsAIM Acknowledgment, ISO Alphabet no. 5 and Maintenance AIO Analog Input/OutputAIOI ARINC 429 input/output interface AIP Analog InputAIRO Analog Input Reference Output AGL Above Ground Level AM Amplitude Modulatedamp AmpereAOM Analog Output Module AOP Analog OutputASCII American Standard Code for Information Exchange ASL Above Sea LevelATC Air Traffic Control ATIS Automated Terminal Information Service ATO Address Time-OutA/W Accessway

BCD Binary Coded Decimal BFO Beat Frequency Oscillator BI Bus IdentificationBPS beats per second BU Buffer UnitB/W Black and White

CAL Instrument Calibration UtilityCAPT Computer Assisted Procedures Trainer CB Circuit BreakerCCD Charge Coupled Device CCU C-Bus Check UtilityCDB Common DatabaseCMS Central Monitoring SystemCO2 Carbon DioxideComp. ComputersCorp. CorporationCPU Central Processing UnitCRA Coefficient RAM Address


List of Terms and Abbreviations 18 Jan 2006 Page xiv

CRT Cathode Ray Tube CS Card SelectCSMA/CD Carrier Sense Multiple Access with Collision Detection CSS Cockpit Simulator System CTS Computerized Test System CVR Cockpit Voice Recorder CWE CAELIB Working Environment

DAC Digital-to-Analog ConverterDACW DAC WriteDASIU Digital Audio System Interface Unit DAST Direct Analog Storage Technology dc direct currentDCB Data Control Block DCR Data Control Register DFC Digital Flight Controls DIN Deutsche Industrie Normen DIO Digital Input/OutputDIO-CB Digital Input/Output Circuit Breaker DIP Digital InputDMC Datapath® C Microprocessor Controller DMM Digital Multi-MeterDN1 Digital Control Cabinet DOP Digital OutputDOP Discrete OutputDOR Digital Output Relay DPA Dual Power AmplifierDRA Data RAM Address DSG Digital Signal Generator DSP Digital Signal Processor DTO Data Time-OutDV Digital VoiceDVM Digital Voltmeter

EFCS Electronic Flight Control System EICAS Engine Instrument and Crew Alert System EL ElectroluminescentElec. ElectronicsEMI Electromagnetic InterferenceEPO Emergency Power OffESU Electronic Service Unit

F/C Flight CompartmentFC Flight CompartmentFDCC Fiber-Optic Digital Chassis Controller FDDI Fiber-Optic Distributed Digital Interface



Page xv

FFIOS Forward-Facing Instructor Operating System FFS Full Flight Simulator FIFO First-In, First-OutFIR Finite Impulse Response FIRCTL FIR ControlFMAST Flight Management and System Trainer FMC Flight Management Computer FOV Field of View FP Feature ProcessorFPMC Floating Point Motion Controller FSK Frequency Shift Keying FTD Flight Training Device FWS Flight Warning System

GAL Generic Array Logic GB Giga ByteGBYTE Giga ByteGPWS Ground Proximity Warning System

HPS Hydraulic Power Supply HP Hewlett PackardHPU Hydraulic Power Unit HS High SpeedHz Hertz

I/O Input/OutputIATA International Air Transport Association IC Integrated CircuitID Identification IDS Integrated Diagnostic System IGW Increased Gross Weight Int’l InternationalIOS Instructor Operating System IP Internet ProtocolIPE Integral Position Equipment

KYBD Keyboard

LAHSO Land and Hold Short Operations LAN Local Area NetworkLCD Liquid Crystal Display LED Light Emitting Diode LRU Line Replaceable Unit LSB Least Significant Bit LVOS Light-to-Voltage Optical Sensor


List of Terms and Abbreviations 18 Jan 2006 Page xvi

MA Mechanical AssemblyMAC MAXVUE™ Autocal Controller MAIB MAXVUE™ Autocal Integrated Board MCL Motion and Control Loading MCU Master Control Unit Misc. MiscellaneousMMU Memory Management UnitMOB Multiple Output Board MOS Metal-Oxide Semi-conductorMSB Most Significant Bit MSV Main Switch-VisualMTFAA Motion Test FAA MTP Motion Test Program

NMI Non-Maskable Interrupt

OEM Original Equipment Manufacturer OSI Open System Interconnection

PA Public AddressPAL Programmable Array Logic PC Programmable ControllerPC Personal ComputerPCB Printed Circuit Board PDM Pulse Duration Modulation PE Position ErrorPHU Projector Head Unit PIC Programmable Interrupt Controller PIT Programmable Interval Timer PP2 Pixel Processor type 2 PROM Programmable Read Only Memory PSC Parallel-to-Serial ConverterPSCD Procurement Specification Control Drawing PTT Press-to-Talk

QTG Qualification Test Guide

RACU Remote Alignment and Control Unit RAM Rapid Access Maintenance RCP Radio Control Panel RFT Ready for Training RPM Rotations per minute RTD Resistance Temperature Detector



Page xvii

SAH Sample and Hold SC-bus Super Chassis Bus SOP Synchro OutputSpec. Specification

TCAS Traffic Alert and Collision Avoidance System TCP Transmission Control Protocol temp. TemperatureTOP Torquer OutputTPD Technical Publications DepartmentTSD Time-Shared Data

UPS Uninterruptible Power Supply

V VoltsVac Volts of alternating current VAE Voice Alteration Effect VCP Video Cassette Player VCR Video Cassette Recorder Vdc Volts of direct current VESDA® Very Early Smoke Detection Apparatus VHF Very High Frequency VHS Very High Speed VOR VHF Omni-RangeVP Vocal PlayerVPC Video Player Card

Instructor’s Operating Manual General

General18 Jan 2006

Page 1-1

General

1. Introduction

The Instructor’s Operating Manual is one manual in a set of CAE-supplied hardware documentation that supports the operation and maintenance of the Boeing 737-700 Full Flight Simulator.

1.1 Reference

The following reference documents for the Boeing 737-700 Full Flight Simulator apply herein:

(1) Technical Specification

(2) Addendum 2 - LCD Pages

(3) Addendum 3 - Instructor Station

(4) Addendum 4 - Instructor Controls

(5) Maintenance Operating Manual (MOM).

1.2 Main Sections

(1) Part 1 is a general introduction.

(2) Part 2 outlines the safety features.

(3) Part 3 outlines the instructor station configuration.

(4) Part 4 describes the startup and shutdown procedures.

(5) Part 5 describes the flight readiness checks.

(6) Part 6 describes the individual instructor station panels.

(7) Part 7 describes the LCD page system.

NOTE: All LCD pages included in this IOM are snapshots of LCD pages at Ready for Training (RFT).

Instructor’s Operating Manual Safety Features

Safety Features18 Jan 2006

Page 2-1

Safety Features

2. Introduction

The instructor station and surrounding areas are provided with the following safety equipment and systems.

2.1 Emergency Cutoff Switches

2.1.1 Motion System Cutoff Switches The motion system can be de-pressurized in less than 30 seconds when it is shutdown either by switching off the motion system (normal operation) or by selecting one of the hydraulic cutoff switches in the off position. These switches are guarded and located at the instructor console, in the maintenance areas and in the forward simulated area. The switch(es) in the simulated area blend with the appearance of the cockpit and are accessible to the flight crew. Operation of any of the switches cuts power from all hydraulic pumps, causes the motion system to make an orderly transition to the rest position, and deactivates the flight controls.

2.1.2 Electrical Power System Emergency Cutoff

An electrical power emergency cutoff system is provided. Emergency cutoff switches are easily accessible and located at the IOS and P1 cabinet. Activation of any EPO switch shall deactivate the main power input.

2.2 Crew Access

When the simulator flight compartment comes to the rest position, the accessway automatically swings into position against the exit platform at the rear of the flight compartment.

2.2.1 Emergency Operation of Accessway

In the event of a complete power failure, the motion platform automatically retracts to the rest position and the accessway lowers. The accessway is driven up and down by means of a dc motor. Power for the dc motor is supplied from an emergency power source. As an alternative, it is possible to unlatch the drive mechanism and manually lower the accessway. If any of the emergency cutoff switches are operated, the power to the drive mechanism of the accessway is maintained and is operable from a switch located at the flight compartment exit.


Safety Features 18 Jan 2006 Page 2-2

2.3 Rope Ladder

If the accessway does not function properly, a rope escape ladder is provided for exiting the simulator. The rope escape ladder is located under the floor at the rear of the simulator.

To use the rope escape ladder, open the access door and unroll the escape ladder over the middle railing rung or lower panel on the back of the flight compartment.

NOTE: If there is no immediate danger, wait for the maintenance crew to provide a solid ladder before using the rope ladder.

2.4 Smoke and Heat Detection System

A Very Early Smoke Detection Apparatus (VESDA®) system detects invisible molecules generated during the precombustion stages of an incipient fire. This system continuously samples air from the equipment environment through a high efficiency aspirator. The detection unit signal is then processed and, depending on the smoke level, can be programmed to indicate:

(1) Alert: to investigate detection of something out of the ordinary

(2) Action: to initiate emergency procedures for a potential fire

(3) Fire: actual fire condition.

Air sampled through pipes installed inside the CAE interface cabinets and simulator flight compartment is routed via tubing to the VESDA® system detector where the air sample is analyzed. The self-contained VESDA® unit is installed in the computer room.

Automatic deactivation of simulator power by the power control cabinet (P1), audible warning, and indication of the effected zone on power control cabinet monitor screen as well as on the detector control unit are provided. The VESDA® detection system is equipped with a component failure detection and self-test capability. Alarm and other monitor signals are available for connection to the building fire detection control panel from the P1 cabinet.

The system operates via a purchaser-supplied facility power source independent from normal simulator power.

The HPS is monitored using a conventional smoke detector system.

Instructor’s Operating Manual Safety Features

Safety Features18 Jan 2006

Page 2-3

2.5 Emergency Lighting

Emergency lighting is provided in the flight compartment and at the entry platform. The lighting is powered from the emergency power source and switches on automatically in the event of a complete loss of building power when the simulator is in operation.

2.6 Emergency Power Source

All emergency operations described are powered from a standby CAE-supplied line-rechargeable battery power pack. The pack automatically recharges when normal power is available.

2.7 Fire Suppression System (Optional)

The fire suppression systems consist of a CO2 fire extinguisher in the instructor's area and an automatic suppression system using a chemical agent. This automatic fire suppression system is often comprised of a control panel, alarm devices and cylinders for chemical agent. For more information, refer to 115-9 (Safety) of the Maintenance Manual.

Instructor’s Operating Manual Instructor Station Configuration

Instructor Station Configuration18 Jan 2006

Page 3-1

Instructor Station Configuration

3. Introduction

A typical CAE forward-facing IOS station is designed to assist the instructor in monitoring all aspects of crew performance in the simulator (see Figure 3-1). Two touch-sensitive color Liquid Crystal Displays (LCDs) are mounted on the Instructor Seat’s workstation which allow the instructor to move his seat forward behind the crew and easily monitor crew performance. The station incorporates the design features necessary to tailor it to the operational needs of the user. The state-of-the-art hardware and software are utilized to make the station a powerful and user friendly human-computer interface. A facility is provided at the sidewall to store books and to house various controls that are not continually required by the instructor. The basic components of the station include:

(1) Two 17" Touch-Sensitive High-resolution Color LCDs. The LCDs use a flexible systemof high-resolution graphics, icons, scrolling, graphic slew/slider controls, contextsensitive popup menus and windowing techniques to simplify and optimize the IOSpages, providing the user with an easy-to-use environment. The flight deck respondswithin a second of instructor input.

To allow the instructor to structure a training exercise before commencing the simulatorsession, a powerful lesson plan editor is provided. With lesson plans, the entire simulatorcontrols and monitor functions may be preprogrammed and automatically executed underinstructor control during the training session.

(2) Seats.

(a) Instructor Seat. The instructor seat is positioned to optimize the instructor’s view oftrainee actions. Equipped with armrests and a lap belt, the instructor seat hasadjustments such as height and position along the track which provide comfort andsafety while the instructor remains seated.

(b) Observer Seat. The observer seat is a non-aircraft seat equipped with armrestsand a lap belt. It is mounted on a track to allow fore and aft movement, and iscapable of height adjustment. The observer seat is mechanically controlled.

(c) Second Observer Seat. The second observer seat is a non-aircraft type seat. Theseat is a non-adjustable folding jumpseat and is maintained in a fixed position atthe rear of the flight compartment.


Instructor Station Configuration 18 Jan 2006 Page 3-2

3.1 Instructor Station Hardware Configuration

The instructor station (see Figure 3-1) consists of the following:

• Simulator controls for emergency motion and control loading stop; emergencypower off

• Communications facility – audio jack panel mounted at the back of the instructorseat and a Press-To-Talk (PTT) switch provided on the station

• Lighting controls for the flight compartment and a reading light for the IOS station

• Service Outlet panel

• Accessway control

• Temperature control.

The panels on the instructor station are described in section 6.

Instructor’s Operating Manual Instructor Station Configuration

Instructor Station Configuration18 Jan 2006

Page 3-3

Figure 3-1 Forward Facing IOS

Instructor’s Operating Manual Startup and Shutdown

Startup and Shutdown18 Jan 2006

Page 4-1

Startup and Shutdown 4. Introduction

The following section includes a startup and shutdown checklist for the motion and control loading on the IOS. For a more detailed description of the safety precautions, and startup and shutdown procedures, refer to the Maintenance Operating Manual.

4.1 Daily Site Inspections

Before prestart, tour the simulator site and check the following:

(1) On the projector maintenance deck atop the flight compartment, if equipped witha hinged rear railing, ensure that that it is in the “flight” position. The railing is inthe flight position when it is canted forward, and should be secured in thisposition using the quick-release pins located near its pivot points. While on theprojector maintenance deck, check to ensure that no maintenance equipmenthas been left behind.

(2) In the mirror cavity, ensure that no maintenance equipment has been left behindand that no service personnel are inside.

(3) Ensure that all doors, covers and hatches on the flight compartment are securedin the closed position.

(4) Ensure that the doors on all cabinets are closed.

(5) Ensure that all personnel and maintenance equipment (ladders, scaffolding,forklifts, etc.) are outside the motion envelope of the simulator.

(6) Check the status of the following battery backup and UPS systems.


Startup and Shutdown 18 Jan 2006 Page 4-2

4.2 Startup

4.2.1 Control Loading System Startup

WARNING: BEFORE STARTING THIS PROCEDURE AND WHILE THE SYSTEM IS IN OPERATION, THE TECHNICIAN MUST ENSURE THAT THE CREW IS CLEAR OF THE FLIGHT CONTROLS.

Table 4-1 lists the steps to startup the control loading system in the NORMAL mode. This procedure will start up the flight controls (control loading) from the IOS.

NOTE: During these procedures, various warnings or failures may be annunciated; they must be cleared before the procedure is continued.

Table 4-1 Control Loading System Startup Procedure Step Location Check(s)/Action(s) Expected

Input(s)/Output(s)

1 IOS In the footer of the IOS page, perform the following:

2 IOS Check C/L button. Reads READY.

3 IOS Press C/L button. Starts flashing while indicating STARTING; changes to ON and remains illuminated.

4.2.2 Motion System Startup

The following paragraphs describe the procedures to start up the motion system in normal mode (see Table 4-2). In normal mode the motion system can be engaged only from the IOS control panel.

NOTE: Prior to engaging the motion system, the hydraulic power supply must be operational and control loading must be ON. The M4 cabinet must be on with the simulator loaded and running.

WARNING: BEFORE STARTING THIS PROCEDURE AND WHILE THE SYSTEM IS IN OPERATION, THE TECHNICIAN MUST ENSURE THAT:

(1) ALL PERSONNEL ARE CLEAR OF THE MOTION BASE.

(2) ANY LOOSE EQUIPMENT IS REMOVED OR SAFELYSTOWED.



Page 4-3

(3) ALL PERSONNEL IN THE FLIGHT COMPARTMENT ARETO BE FASTENED WITH SEAT BELTS.

(4) THE ACCESSWAY GATE, FC DOOR AND ALL BAYDOORS ARE CLOSED.

Table 4-2 Motion System in Normal Mode Startup Procedure (IOS) Step Location Check(s)/Action(s) Expected

Input(s)/Output(s)

1 IOS On the IOS SIMULATOR CONTROLS page perform the following:

2 IOS Check MOTION button. Reads READY

3 IOS Press MOTION button.. Starts flashing while indicating STARTING; changes to ON and remains illuminated.

NOTE: Cooling pump motor must be ON.

Another person will observe the following actions outside the simulator.

4 Audible alarm. Sounds until the motion system rises to the neutral position

5 Drawbridge warning light (located near the drawbridge entrance.

Flashes red

6 Motion warning lights (located under the motion platform).

Flashes red

7 Accessway. Accessway is raised and system is pressurized.

8 Motion platform. Rises to the neutral position (mid travel)

4.2.3 Instructor Operating Station Touch Screen

To turn on the IOS touch screen, locate and turn on the power switch. Power indicator should illuminate.



4.3 Shutdown

4.3.1 Control Loading System Shutdown

Table 4-3 lists the steps to turn off the control loading system from the IOS in the flight compartment.

NOTE: During this procedure, various warnings or failures may be annunciated; they must be cleared before the procedure is continued.

Table 4-3 Control Loading System Shutdown Procedure (IOS) Step Location Check(s)/Action(s) Expected

Input(s)/Output(s)

1 IOS On the IOS SIMULATOR CONTROLS page perform the following:

2 IOS Press FLIGHT CONTROLS (CONTROL LOADING) button.

Indicates STOPPING then changes to READY.

4.3.2 Motion System Shutdown



Page 4-5

Table 4-4 lists the steps to shut down the motion system from the instructor operating station.

NOTE: During this procedure, various warnings or failures may be annunciated; they must be cleared before the procedure is continued.



Table 4-4 Motion System Shutdown Procedure (IOS) Step Location Check(s)/Action(s) Expected

Input(s)/Output(s)

1 IOS On the IOS SIMULATOR CONTROLS page, perform the following:

2 IOS Press MOTION button. Audible alarm sounds. 3 IOS Check Motion button Starts flashing while

indicating STOPPING and then changes to READY and remains illuminated.

Another person will observe the following actions outside the simulator.

4 Accessway warning light Flashes red.

5 Motion warning lights. Flash red.

6 Motion platform Lowers to rest position.

7 Accessway Once the motion pressure is below 600 psi (4137 kPa) the accessway will lower and the motion warning lights will stop flashing.

4.3.3 Instructor Operating Station Touch Screen

Turn off the IOS touch screen power switch. Power indicator should extinguish.

Instructor’s Operating Manual Flight Readiness

Flight Readiness18 Jan 2006

Page 5-1

Flight Readiness

5. Introduction

Before starting a training session, ensure that the instructor station is in a preflight condition, i.e., ready to be activated. Scan the station and refer to the following paragraphs to determineits readiness.

5.1 Preflight Checks

5.1.1 Panel 1: Emergency Shutdown

No preflight check is necessary.

5.1.2 Panel 2: Communications Facility

Set up the panel as required for the training session.

5.1.3 Panel 3: Lighting Control

Adjust the two control knobs to the desired lighting intensity and push the CEILING LIGHTS button to turn the ceiling lights on.

5.1.4 Panel 4: Accessway Control

No preflight check is necessary.

5.1.5 Panel 5: Temperature Control

Ensure that the desired temperature is displayed. If not, set accordingly (refer to Section 6 for instructions on how to set the controls).

5.2 Postflight Checks

At the end of a training session, it is desirable to return the simulator to normal conditions. To achieve this, perform the following functions:

5.2.1 Reset To return the simulator to normal conditions select TOTAL RESET from the Resets/Freezes page.

5.2.2 Motion and Control Loading

Refer to Section 4 for a description of the Motion and Control Loading shutdown procedures.

Instructor’s Operating Manual Instructor Station Panel Description

Instructor Station Panel Description

18 Jan 2006Page 6-1


6. Introduction

This section provides a description of the individual panels located on the instructor station.

6.1 Panel 1: Emergency Shutdown

This panel provides the facility to shut down the motion and control loading systems in the event of an emergency. The emergency control panel consists of two switches as shown in Figure 6-1.

Figure 6-1 Emergency Shutdown Panel

Item Description

MOTION & C/L OFF Pressing the MOTION & C/L OFF button cuts off hydraulics to the motion loading system. The motion system returns to its rest position in a controlled manner, and the crew access platform lowers automatically.


Instructor Station Panel Description 18 Jan 2006 Page 6-2

Item Description

POWER OFF Pressing the POWER OFF button cuts off electrical power to the P1 cabinet, shutting off the motion and control loading systems. The motion system returns to its rest position in a controlled manner and the crew access platform lowers automatically.

NOTE: EMER MOTION & C/L OFF buttons are also located in the forward flight compartment area and are accessible to both crew members. An EMER MOTION & C/L OFF button is also located on the instructor seat.



18 Jan 2006Page 6-3

6.2 Panel 2: Communications Facility

This panel allows the instructor to communicate with the crew over aircraft communication systems. The instructor controls the functions of the communications facility via the appropriate selections on the IOS page.

The panel on the back instructor seat contains three jacking facilities labeled as shown in Figure 6-2. There is also a Press-To-Talk (PTT) switch available on the instructor seat.

Figure 6-2 Communications Facility Panel

Item Description

HEADSET The headphone jack enables reception at the instructor station.

HANDMIC This microphone jack allows transmission to the flight crew.

BOOMSET The boomset jack enables reception and transmission with the flight crew.



6.3 Panel 3: Lighting Control

This switch on the Pilot side Miscellaneous Panel allows the instructor to control the ceiling lights. The Lighting Control panel consists of a switch labeled CEILING LIGHT as shown in Figure 6-3.

Figure 6-3 Lighting Control Panel

Item Description

CEILING LIGHT This button turns the ceiling lights on and off.



18 Jan 2006Page 6-5

6.4 Panel 4: Accessway Control

The Accessway Control Panel is located on the Pilot side Miscellaneous Panel and allows the instructor to control the crew accessway. The panel consists of three push buttons and is labeled ACCESSWAY as shown in Figure 6-4.

Figure 6-4 Accessway Control Panel

Item Description

UP To lift up (remove) the accessway.

DOWN To lower down the accessway.

STOP To stop the action in case of emergency.



6.5 Panel 5: Temperature Control

This panel allows the instructor to display the present temperature, the set temperature or an alarm value, and to set a temperature or an alarm value. The panel contains an LED display and three control keys as shown in Figure 6-5. A hidden key provides for protection from unauthorized users.

Figure 6-5 Temperature Control Panel

Item Description

LED Display The LED display displays the present temperature, set temperature or alarm value (usually not used) depending on the main display value chosen using the return key. The up and down deviation indicators to the left of the main display illuminate if the present temperature is higher or lower than the set temperature. The square indicator appears in green if the deviation is within 1% of the full scale.

SP SP appears beside the main display when set temperature is displayed.

ON The control output indicator illuminates while the control output is being produced.

Return Key The return key changes the value displayed on the main display from present temperature to set temperature to alarm value.

Instructor’s Operating Manual LCD Page System

LCD Page System18 Jan 2006

Page 7-1

LCD Page System

7. Introduction

The instructor is provided with two physically identical LCDs at the instructor station. Each LCD has a 14-inch wide by 10-inch high viewing area.

Figure 7-1 illustrates the LCD layout.

Figure 7-1 LCD Layout

The LCDs are used to display the following:

(1) LCD pages and footers consisting of graphics text and numerical data.

(2) Graphics consisting of navigation station symbology, aircraft track, glide slope andlocalizer deviations, and runway plotting which usually appear on the second LCD. Afooter and header appear with graphic pages.

(3) Graphic recorder data consisting of plots of up to 16 variables at a time which usuallyappear on the upper LCD.


LCD Page System 18 Jan 2006 Page 7-2

LCD pages are lists of information grouped logically by function or system, each uniquely identified by a number in the range of 1 to 2500. Each LCD page is a collection of items. Typically, an item is composed of a comment field and a volatile field. The comment field describes the parameter or function and does not change (although it may change color), and the volatile field displays the parameter value or state and follows changes in the value or state.

In addition to displaying information, the instructor can change information on an LCD page. Items whose state or value the instructor can change have a box or touch area around them. Items are selected by touching the area within the box.

LCD pages can be selected from:

(1) Index pages

(2) Menu from the footer area

(3) Lesson plans.

7.1 LCD Page Input/Output Types

Variables on an LCD page are displayed using different formats depending on the type of the variable. The types of variables that may be found on an LCD page are described as follows:

(1) DECIMAL: A decimal type function displays and accepts input in a decimalformat. This includes the latitude/longitude, angle, time, and alphanumericformats.

(2) BOOLEAN. A Boolean type function has two states: on and off.

(3) SET VALUE: A set value type function sets a predetermined value for up to 60decimal or Boolean type variables when selected. A set value may also be pre-programmed to activate when certain criteria are met.

(4) MULTIPLE: A multiple type function is a single display, which may display up to10 decimal functions.

(5) BAR CHART/BAR SCROLL: Decimal values also may be displayed and acceptinput in the form of a bar chart/bar scroll graphic representation.

(6) POPUP MENU: A popup menu function displays a window that containsadditional controls relating to the selection made.



Page 7-3

7.2 LCD Pages Color Logic

The LCD pages can use the following eight colors: red, green, blue, cyan, magenta, white, yellow and black. The LCD page color logic is described in the following paragraphs.

7.2.1 Regular and Lesson Page Color Logic

The color logic for regular text pages and scenario pages is as follows:

(1) GREEN: The fill color of boxes around discrete functions which areactive (on), and the lesson plan text for steps already actioned is green.

(2) RED: The fill color of boxes around freeze functions which are active (on)is red.

(3) LIGHT GRAY: The fill color of boxes around freeze functions which areinactive (off) is light gray.

(4) BLACK: This is the normal color for text displayed within the touchboxes.

(5) WHITE: This is the normal color for text displayed on the LCD page andin the header and footer areas. The lesson plan text for steps yet to beactioned is white.

(6) YELLOW: The lesson step of interest in an active lesson plan is yellow.The fill color of a decimal item on input is yellow.

(7) CYAN: The fill color of an item on input (when touched) is cyan.

7.2.2 Malfunction Pages Color Logic

The color logic for malfunction pages is as follows:

(1) RED: The fill color of the box around an active malfunction is red.

(2) LIGHT GRAY: The fill color of the box around an inactive malfunction islight gray.

(3) WHITE: Text on malfunction pages is white.

(4) MAGENTA: Preselected malfunction information text is magenta.



7.2.3 Map Color Logic

The color logic for map pages is as follows:

(1) GREEN: The default color for all information and the spiderweb is green.

(2) RED: Killed stations (including idents) are red.

(3) YELLOW: Tuned stations (including idents) are yellow.

NOTE: Killed status overrides tuned status for display purposes.

(4) WHITE: The aircraft symbol and aircraft track and trail, including thespiderweb, are white. Radio station idents have the same color as thestation symbol. Station frequency displays are white.

7.2.4 Approach Plots Color Logic

The approach plot color logic is as follows:

(1) GREEN: The default color for all information and the plot grids are green.

(2) WHITE: The localizer deviation, glide slope deviation, target speed, andthe non-precision plots are white.

(3) RED: The localizer deviation plot is red when ±2 dots deviation isexceeded or the grid limits are reached. The glide slope deviation plot isred when ±1 dot deviation is exceeded or the limits are reached. Thespeed deviation plot is red when the grid limits are reached. Thetouchdown marker and the runway length vector are also red.

7.2.5 Runway Plots Color Logic

The runway plot color logic is as follows:

(1) GREEN: The default color for all information is green. The plot grids aregreen.

(2) WHITE: The aircraft symbol is white. The aircraft track is white when theaircraft is on the ground,

(3) CYAN: The aircraft track is cyan when the aircraft is in the air.



Page 7-5

7.3 Map Symbology

Table 7-1 Map Symbology

Symbol Type Symbol Color

Aircraft white

ILS green

VOR green

VORTAC green

TACAN green

Marker green

NDB green

Spiderweb green

Cloud cell*

red green yellow

Flight Capture green

Runway green



7.4 LCD Pages

LCD pages are divided into the following groups and are described on the following pages:

(1) Footer pages

(2) Index pages

(3) Control pages

(4) Map pages

(5) Malfunction pages

(6) Lesson Plan pages

(7) Maintenance pages

(8) Help pages.

NOTE: All LCD pages included in this IOM are snapshots of LCD pages at Ready for Training (RFT).



Page 7-7

7.5 Footer Pages

Footers appear at the bottom of all LCD pages. Footers contain controls to call LCD pages to the screen and miscellaneous controls such as malfunction resets and freezes. The footers on the upper and lower LCDs contain different information.

7.5.1 Footer No. 1

Footer No. 1 is displayed at the bottom of the display. It provides controls for displaying the plots and other commonly used functions.

The message area on the right side of the footer is a warning summary area that displays warnings for the following conditions:

- CB tripped - Crash suppress- Station failed - Environment non-standard



Item Description

PREV PAGE Selection displays the previously displayed page. When selected, the button remains active for two seconds.

FOOTER NO 2 Selection displays the Footer No. 2 page in the footer area.

SPEED UP X X Displays status and selection allows input of the ground speed, speed up factor. Selection maintains current indicated airspeed but increases ground speed rate by the speed up factor.

Although the speed up factor displayed on the button does not change, the speed up factor used in the simulation automatically reverts back to one in conditions where LNAV is engaged and the roll or pitch exceed reasonable angles. The purpose is to force back a normal speed to allow the aircraft to follow the flight plan properly in the critical phases of the flight plan. Please note the fuel consumption follows the speed up factor. (Min = 1, Max = Dynamic)

CAPTURE FLIGHT Displays status and selection activates a flight situation capture operation. When selected, the button remains active for 2 seconds. The button is dark if a recall is active.

RECALL LAST CAPTURE Selection displays the Recall Last Capture confirm popup menu.

SIMULATOR CONTROLS Selection displays the requested page.

HELP Displays status and selection activates/deactivates help mode. Selecting an item on the page while help mode is active displays a popup containing a description of the selected item. If no selection is made within 2-3 seconds after help mode is activated, a popup describing the functionality of the current page appears.

MASTER INDEX Displays status and selection displays the Master Index page on the display.



Page 7-9

Item Description

MAP Displays status and selection displays the Map page on the display.

APPROACH PLOT Selection displays the Approach Plot.

RUNWAY PLOT Displays status and selection displays the Runway Plot on the display.

COMM Selection displays the requested page.

FLIGHT FREEZE Displays status and selection activates/deactivates flight freeze.

When flight freeze is active, the following occurs:

(1) All flight parameters (i.e., pitch, bank,heading, airspeed) freeze.

(2) Altitude and position freeze.(3) The motion system freezes except for

washout as predicted by the flight conditionsat the moment of freeze.

(4) Sound level decreases.(5) Most simulated aircraft systems remain

unaffected and continue to follow crewactions and malfunction insertions exceptfor the effects of frozen altitude and positionparameters. Release of flight freeze doesnot cause violent control or motionmovements, irrespective of whether theautopilot is on or off and independent of thecontrol positions at the moment of unfreeze.

(6) During a reposition, the flight freeze buttonis dark until the reposition or flight trim iscompleted.

HARDCOPY Displays status and selection makes a hardcopy of the page displayed.

WARNING

DATE Displays the current year, month and day.

TIME Displays time in hours, minutes, seconds format.

AAAAAAAAAAAA Displays the warnings.



7.5.2 Recall Last Capture

Item Description

YES Displays status and selection performs a flight situation recall for the last flight situation capture operation. The button remains active until the flight freeze is released. This button is dark when conditions for performing a flight situation recall are not met.

CANCEL Displays status and selection cancels the operation.



Page 7-11

7.5.3 Footer No. 2

Footer No. 2 is displayed at the bottom of the display. It provides controls for accessing the most commonly used control pages and functions.

The message area on the right side of the footer is a malfunction summary area that displays all malfunctions that are active or preselected.

Item Description

PREV PAGE Selection displays the previously displayed page. When selected, the button remains active for two seconds.

FOOTER NO 1 Selection displays the Footer No. 1 page in the footer area.

MALF INDEX Displays status and selection displays the Malfunction Index page on the display.



Item Description

FAIL SUMMARY Displays status and selection displays the Fail Summary page, which lists all active/preselected malfunctions, popped CBs, and failed stations.

CLEAR MALF Displays status and selection clears all active and preselected malfunctions. This button is dark if no malfunctions are active or preselected. When selected, the button remains active for 2 seconds.

RETURN TO LESSON Selection displays the active lesson plan. This button is dark if there is no lesson plan active or a lesson is active and is currently being displayed.

HELP Displays status and selection activates/deactivates help mode. Selecting an item on the page while help mode is active displays a popup containing a description of the selected item. If no selection is made within 2-3 seconds after help mode is activated, a popup describing the functionality of the current page appears.

MASTER INDEX Displays status and selection displays the Master Index page on the display.

AIRCRAFT SET Displays status and selection displays the A/C Set page, which displays and allows input of aircraft parameters (e.g. GW, CG, fuel tanks).

POSITION SET Displays status and selection displays the Position Set page, which allows the instructor to reposition the aircraft, specify the reference runway, and initiate pushback.

ENVIR SET Displays status and selection displays the Environment Set page, which allows input of environment conditions (e.g., QNH, temp, runway conditions, special effects, and visual conditions).

RESETS/ FREEZES Displays status and selection displays the Freeze/Reset page, which lists the freezes and resets available.



Page 7-13

Item Description

FLIGHT FREEZE Displays status and selection activates/deactivates flight freeze.

When flight freeze is active, the following occurs: (1) All flight parameters (i.e., pitch, bank,

heading, airspeed) freeze.(2) Altitude and position freeze.(3) The motion system freezes except for

washout as predicted by the flight conditionsat the moment of freeze.

(4) Sound level decreases.

Most simulated aircraft systems remain unaffected and continue to follow crew actions and malfunction insertions except for the effects of frozen altitude and position parameters. Release of flight freeze does not cause violent control or motion movements, irrespective of whether the autopilot is on or off and independent of the control positions at the moment of unfreeze.

During a reposition, the flight freeze button is dark until the reposition or flight trim is completed.

HARDCOPY Displays status and selection makes a hardcopy of the page displayed.

MALFUNCTION

DATE Displays the current year, month and day.

TIME Displays time in hours, minutes, seconds format.

DESCRIPTION Displays the description of the selected malfunction.

SYSTEM DESCRIPTION Displays the system name of the selected malfunction.



7.6 Index Pages

All LCD pages can be requested for display via an index page. An index page lists by type, function or system all the LCD pages within a category, and page selection is accomplished by touch selecting the appropriate item.

7.6.1 Master Index

The Master Index page provides access to all index pages. Selection displays one of the simulation, graphics, messages control, recording control pages on the LCD.

Item Description

CUSTOMER AIRCRAFT Displays the customer name and aircraft type.

ENGINE TYPE Displays the engine type for the aircraft.



Page 7-15

Item Description

INDEX PAGES

MALFUNCTION Selection displays the requested page.

LESSON PLAN Selection displays the requested page.

RADIO STATIONS Selection displays the requested page.

SIMULATOR Selection displays the requested page. MAINTENANCE

SIMULATION SET

AIRCRAFT SET Selection displays the requested page.

POSITION SET Selection displays the requested page.

ENVIRONMENT SET Selection displays the requested page.

RESETS/FREEZES Selection displays the requested page.

PLOTS

MAP Selection displays the requested page.

APPROACH Selection displays the requested page.

RUNWAY Selection displays the requested page.

RECORDING CONTROL

FLT CAPTURE/RECALL Selection displays the requested page.

FMS MEMORY SAVE/ Selection displays the FMS Memory Save/ RECALL Recall page.

RADIOS

COMMUNICATIONS Selection displays the requested page.

ATIS/VOICE Selection displays the requested page.

ACARS Selection displays the requested page.



Item Description

MISCELLANEOUS

TCAS Selection displays the requested popup menu.

FAIL SUMMARY Selection displays the requested page.

AIRCRAFT UPSET Selection displays the requested page.

SIMULATOR CONTROLS Selection displays the requested page.



Page 7-17

7.6.2 Malfunction Index

The Malfunction Index page allows access to all the malfunction pages.

Item Description

ALL BUTTONS Selection displays the requested page.



7.6.3 Lesson Plan Index

The Lesson Plan Index page provides access to all the lesson plan pages. Selection displays the respective lesson plan page.

Item Description

RETURN TO ROOT Selection returns to the root of lesson index tree. This button is dark if the index is already at the root.

RETURN TO PARENT Selection returns to the parent index. This button INDEX is dark if the index is at the root.

LP Displays the current location (path) in the lesson index tree. The string will be blank when at the top most level (home).



Page 7-19

Item Description

INDEX SCROLL BAR Displays status and selection allows the instructor to scroll through the lesson/session index listing.

LESSON/INDEX CALL Selection displays the corresponding Lesson Index or Lesson Plan.



7.7 Control Pages

These LCD pages allow the operator to control and monitor the simulated aircraft configuration and environment.

7.7.1 Aircraft Set (737-800)

The Aircraft Set page provides control to change aircraft parameters (e.g., GW, CG, fuel tanks). It also displays the operating envelope of the aircraft, as well as the current aircraft configuration in the envelope. The instructor can with a single touch within the envelope change the aircraft configuration.

Item Description

GW Displays status and selection allows input of aircraft gross weight in the selected unit (Metric/Imperial). Selection of new gross weight is achieved with appropriate change in zero fuel weight. If new zero fuel weight is outside limits identified by approved data, then fuel weight is also adjusted as required. (Dynamic Min/Max)



Page 7-21

Item Description

ZFW Displays status and selection allows input of aircraft zero fuel weight in the selected unit (Metric/Imperial). Selection of new zero fuel weight is achieved with appropriate change in gross weight. If new gross weight is outside limits identified by approved data, then fuel weight is also adjusted as required. (Dynamic Min/Max)

FUEL Displays status and selection allows input of aircraft total fuel in the selected unit (Metric/Imperial). Fuel is distributed in accordance with the aircraft fuel distribution schedule. Selection of new fuel weight is achieved with appropriate change in gross weight. If new gross weight is outside limits identified by approved data, then zero fuel weight is also adjusted as required. (Dynamic Min/Max)

CG Displays status and selection allows input of center of gravity in % MAC. Selection of new aircraft center of gravity is achieved with appropriate change in zero fuel weight center of gravity. If new zero fuel weight center of gravity is outside limits identified by approved data, then the fuel weight is reduced and the zero fuel weight is increased as required. (Dynamic Min/Max)

EXECUTE Displays status and selection executes the selected aircraft configuration change ( Gw, ZFW, or CG). This button is dark if no change has been selected.

CANCEL Displays status and selection cancels the selected aircraft configuration change (GW, ZFW, or CG). This button is dark if no change has been selected.

SERVICES

GROUND POWER AC Displays status and selection activates/deactivates external AC electric power. External AC electric power is automatically disconnected if the aircraft starts moving. This button is dark when the aircraft is moving.



Item Description

EXTERNAL AIR Displays status and selection connects/disconnects external pneumatic ground air. External pneumatic air is automatically disconnected if the aircraft starts moving. This button is dark when the aircraft starts moving.

NAV FAST ALIGN Displays status and selection aligns the reference system bypassing the systems normal alignment period (IRS, INS, AHRS, ADIRS). This button is dark when the reference system is aligned or the reference system is off. When selected, the button illuminates active for 2 seconds.

APU QUICK START Displays status and selection starts the APU. The electrical and pneumatic outputs are available within 5 seconds. This button is dark when the APU is running or if correct conditions for operating are not met (master switch on, CB in, fuel available). When selected, the button remains active for 2 seconds.

ENG QUICK START Displays status and selection starts the dead engine dependent upon the correct conditions being met (e.g. fuel available, fuel levers at idle). This button is dark when all engines are running. When selected, the button illuminates active for 2 seconds.

A/C ON JACKS Displays status and selection selects/deselects the aircraft on jacks condition. It is possible to apply thrust without falling off or rotating around the jacks. When selected, the aircraft is raised such that the landing gear strut is fully extended. It is then possible to raise and lower the gear. This button is dark when the aircraft is moving. The A/C On Jacks and the A/C On Chocks selections are mutually exclusive.

A/C ON CHOCKS Displays status and selection chocks the wheels. The aircraft does not move under any conditions. This button is dark when the aircraft is moving. The A/C On Jacks and the A/C On Chocks selections are mutually exclusive.



Page 7-23

Item Description

MISCELLANEOUS

ALL SYSTEM RESET Selection resets all systems, including temperatures, to normal operating values: - Engine Oil Qty - Engine Oil Temp- Engine Exceedance - Fuel Temp- Fire Bottles - Hydraulic Fluid Temp- Hydraulic Fluid Qty - Brake Temp- IDG Oil Qty - Engine Gas Temperature- IDG Connect - Tire Pressure- Oxygen

When selected, the button remains active for 2 seconds.

A/C CONFIG QUICKSET Selection displays the requested popup menu.

DOORS Selection displays the requested popup menu.

FUEL SET Selection displays the requested popup menu.

V1 Displays V1 speed in knots.

VR Displays VR speed in knots.

V2 Displays V2 speed in knots.

VREF Displays Vref speed in knots.



7.7.2 Doors (737-800)

The Doors page provides controls for opening/closing the A/C doors.

Item Description

CLOSE ALL DOORS Selection closes all the aircraft doors. This button is dark when all the aircraft doors are closed.

FLIGHT DECK DOOR

OPEN Displays status and selection opens/closes the flight deck door. This button is dark if the flight deck door is locked.

ACCESS SYSTEM Displays status and selection toggles the access SWITCH NORM system switch between the NORM/OFF positions.



Page 7-25

Item Description

ACCESS REQUEST Displays status and selection emulates an access request at the flight deck door. This button is dark if the flight deck door access keypad is deactivated because an access request has been denied or if the system control unit is unpowered. When selected, the button remains active for 2 seconds.

EMERGENCY ACCESS Displays status and selection emulates an REQUEST emergency access request at the flight deck door.

This button if dark if the flight deck door access keypad is deactivated because an access request has been denied or if the system control unit is unpowered. When selected, the button remains active for 2 seconds.

ACCESS SYSTEM RESET Displays status and selection resets the flight deck door access system. This button is dark if a denied delay has not been activated by the crew via a cockpit panel selection. When selected, the button remains active for 2 seconds.

ALL DOORS Displays status and selection opens/closes theselected aircraft door.



7.7.3 Fuel Set

The Fuel Set popup menu provides controls to change the aircraft fuel.

Item Description

TOTAL Displays status and selection allows input of aircraft total fuel in the selected unit (Metric/Imperial). Fuel is distributed in accordance with the aircraft fuel distribution schedule. Selection of new fuel weight is achieved with appropriate change in gross weight. If new gross weight is outside limits identified by approved data, then zero fuel weight is also adjusted as required. (Dynamic Min/Max)



Page 7-27

Item Description

CENTER FUEL Displays status and selection allows input of fuel quantity in the center fuel tank in the selected unit (Metric/Imperial). Selection of new fuel weight is achieved with appropriate change in gross weight. If new gross weight is outside limits identified by approved data, then zero fuel weight is also adjusted as required. (Dynamic Min/Max)

CENTER FUEL TANK Displays maximum value for center fuel tank. MAXIMUM

LEFT WING Displays status and selection allows input of fuel quantity in the left wing fuel tank in the selected unit (Metric/Imperial). Selection of new fuel weight is achieved with appropriate change in gross weight. If new gross weight is outside limits identified by approved data, then zero fuel weight is also adjusted as required. (Dynamic Min/Max)

LEFT WING FUEL Displays maximum value for left wing fuel tank. TANK MAXIMUM

RIGHT WING Displays status and selection allows input of fuel quantity in the right wing fuel tank in the selected unit (Metric/Imperial). Selection of new fuel weight is achieved with appropriate change in gross weight. If new gross weight is outside limits identified by approved data, then zero fuel weight is also adjusted as required. (Dynamic Min/Max)

RIGHT WING FUEL TANK Displays maximum value for right wing fuel MAXIMUM tank.

FUEL BALANCE Displays status and selection balances fuel quantities in tanks. When selected, the button illuminates active for 2 seconds.

FUEL FREEZE Displays status and selection activates/deactivates fuel freeze. With fuel freeze active, all instruments other than fuel quantity indicate normally. All other aircraft systems remain unaffected except for the effects of frozen fuel. Refuel is possible when fuel freeze is active



7.7.4 A/C Config Quick Set (Metric & Imperial) - (737-800)



Page 7-29

Item Description

ALL BUTTONS Selection sets the aircraft to its predefined weights.



7.7.5 Position Set

The Position Set page provides control to change the reference airports reference runway and to reposition the aircraft with respect to the reference runway.

Item Description

REF AIRPORT Displays status and selection allows input of reference airport 4-character ICAO code or 3-character IATA code.

REF RWY Displays the current reference runway and selection displays the available runways popup menu.



Page 7-31

Item Description

AUTO REF RUNWAY Displays status and selection toggles between auto and manual mode. Auto allows automatic updates of the reference airfield to the nearest available runway until the nearest is the arrival airfield (then reference airfield locks to arrival airfield and runway). Selection unlocks if manual mode is selected or the arrival airfield is changed. In manual mode, the reference airfield and runway do not change unless there is new input from the instructor or lesson plan.

MEDIUM AIRWORK FL100 Displays status and selection repositions the aircraft to the medium airwork FL100 position, followed by the execute button, relative to the current reference runway. Flight freeze is set at the end of the reposition.

The aircraft is configured as follows:

Gear : Up Flap : Clean Speed: 250 KCAS Altitude: 10000 feet ASL Localizer Deviation: Centered Profile : Level Distance: 30 NM

HIGH AIRWORK FL350 Displays status and selection repositions the aircraft to the high airwork FL350 position, followed by the execute button, relative to the current reference runway. Flight freeze is set at the end of the reposition.


Gear : Up Flap : Clean Speed: Mach 0.78 Altitude: 35000 ft pressure alt Localizer Deviation: Centered Profile : Level Distance: 100 NM



Item Description

LATITUDE/LONGITUDE Displays status and selection allows input SXX:XX:XX/SXXX:XX:XX of new aircraft latitude and longitude positions.

LOCALIZER FAIL Displays status and selection fails the localizer of the reference runway.

GLIDESLOPE FAIL Displays status and selection fails the glideslope of the reference runway.

AIRPORT REPOS/ Selection displays the Airport Reposition popup LIGHTING menu.

12 NM, 1 NM LT Displays status and selection, followed by the execute button, repositions the aircraft to 12 nm, 1 nm left relative to the current reference runway. Flight freeze is set at the end of the reposition. Speed up is deactivated.


Gear : Up Flap : Flaps 5 Speed: 200 KCAS Altitude: 3000 ft AGL Localizer Deviation: 1 NM left Profile : Level Distance: 12 NM Intercept Angle: 30 degrees

LH DOWNWIND, 1NM, Displays status and selection, followed by the 3NM LT execute button, repositions the aircraft to LH

downwind, 3 nm abeam and 1 nm prior to touchdown point, relative to the current reference runway. Flight freeze is set at the end of the reposition. Speed up is deactivated.


Gear : Up Flap : Flaps 5 Speed: 200 KCAS Altitude: 1500 feet AGL Localizer Deviation: 3 NM left Profile : Level Distance: 1 NM



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Item Description

12 NM Displays status and selection, followed by the execute button, repositions the aircraft to 12 nm relative to the current reference runway. Flight freeze is set at the end of the reposition. Speed up is deactivated.


Gear: Up Flap: Flaps 5 Speed: 200 KCAS Altitude: 3000 feet AGL Localizer Deviation: Centered Profile : Level Distance: 12 NM



Gear : Up Flap : Flaps 5 Speed: Vref +5 Altitude: 2000 feet AGL Localizer Deviation: Centered Profile : Level Distance: 8 NM




Item Description


Gear : Down Flap: Flaps 30 Speed: Vref +5 Localizer Deviation : Centered Glideslope Deviation: Centered Profile : Descent Distance: 6 NM

3 NM Displays status and selection, followed by the execute button, repositions the aircraft to 3 nm relat

2RMX IOM - Flight Simulation Company...B737-700 Full Flight Simulator Instructor’s Operating...

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