(twin) manual
Contents
1. A conventional trim wheel is also provided for rudder trim Right rudder pressure can be trimmed out by rolling the rudder trim wheel to the right and vice versa Trim position indicators appears on the instrument panel a rudder neutral mark Also provided on the top right Yoke handle is a rocker switch lt gt which allows the user to fine tune RUDDER TRIM 2 ELEVATOR TRIM Conventional trim wheels are provided for pitch Rolling the pitch trim wheel forward will produce nose down trim and vice versa Trim position indicators appears on the instrument panel with a take off index mark Also provided on the top left Yoke handle is a rocker switch 0 which allows the user to fine tune ELEVATOR TRIM MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 6 V4 2 Issue 2 Aug 2008 OM6TV4 2 3 ENGINES 3 1 THROTTLES The throttles large black knobs are conventional in operation and provide a means of setting Manifold Pressure The trainer has normally aspirated fuel injected engines which will necessitate periodic throttle adjustment with changing altitude 3 2 PITCH LEVERS The pitch levers central black serrated knobs allow the RPM of the corresponding engine to be set and in the full rearward position to be feathered 3 3 MIXTURES Mixture controls are fitted red knobs which function generally in the normal way When in the cut off position no fuel will reach the engine which will therefore deliver zero pow2. a track made good display or an altitude profile display The track display is oriented True North and plots the trainer s track in relation to any navaids up to the last 50 that have been tuned These plots can be viewed at any time Plot information is progressively updated and plot data is retained The instructor console plots can be viewed while the trainer is flying and will progressively update At the pilot s console a composite plot is generated which while it can be viewed at any time causing the flight to freeze 1s intended to provide a single page print out at the completion of a flight for recording and verification purposes This manual contains in addition to detailed descriptions of the equipment operation a syllabus of ground training for the command instrument rating and typical flight scenarios applicable to the type of exercise appropriate for the gaining of recency credits for ADF VOR ILS amp LLZ and DME as well as instrument ground time MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 1 V4 2 Issue 2 Aug 2008 OM6TV4 2 MARK 6 TWIN EQUIPMENT CHECK LIST SUPPLIED IN THIS PACKAGE AERO GUIDANCE MARK 6 Twin Synthetic Trainer software CD Control Console Unit including Yoke assembly Rudder Pedal assembly Cross over network cable 5M USB A to USB B cable Operations Manual Including full instructions and enclosure drawing SUPPLIED BY THE CUSTOMER Two 2 computers each
3. having the following minimum specifications TYPE PROCESSOR RAM AUDIO VIDEO CARD DISPLAY MONITOR PORTS DISK DRIVES PRINTER SOFTWARE IBM or similar Intel AMD 1GHz or greater 512Meg minimum Sound card and speakers AGP or PCI Express 128MB minimum OpenGL Compliant Minimum 800x600 VGA colour 15 inch minimum 2 x USB ports 1 x 10 100 network port 1x CD ROM and Hard drive with 1GB free space Colour or mono printer Windows compatible For plot print out only Print out 1s required for CASA verification MS Windows XP VISTA or Win Enclosure built to AERO GUIDANCE Drg 01141191 In Ops manual 2 station intercom amp headsets Approach plates charts etc to suit intended exercise MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 2 V4 2 Issue 2 Aug 2008 OM6TV4 2 EQUIPMENT SET UP It is ESSENTIAL that a suitable location be made available for the trainer Most important in selecting a location is that the pilot or student using the trainer not be distracted in any way It is preferable that the location be in a separate room housing both consoles and appropriate briefing facilities although the latter could be located elsewhere Next most important is to ensure that the monitors are free of reflections This is best achieved by arranging them to face internal walls preferably dark coloured without strong light impinging on them It may be necessary to draw blinds
4. or curtains to achieve this The rest of the equipment should be arranged to provide comfort and a logical placement of the controls Since it is necessary to use the keyboard for some functions during flight although not simultaneously with other controls except the yoke and rudder care needs to taken in the placement of each component A suggested layout is given in Figure 1 Pilot Enclosure TABLE COMPUTER MONITOR KEY BOARI CONTROL BOX x a Y Rudder Pedal AR under table FIGURE 1 LAYOUT OF MARK 6 PILOT EQUIPMENT Once all the equipment has been arranged to provide a location free of distraction free of monitor reflection and comfortably laid out it can all be connected up as shown in Figures 2 amp 3 in preparation for starting the trainer MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 3 KEYB DARD rh rh ch rh rn AUDO DUT Network USB USB a ONITOR 5 is a 4 a Z er m m gt 2 STUDENT COMPUTER SPK P A RUDDER uw PEDALS CONTROL BOX STUDENT S STATION FIGURE 2 CABLE CONNECTIONS V4 2 Issue
5. sets a radius from the datum point which is displayed on the screenplot and represents nearly a full screen The value set can be any whole distance between 1 and 999 NM Leave or change the value then press TAB to move down to the next item PROFILE ALIGNMENT sets an azimuth in degrees magnetic for the profile plot Normally the final approach track bearing would be most useful and would allow reasonable comparison with the DAPs approach plate Again change or accept and press TAB to move down MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 15 V4 2 Issue 2 Aug 2008 OM6TV4 2 MAX DISPLAY ALTITUDE sets the vertical scale of the profile plot up to a maximum of 9000 feet Normally this would be set to the nearest 1000 feet above LSALT for the approach to be examined It can only be set in whole 1000 s of feet When this item has been set press ENTER or click OK to activate the settings and return to the instrument panel NOTE The plot displays the maximum and minimum altitude for the flight At any time they can be reset to current altitude by pressing the F8 function key It is important to do this at some point prior to commencing a procedure so that your altitude keeping can be accurately verified particularly minimas 11 6 PAUSE FACILITY At times it is desirable to pause and examine just what is happening To do this simply type p ENTER When ready to resume the flight press any key on the p
6. the Authority and for any changes subsequently approved by the Authority The conditions relating to the use of the trainer for instrument flight training and to instrument rating credits available under this approval are as set out in the relevant Civil Aviation Regulations or Civil Aviation Orders CtAng District Flight Operations Manager Mograbbin District Office lst May 1996 MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 36
7. using the NAV receiver in the same way as a VOR eg type n109 9 ENTER If the ILS is within range 25NM and 35 both localiser and glideslope flags will disappear and the needles will assume their correct position If an associated DME 1s present and Hold is initially OFF it will indicate distance NM ground speed Kts to the station and if applicable Time To Station Mins Hold can be turned ON if desired after tuning Check the ILS ident by pressing the audio panel NAV button The Markers MKRS are automatically tuned with the ILS but the MKRS button on the audio panel should be selected to hear the MKRS audio on flying over the beacons MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 12 V4 2 Issue 2 Aug 2008 OM6TV4 2 11 2 COMPASS AND HEADING INDICATOR HI DG Primary heading information is provided by the magnetic compass mounted on the panel Ensure wings are level and the compass is stable before setting the HI DG to ensure that turning and turbulence errors are minimised The HI DG will start up on the heading last indicated when the trainer was shut down however the trainer itself will be aligned to North magnetic To set the HI DG against the compass press the key to increase its reading or rotate the compass card anti clockwise and the key to reduce the reading Used alone these keys produce 10 degree increments or when used with the SHIFT key produce 1 degree increment
8. 2 Cross over Network cable oa Network port MONITOR INSTRUCTOR COMPUTER KEY BOARD INSTRUCTOR S STATION Kinetic Technology Internationa Pty Ltd N41 Model TVA1 FIGURE 3 REAR PANEL LAYOUT MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 4 Aug 2008 OM6TV4 2 V4 2 Issue 2 Aug 2008 OM6TV4 2 Installing knob retainer clips Retainer caps are supplied with the Twin Engine systems to allow the user to also operate the system as a Single Engine When operating the Aero Guidance in Twin Engine mode ensure retainer caps are removed To install align both knobs position cap over knobs and gently press down snap fit To remove rotate cap forwards on knobs and carefully lift back edge up LOADING THE PROGRAM Note The MARK 6 Twin version 4 is designed to run under Windows XP VISTA or Win7 and will not run under DOS Use the following process on both the Pilot and Instructor computers when installing Aeroguidance Insert the Aeroguidance CD into the CDROM and wait for the installation program to load If the autorun is disabled for the current CDROM then use the following steps to begin installation 1 Insert the CD into the CDROM Double click on My Computer Double click on the appropriate CDROM drive letter Double click on the Setup exe file to start the installation process Follow the on s
9. ARKERS MKRS SELECTED VOLUME MID SCALE YORE oon CENTERED BOTH AXES Hands off RUDDER CENTERED Feet off Select the starting details by clicking on the modify button in the Starting Details section Respond to the prompts that subsequently appear in the appropriate manner Enter in your departure airport and other prompts as they appear One prompt requests a radius of operation Type in a figure say 35 that will cover the area of the exercise Whatever radius 1s chosen can however be changed later as outlined in para 11 5 3 RE CENTERING amp SCALING Enter your name or licence number when requested for CASA log verification Another prompt the last will ask if you want a random failure If you nominate yes a random failure of the items selected will occur No warning or advice 1s given The full instrument panel will now appear on both computers The trainer is stationary on the ground and heading 360 deg Mag It is located at either the Aerodrome Reference Point of the nominated aerodrome or at the nominated latitude and longitude Proceed now with the planned exercise or select one of the sample exercises MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 21 V4 2 Issue 2 Aug 2008 OM6TV4 2 SHUTTING DOWN It is important that shut down is carried out in the correct manner to ensure that 1 The current VDO reading is recorded properly 2 Current t
10. ER is a software based system that couples the reliability and graphical presentation capability of modern desk top computer equipment with a simple man machine control panel that provides control devices very similar to those found on conventional light twin engine aircraft This MARK 6 trainer simulates a light normally aspirated twin engine aircraft having constant speed propellers and retractable undercarriage with a cruise speed in the range 150 200 knots TAS It is equipped with a conventional attitude flight panel including a Moving Card Heading Indicator airframe engine and fuel management panels a 3 axis auto pilot a clock and a stop watch A navigation panel is provided which is equipped with a fixed card ADF a VHF Nav receiver having VOR ILS Markers and DME and a non approach GPS with full waypoint capability At any time the Heading Indicator can be changed to a Horizontal Situation Indicator HSI The data file contains information on all Australian navaids aerodromes and waypoints as listed in ERSA It is possible therefore to fly any published procedure except GPS Approaches User USR waypoints can also be created Wind and turbulence conditions can be set or changed at any time and the trainer will respond accordingly Flight progress can be examined at any time This is accomplished by a simple reversible keyboard command that replaces the normal instrument panel display with at the instructor console either
11. OPERATIONS MANUAL MARK 6 Twin Engine SYNTHETIC TRAINER V4 2 x LICENSED TO AERO GUIDANCE SYNTHETIC TRAINER SYSTEMS Kinetic Technology International Pty Ltd 1 Kembla street Cheltenham East Victoria 3192 Australia Telephone 61 3 9583 9566 Facsimile 61 3 9583 9805 internet http www kti com au e mail info kti com au ACN 058 419 695 ABN 50 058 419 69 MARK 6 TWIN CONTENTS INTRODUCTION EQUIPMENT CHECK LIST EQUIPMENT SET UP LOADING THE PROGRAM OPERATING PROCEDURES 1 Main Flying Controls 1 1 Yoke 1 2 Rudder Trim 2 Elevator Trim 3 Engine Controls 3 1 Throttles 3 2 Pitch Controls 3 3 Mixtures 4 Fuel 5 Flaps 6 Undercarriage 7 Audio Panel 7 1 Selector Switches 7 2 ADF Test 7 3 Audio Volume 8 Auto Pilot Disengage 9 Power Supply 10 Press to talk 11 Keyboard Controls 11 1 Navaid Tuning 11 1 1 ADF 11 1 2 VOR or VOR DME or VORTAC or DMEN 11 1 2 1 OBS Setting 11 1 2 2 DME Hold 11 1 3 Using the GPS 11 1 4 ILS or ILS DME 11 2 Compass amp Heading Indicator 11 3 Auto Pilot 11 4 Wind Vector amp Turbulence Set up 11 5 View Plot 11 5 1 Pilot s Console 11 5 2 Instructor s Console 11 5 3 Re centering amp Scaling 11 6 Pause Facility 11 7 Stop Watch V4 2 Issue 2 Aug 2008 page 1 3 5 NO NO NO OO AWA OO N 1 1 G O MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE i OM6TV4 2 CONTENTS cont 11 8 Heading Bug 11 9 HSI Function 11 10 Re
12. T BE ARRANGED TO ILLUMINATE KEYBOARD amp CONTROL CONSOLE ONLY MUST NOT LIGHT MONITOR OR REAR OF ENCLOSURE OR DISTRACT OCCUPANT SCALE 20 1 AERLI GUIDANCE Position 2 station intercom to suit Revns 10 12 91 Genl detoit eee cee ee C 16 1 92 Width was 1200 additional notes added D 20 5 92 Table dims add E 8 7 93 Toble 100 deeper TITLE MARK 6 SYN TRAINER PILOTS ENCLOSURE DRAWN JN DATE 14 11 91 APPD DATE 13 7 01141191 E MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 35 V4 2 Issue 2 Aug 2008 OM6TV4 2 CIVIL AVIATION SAFETY AUTHORITY AUSTRALIA F85 1600 APPROVAL CERTIFICATE AERO GUIDANCE MK 6 T SYNTHETIC TRAINER SYSTEM This is to certify that the Aero Guidance Mark 6 T Synthetic Trainer system being a computer based software system produced by Kinetic Technologies International Pty Ltd of 1 Kembla Street Cheltenham East VIC 3192 having been assessed as complying with the required specifications equipment handling and operating requirements has now been designated as an approved Category B synthetic trainer system for the purpose of a conducting instrument flight training b accruing instrument ground time and c for satisfying recent experience requirements The system is not approved for the conducting of ab initio flight training This certificate remains valid for the Mark 6 T software program currently approved by
13. Your clearance is India Foxtrot Romeo clearance track Plenty Essendon planned route Maintain 3000 Sqwark 4013 On leaving 2500 call Melbourne Approach on 132 0 On calling Melbourne Approach passing 2000 you are told India Foxtrot Romeo climb to 3000 report maintaining After this call Approach tells you India Foxtrot Romeo Turn right heading 040 for vectoring for the ILS At 10 DME MB Approach advises India Foxtrot Romeo turn left heading 360 Position 6 miles South of the LLZ Continue heading 360 Make pilot intercept report established Subsequently you are handed over to EN tower who advise India Foxtrot Romeo make ILS approach For your overshoot at the minima turn left track to Moorabbin climb 4000 MB ATIS unchanged but you intend to practise an overshoot to 2000 then return to land Exercise ends at top of overshoot MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 24 V4 2 Issue 2 Aug 2008 OM6TV4 2 SAMPLE NDB RECENCY EXERCISE CHARTS REQUIRED ROMA QLD NDB PLAN Take off ROMA Enter holding pattern on climb via appropriate sector entry On reaching 3300 complete that holding pattern and enter the approach At the MAPt follow the published overshoot WEATHER ROM TAF 0214 18020KT 6000 80RASH 8ST1500 26 28 26 24 1013 1013 1013 1013 EXERCISE COMMENCES Set wind to forecast and turbulence to 3 When ready take off RWY 18 Make left turn Enter holding pattern via
14. aircraft must be turned toward the pointer to close the off course error Think of the scale centre as the aircraft and the pointer as the required course line Receiver Autonomous Integrity Monitor RAIM A red lamp labelled RAIM will illuminate when integrity is lost this is under the full control of the instructor at all times To turn the RAIM lamp ON the instructor issues the command fail RAIM by typing fr enter The RAIM lamp comes ON and 11 says on until the instructor clears RAIM by typing cr enter Cross track error Alert X TRACK A orange lamp labelled X TRACK Normally the lamp is off greyed out when the cross track error reaches 7degrees the lamp turns ON and says on until the error drops to below 7 degrees ENTERING OR MODIFYING USER WAYPOINTS User Waypoints may be entered to the database before a flight is commenced either add change or deleted using the GPS Waypoint Editor Once entered waypoints can be selected on the GPS instrument during the flight To access the editor at the Aeroguidance start up screen main menu select Database then GPS Waypoint Editor Also see Help at Aeroguidance start up screen main menu will step you through the procedure if required User Waypoint is selected in flight by pressing G and navigating across to the user waypoint tab See the user manual for more details on the GPS operations 11 1 4 ILS or ILS DME An ILS or ILS DME is tuned
15. al scale of initially 4000 feet and is oriented 90 to the horizontal To move back to the instrument panel press the ENTER key again Note that the trainer will freeze while the plot is displayed MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 14 V4 2 Issue 2 Aug 2008 OM6TV4 2 11 5 2 INSTRUCTOR S CONSOLE To move into the plot view screen change simply type s ENTER As at the pilot s console the screen will switch from the instrument panel to the TRACK and PROFILE plot To escape from the plot mode simply press ENTER and the instrument panel will be restored If the pilot console has been shut down the instructor screen will no longer update and can be exited by pressing q ENTER 11 5 3 RE CENTERING AND SCALING To initiate re centreing and scaling press the F5 function key The current screen will display a menu screen as below Reconfigure Plots Reconfigure Plot Datum Point S A N D or w Horizontal Scale 10 Profile Alignment 0 360 180 Maximum Display Altitude 4000 Cancel DATUM POINT permits the re centreing of the plot to one of the currently tuned navaids or waypoint WPT or back to the original start location Type S A N I D or W representing Start ADF VOR ILS DME or WPT or leave present setting Start depicted above then press TAB to move down to the next item or use the mouse to select the next edit position HORIZONTAL SCALE
16. course value is typed in preceded by the OBS identifier o For example to set OBS to 159 type 0159 ENTER If on the other hand it is desired to ascertain your present position line the OBS can be incremented through 360 degrees by repetitive pressing of the and keys for scan up and scan down respectively Used alone these keys produce 10 degree increments or 1f used with the SHIFT key produce 1 degree increments Note that the OBS setting 1s indicated at the top of the dial face and the reciprocal 1s displayed at the bottom If HSI is also active the orange Omni Bearing Pointer will point to the selected value on the rotating card 11 1 2 DME HOLD A HOLD facility is provided with the DME which enables it to remain tuned to a station while the NAV receiver is retuned to a different station To toggle the HOLD either ON or OFF press the h key This is an immediate control 11 1 3 USING THE GPS INTRODUCTION The Global Positioning System GPS gives the user a continuous readout of the aircraft position at all times and in addition provides a navigation facility which allows the user to specify a waypoint destination or en route point to which it is desired to track The GPS will indicate the bearing and distance to that point the time interval required to reach it at the current ground speed and will indicate the aircraft position relative to the direct track on a Course Deviation Scale similar to a VOR CDI Fiv
17. creen prompts to complete the installation Ot eee s Once the installation is complete Aeroguidance will install a shortcut on the desktop and a shortcut in the Start Bar On first use Aeroguidance will prompt the user for registration information Note Be sure to enter details exactly as shown on the registration sheet provided Once registration details are entered in Aeroguidance will open the Options window The user will need to specify the resolution Aeroguidance will use to display graphics Select an appropriate resolution to suite the graphics card monitor of your system The student computer will also need to specify the serial port in which the instructor computer resides Similarly the instructor computer will need to specify the serial port in which the student computer resides This can be accomplished from the Options screen in the Devices tab at start up MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 5 V4 2 Issue 2 Aug 2008 OM6TV4 2 OPERATING PROCEDURES 1 MAIN FLYING CONTROLS 1 1 YOKE The trainer uses a conventional yoke assembly as the primary control of roll and pitch It closely resembles the yoke of a conventional light aircraft and has the same sense that is clockwise turn produces right roll and yoke back produces nose up The sensitivity of the control is a function of airspeed where although the controls do not become harder and they have positive return to neutral at all speeds as s
18. ction 11 KEYBOARD CONTROLS MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 8 V4 2 Issue 2 Aug 2008 OM6TV4 2 9 POWER SUPPLY The power lamp PWR to indicate power is ON or OFF is located on the front left of the control console Power to control console unit is supplied via the USB cable from computer 10 PRESS TO TALK A red push button on the back of the yoke right hand grip provides a press to talk function when simulating use of the radio A transmitter signal is illuminated on the instructor s console while this button is pressed 11 KEYBOARD CONTROLS A number of functions none of which are of an urgent or immediate nature are actioned through the computer keyboards In summary these are 1 Navaid tuning 2 Setting the Heading Indicator 3 Auto Pilot selection and de activation de activation is also available from a yoke mounted push button Wind vector and turbulence set up Screen change to view plot Pause facility Stop watch Heading bug 9 HSI on off 10 Refuel 11 Reposition facility 12 QNH setting 13 Assigned Altitude setting 14 Simulating failures 15 Quit shut down the program Most of these controls can be operated from the instructor s console as well as from the pilot s An asterisk indicates those that have this capability owe 11 1 NAVAID TUNING 11 1 1 ADF The ADF is tuned by entering the NDB s published frequen
19. ctor is easily done from the keyboard by typing the required vector preceded by the identifier w For example to set a wind from 270 deg magnetic at 30 knots type w270 30 ENTER It is important to use the format exactly as shown that is w followed by 3 figures for direction followed by a followed by 2 figures for speed Wind can be zero d by the short cut method of typing w0 zero 0 ENTER 11 4 2 TURBULENCE Turbulence may be simulated with increasing levels of severity ranging from zero 0 to high 9 Moderate turbulence can be set for example by typing t4 ENTER 11 5 VIEW PLOT The trainer software retains in memory positional and altitude information for the most recent flight At any time during or after an exercise the track made good and the altitude profile can be viewed on the computer screen by swapping between the instrument panel display and the plot display 11 5 1 PILOT S CONSOLE To move into the plot view screen change simply type s ENTER The screen will now switch from the instrument panel to the plot The track made good will be displayed in red in relation to any navaids tuned up to 50 during the flight that are within the area viewed and centered initially on the start location The TRACK plot will be scaled according to the figure nominated at start up and is shown on a horizontal plot The PROFILE plot showing the trainer s flight profile appears in red on a vertic
20. cy through the keyboard preceded by an a being the trainers method of indicating that the ADF is to be tuned For example to tune the ADF to the Wonthaggi NDB type a383 ENTER If the NDB is within range the needle will assume its correct relative bearing and the morse ident WON __ will be heard if the ADF button on the audio panel is selected The ADF can be tested by pressing the ADF TEST button on the audio panel MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 9 V4 2 Issue 2 Aug 2008 OM6TV4 2 11 1 2 VOR or VOR DME The NAV receiver with it s associated DME receiver is tuned by entering the published frequency through the keyboard preceded by an n being the trainers method of indicating that the NAV is to be tuned For UE to tune the Wonthaggi VOR type n115 9 ENTER If the selected VOR 1s within range a function of altitude and distance the localiser flag NAV flag on the HSI RMI will disappear and the bearing indicator needle will assume a position relative to the OBS setting If a DME 1s present within range and with DME Hold OFF it will present slant distance NM ground speed Kts and Time To Station Mins The station ident can be checked by pressing the NAV and or DME button on the audio panel refer para 7 1 11 1 2 1 OBS SETTING The Omni Bearing Selector OBS can be set to a particular value in much the same way as the station 1s tuned In this case the required
21. ding button is pressed and the Morse ident will be heard if the aid is within range for as long as that button remains down To discontinue monitoring press the MKRS button or partially press another button to turn the audio select button to the UP position This will make Marker audio available but normally will simply result in silence No audio will be heard if no valid navaid is tuned 7 2 ADF TEST An ADF test button forms part of the audio panel Pressing this button at any time will cause the ADF needle to rotate for as long as the button is held down On release the needle will return either to the 090 parked position or if a valid NDB is tuned and within range to the correct relative bearing 7 3 AUDIO VOLUME and ENGINE SOUND All engine and navaid sounds are produced through the computer soundcard Volume levels may be altered through the computer speaker s volume control The engine sounds which are normally on can be toggled on off by pressing the F10 key To completely silence the ADF NAV or DME audio it is necessary to select MKRS or all switches OFF by partly pushing on a non operating audio select button which will release any selected button 8 AUTO PILOT DISENGAGE The Auto Pilot may be disengaged immediately by the pilot with the red push button mounted on the rear left hand yoke grip It may also be disengaged auto pilot tripped by the instructor with the command at To engage the Auto Pilot refer to se
22. e aircraft at any time e g w090 05 Following the w must have 3 digit direction then 2 digits e g t4 gives moderate turbulence Fails the AI Clear again with ca Fails the Headg Ind Clear with ch Fails the Turn Co ord Clear with ct Fails the NAV Rx Clear with cn Randomly fails one or other engine on climb or descent Clear by feathering prop Fails left engine immediately Clear with cel or by feathering prop As above but for right engine Fails the left vacuum pump Clear with As above but right vacuum pump Fails the Glideslope Clear with cg Fails the DME Clear with cd Fails RAIM on the GPS Clear with cr View the Track and Profile plots Enter to return to the panel Menu appears to permit reposition of A C Freezes the student s end Hit Enter to continue Terminates program amp returns to Windows MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 34 1400 V4 2 Issue 2 Aug 2008 OM6TV4 2 Reinforce alt joins with 25mm quad Joins and seams must be light tight Shelf to carry 25 Kg in centre Make from minimum 2 layers 12mm 1 particle board screwed and glued Round off front edge top amp bottom 1700 Position cable 059 cut out to suit dl 1050 600 MATERIAL 12mm PARTICLE BOARD FINISH INTERIBR MATT BLACK EXTERIOR TO TASTE LIGHTING MUS
23. e and trainer heading can then be entered Accept Cancel Note that the trainer remembers the reposition data as latitude longitude altitude and heading If you simply want to return to the previous re positioning point say to retry an aborted approach then nominate to enter latitude and longitude then click on OK MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 17 V4 2 Issue 2 Aug 2008 OM6TV4 2 11 12 QNH At start up the trainer sets a QNH of 1013 hP This may be altered by the instructor to some other value which will then require the pilot to set the same value for his altimeter to read correctly To set QNH type q followed by 3 or 4 numerals eg to set a QNH of 1023 type q1023 ENTER 11 13 ASSIGNED ALTITUDE INDICATOR An Assigned Altitude window on the pilot s instrument panel displays whatever 4 figure number the pilot enters The value entered is repeated on the instructor s console To enter an Assigned Altitude of 5000 type 5000 ENTER 11 14 SIMULATING FAILURES Provision exists to directly simulate the failure of various systems These are the engines their vacuum pumps the gyro instruments Attitude Indicator Heading Indicator alternatively HSI and Turn Co ordinator the NAV receiver the DME and the Glideslope To fail a system the prefix f is used and to clear the fault the prefix is used fa will fail the Attitude indicator ca will clear the fault fd wi
24. e classes of waypoint WPT are available to the GPS namely Airports APT Non Directional Beacons NDB VHF Omni range VOR Intersections INT User defined USR The last of these classes the USR WPTs are defined by the user and can be any point or place desired Use the User Waypoint editor program included with your simulator to enable the off line creation or modification of user WPTs Except for these USR WPTs all others use the Australian standard idents MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 10 V4 2 Issue 2 Aug 2008 OM6TV4 2 THE GPS SCREENS or WINDOWS Three windows can be displayed one at a time They are Window 1 NAV display The normal window Window 2 Nearest WPTs and pre selection Window 3 Confirm pre selection or specify other Selection of windows is in the strict order 1 2 3 1 and is initiated by typing g ENTER for GPS from the keyboard and then just Enter to cycle through to Window 1 again If no action is taken ie no keystrokes for a period greater than 10 seconds when within Window 2 or 8 the display will automatically revert to Window 1 and no change to WPT selection will occur Window 1 If no WPT has been selected the Brg ETI and Dis indications will be blank and the CDI scale will not display a pointer If G S is displayed in lieu of ETI it will indicate current ground speed irrespective of WPT selection G S or ETI display is toggled by
25. e day the computer program should be terminated before powering down This will ensure that things like VDO time restart values and so on are stored for subsequent use Terminate the program by typing q ENTER The instrument panel will disappear and the screen plot will appear giving the pilot a chance to print their current flight If you wish to print the plot press the p key ENTER otherwise type q ENTER The computer will then return to the Aero Guidance main window and bring up a prompt to confirm if you wish to save the flight log to a file POWER TABLE Altitude RPM 75 65 55 45 o 26 23 20 fis x o a a 19 ao a jo o o a x _ __ e e gt Geo a o APER 5000 ft o0 FT 7O 23 20 fis 2500 a tg 1240 23 20 oo do e 2 21 x o e e 22 10 000 ft 2700 FT 609 19 17 200 e o 81 19 x ao 20 ENENEE VON NENNEN e 15000 2700 Frd2 MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 19 V4 2 Issue 2 Aug 2008 PERFORMANCE SUMMARY 1 ENGINES Take off and Max Continuous Power Full throttle 2700 rpm Recommended Maximum Cruise Power 26 in Hg 2600 rpm 2 SPEEDS Extension 160KTS IAS Retraction 140KTS IAS A
26. er If the airspeed is above Vs and the propeller is not feathered the engine will continue to windmill but below Vs it will stop The engine is started simply by moving the mixture control to the full rich position with the pitch lever at full fine IE fully forward Assuming the throttle is retarded an idle speed of 600 RPM will result The trainer will not move on the ground in this condition Leaning the mixture should be done except in full power 100 power climbs below 5000 feet At all other times the mixture is carefully leaned to a point 2 divisions on the rich side of peak EGT Mixture should be readjusted whenever changing altitude and reset from time to time in cruise Note The VDO will increment only when either engine is rotating 4 FUEL Two wing tanks are fitted to the trainer with gravity feed Associated with each engine is a fuel selector switch with positions for normal feed an off position and a cross feed position Cross feed should normally only be used in cruise Fuel capacity is sufficient for about 180 minutes total time at normal cruise If necessary the trainer can be refuelled at any time by typing the command fuel on the keyboard Fuel consumption is zero at idle and idle cut off Otherwise it corresponds to the power level set 5 FLAPS The flaps can be set anywhere between zero and 30 degrees Flaps down is by pressing the center off switch downward and holding it until the desired setting is disp
27. er to complete FUNCTION ADF NAV VOR OBS GPS BUG ASSIGNED ALTITUDE QNH HSI RMI FUEL WIND TURBULENCE FAIL AI HI T C NAV Engine Left eng Right eng Left vac Right vac G S DME RAIM VIEW PLOT REPOSITION PAUSE QUIT FIRST KEY a nv none none none h mh mh NEXT KEY S 3 or 4 digits e g 117 6 must be in form 123 4 e g 117 6 must be in form 123 4 3 digits none 3 digits 4 digits 4 digits rmi fuel 5 digit vector 0 to 9 B ct gt er vl vr d r none none none none ACTION Tunes the ADF to the frequency represented by the numerals after the a e g a398 Tunes the NAV reciever to the specified frequency e g 117 6 MHz May be VOR VOR DME VORTAC or ILS Tunes ONLY the VOR indicator to the specified frequency e g 117 6 MHz May be VOR VOR DME or ILS e g 0330 Optional method of setting the OBS See also immediate method Enter to cycle through each window Use the number pad arrow keys to select in Window 2 Optional method of setting the Heading BUG See also immediate method e g 4000 or 0500 Sets the Assigned Altitude Indicator Has no other effect e g q1020 Sets QNH Student s end must match instructor s to eliminate altimeter error Type rmi to toggle the HSI RMI function ON OFF Refuels th
28. fueling 11 11 Reposition Facility 11 12 QNH 11 13 Assigned Altitude Indicator 11 14 Simulating Failures 11 15 Quit POWER TABLE PERFORMANCE SUMMARY STARTING THE TRAINER SHUTTING DOWN THE TRAINER INSTRUMENT GROUND TRAINING SYLLABUS PART 1 GFPT PART 2 PPL A PART 3 CPL PART 4 CIR SAMPLE ILS PLUS NDB RECENCY EXERCISE SAMPLE NDB RECENCY EXERCISE SAMPLE VOR RECENCY EXERCISE APPENDIX 1 EMERGENCY PROCEDURES REAL APPENDIX 2 Permissable Unserviceabilities APPENDIX 3 Student Endorsment APPENDIX 4 Instructor Endorsment APPENDIX 5 Approved Instructors APPENDIX 6 Maintenance Release APPENDIX 7 Summary of Keyboard Controls Drawing 01141191 Enclosure Approval Document V4 2 Issue 2 Aug 2008 OM6TV4 2 page 16 17 17 17 18 18 18 19 19 20 21 22 23 23 23 23 23 24 25 26 27 28 29 30 31 32 33 34 35 36 MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 11 V4 2 Issue 2 Aug 2008 OM6TV4 2 INTRODUCTION Important Note The MARK 6 twin engine synthetic trainer package includes additional software for both low and high speed single engine trainers However although the single engine software is compatible with the twin control console and may be used with it it does not have CASA approval when used in this way The single engine software approval is only valid when used in conjunction with a single engine control console The AERO GUIDANCE MARK 6 TWIN SYNTHETIC TRAIN
29. g fully trained in them 2 Explain fully the features of the Instructor s Console Demonstrate the method of tuning de tuning navaids setting wind and turbulence and communicating with the intercomm system 3 Point out that the instructor MUST remain at the instructor console for the duration of the exercise unless interrupted by a real emergency and maintain communications only via the intercomm The working of the press to talk function should be demonstrated in particular in respect of simulated radio communications 4 Demonstrate the method adopted by the school for logging the exercise and the correct method of shutting down the trainer Refer to the Shut down check list for this 5 When satisfied the instructor is fully competent to instruct on the trainer his or her name and details must be entered in the register of Approved Instructors in this manual and signed by the operator MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 30 V4 2 Issue 2 Aug 2008 OM6TV4 2 APPENDIX 5 APPROVED INSTRUCTORS List below all instructors endorsed to operate the MARK 6 MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 31 V4 2 Issue 2 Aug 2008 APPENDIX 6 AERO GUIDANCE MARK 6 SYNTHETIC TRAINER MAINTENANCE RELEASE OPERATOR LOCATION SERIAL NUMBER Item No Endorsements Certification Clearing Endorsement Date Daily Inspection Certification Since Last Prog Total Entry MARK 6 TWIN Sy
30. he GFPT training sequences in the school s approved operations manual PART 2 PRIVATE PILOTS LICENCE A INSTRUMENT TRAINING In accordance with the PPL A training sequences in the school s approved operations manual PART 3 COMMERCIAL PILOTS LICENCE INSTRUMENT TRAINING In accordance with the CPL training sequences in the school s approved operations manual PART 4 INSTRUMENT GROUND TRAINING SYLLABUS In accordance with the CIR training sequences in the school s approved operations manual MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 23 V4 2 Issue 2 Aug 2008 OM6TV4 2 SAMPLE ILS AND NDB RECENCY EXERCISE CHARTS REQUIRED Melbourne Essendon RWY 26 ILS or LLZ Melbourne Moorabbin NDB Area Chart Melbourne section PLAN MB to PLE at 3000 for a practise ILS to EN Overshoot at the minima and return to MB for an NDB at 4000 Overshoot MB END exercise MB ATIS MB terminal information ROMEO Runways 17 Arrivals and departures West RWY 17 Right frequency 123 0 Arrivals and Departures East RWY 17 Left frequency 118 1 Wind 150 to 190 20 gusting to 25 knots Crosswind 9 knots Cloud 3 scattered at 1500 QNH 1003 Temperature 15 EN ATIS EN terminal information QUEBEC Runway 17 Wind 150 at 25 knots Crosswind 9 knots QNH 1004 Temperature 15 Cloud overcast at 900 feet Expect instrument approach EXERCISE COMMENCES Set wind to ATIS and turbulence to 3 W150 25 and T3 resp
31. ilot s keyboard During Pause the instructor can move from the instrument panel to the plots using the s ENTER command 11 7 STOP WATCH A stop watch is provided to enable accurate timing for timed procedures This watch is coupled to the screen change and pause facilities so that timing is not lost The stop watch display is independently controlled on the instructor s panel To start the stop watch press the space bar once To stop and reset the stop watch press the space bar once again 11 8 HEADING BUG The heading bug is controlled in either of 2 ways First the bug can be set by typing the desired value as a 3 figure group preceded by the identifier b For example to set the bug to say 097 type b097 ENTER Alternatively the bug can be moved around the HI or HSI using single presses of the gt key to move clockwise and the lt key to move anti clockwise Used alone these keys produce 10 degree increments or if used with the SHIFT key produce 1 degree increments This is very convenient for setting up intercept angles and returning to the desired heading MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 16 V4 2 Issue 2 Aug 2008 OM6TV4 2 11 9 HSI FUNCTION Instead of the Heading Indicator HI which provides heading information and a bug only and is subject to precession a Horizontal Situation Indicator HSI RMI can be activated This function can be turned ON or OFF by typi
32. ir Minimum Control 65 KTS IAS OM6TV4 2 Single Engine Best Rate of Vyse 105 KTS IAS Climb 3 ASI MARKINGS 63 145 KTS IAS Full flap operating range Blue Radial 105 KTS IAS Single engine Best Rate Of Climb Red Radial 238 KTS IAS 70 202 KTS IAS Normal Operating Range Yellow Arc 202 238 KTS IAS Cautionary Range Smooth Air Only 4 PERFORMANCE Rate of Climb S L Max Cont 110 KTS 1700 ft min Rate of Climb S L 75 Power 110 KTS 1100 ft min Service Ceiling 18500 ft S E Rate of Climb Max Continuous 350 ft min S L Either Engine Vyse Either Engine po HO KTS po HT KTS PA KTS TAS MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 20 V4 2 Issue 2 Aug 2008 OM6TV4 2 STARTING THE TRAINER 1 Ensure that all plugs and cables are correctly and fully inserted in their respective receptacles Power up in the following order Monitor Pilot If not connected permanently to the computer Computer with Control Yoke Console Pilot Monitor Instructor If not connected permanently to the computer Computer Instructor Load Aero Guidance by double clicking on the Aero Guidance icon or though the start menu Check that the Control Console controls are set as follows PRE START CHECK LIST GREAT sospes DOWN THROTTLES CLOSED PROPELLERS PITCH FULL FINE MIXTURES CUT OFF TO CORRESPONDING TANKS M
33. layed on the instrument panel indicator Flaps up control is by moving the flap switch up momentarily causing the flaps to full retract Less than full retraction can be achieved during up travel by momentarily pressing flaps down Nose attitude airspeed and drag will change with flap setting A moderate ballooning will occur when the flaps are lowered particularly for the first 10 and some sink will occur when they are raised MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 7 V4 2 Issue 2 Aug 2008 OM6TV4 2 6 UNDERCARRIAGE An undercarriage control switch is provided which allows the landing gear to be raised and lowered Moving the switch to the UP position will initiate a gear retraction cycle and moving it to the DOWN position will initiate an extension cycle In each case indicators on the instrument panel will display the status Gear down and locked is indicated by 3 green lamps gear in transit is indicated by the GEAR label glowing red and gear up and locked is indicated by all 4 lamps being extinguished Gear cycle time is approximately 3 seconds during which airframe drag is slightly higher than in the gear extended condition 7 AUDIO PANEL 7 1 SELECTOR SWITCHES A panel of 4 lock on push buttons enable the selection one at a time of the audio output from the various navaids They are labelled ADF NAV DME and MKRS respectively When it is desired to monitor the ident of a particular aid the correspon
34. ll fail the DME cd will clear the fault fel will fail the Engine Left Refer note cel will clear the fault fer will fail the Engine Right Refer note cer will clear the fault fe will randomly fail an Engine Refer note No separate clearance fvl will fail the Vacuum Left will clear the fault fvr will fail the Vacuum Right evr will clear the fault fg will fail the Glideslope cg will clear the fault fh will fail the Heading Indicator ch will clear the fault fn will fail the NAV receiver en will clear the fault ft will fail the Turn Co ordinator not the ball ct will clear the fault fr will fail the RAIM cr will clear the fault Note Failure of an engine by any method will be automatically cleared once the corresponding propeller is feathered If the random engine failure method is requested one of two possibilities may occur depending on when the failure is requested If requested on the ground a failure may occur on take off or on approach If requested while airborne the failure will occur on approach No failure will occur in cruise To fail the ADF the most convenient way is to tune it just off frequency Random failures can be selected in the Aero Guidance main screen by clicking on Modify in the random failures section MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 18 V4 2 Issue 2 Aug 2008 OM6TV4 2 11 15 QUIT When the trainer is to be shut down for example at the end of th
35. ng rmi ENTER The HSI RMI provides in addition to heading information NAV and ADF displays The NAV display consists of an orange coloured Omni Bearing Pointer with Deviation Bar and a Glide slope GS pointer each with a corresponding 5 dot scale NAV and GS flags appear when the corresponding signals are invalid The ADF display consists of a green coloured pointer head and tail with no central section which will indicate the course to and from the NDB when in range Out of range indication is given by a constant 90 abeam indication A COMPASS flag will appear when the HSI RMI reading is inoperative as a result of vacuum or instrument failure 11 10 REFUEL The trainer has an endurance of approximately 180 minutes total shared between the two tanks It can be refuelled at any time even in the air by typing the command fuel ENTER 11 11 REPOSITION FACILITY This is a facility to enable a procedure Relocate to be recommenced from a specified location altitude and heading Relocate A reposition is invoked by typing Relocate Using Parameters r ENTER Latitude 42 degrees 14 5 Two choices for repositioning are offered viz by entering latitude and longitude or Hegees 122 by nominating one of the currently tuned Sipat navaids or WPT then specifying bearing PEE and distance from that aid WPT Following Radial Distance Alituds 2000 m this position information altitud
36. nt or the main wall outlet itself Vacate the area of immediate risk Raise the alarm Refer local procedures F Take other action as dictated by local circumstances e g fire extinguishers evacuation procedure etc FIRE OTHER THAN THE EQUIPMENT Follow local site requirements ELECTRICAL SHOCK Follow local site requirements OTHER EMERGENCIES Follow local site requirements MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 27 V4 2 Issue 2 Aug 2008 OM6TV4 2 APPENDIX 2 SCHEDULE OF PERMISSIBLE UNSERVICEABILITY There are NO permissible unserviceabilities for instructional use For solo recency use it is permissable for the instructor s console to be non operational MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 28 V4 2 Issue 2 Aug 2008 OM6TV4 2 APPENDIX 3 STUDENT ENDORSEMENT To be carried out by the Operator or an Approved Instructor Following power up the student or pilot under instruction should be seated in the normal control position such that all controls are within easy reach and can be comfortably operated to their respective extremes A start up location such as Moorabbin Vic should be chosen so that a Navaid of each type is within range and their working can be effectively demonstrated 1 Go over the real emergency check list and confirm that the student understands fully his required actions 2 Explain the features of the trainer and i
37. nthetic Trainer Copyright AERO GUIDANCE 32 OM6TV4 2 APPENDIX 7 V4 2 Issue 2 Aug 2008 OM6TV4 2 SUMMARY OF KEYBOARD CONTROLS IMMEDIATE No Enter required FUNCTION KEY HDG IND set Si OBS set V UI BUG set gt lt DME hold h STOP WATCH Space bar AUTO PILOT F1 Hdg Hold Altitude Hold F2 RECONFIGURE F5 PLOT RESET ALT F8 LIMITS ENGINE SOUND F10 Continued over ACTION Alone causes the HI to read 10 higher With Shift causes the HI to read 1 higher As above but reads lower Alone causes the OBS to increase by 10 With f Shift causes a 1 increase As above but causes a decrease Alone causes the BUG to increase 10 With Shift causes a 1 increase As above but causes a decrease Toggles the DME between hold ON and OFF Toggles the stop watch between counting up from Zero and reset to zero The auto pilot will couple to the Hdg bug and turn the aircraft to this heading Use again for OFF Providing Hdg Hold is ON F2 will toggle altitude hold Brings up a menu which allows recentering rescaling azimuth and max displayed altitude to be changed Resets the MAX and MIN altitude recorder to the current altitude Use before commencing approach Viewed on either plot Toggles engine sound between ON and OFF MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 33 V4 2 Issue 2 Aug 2008 OM6TV4 2 NON IMMEDIATE DATA ENTRY Requires Ent
38. peed increases they do become more sensitive The yoke incorporates a red thumb operated push button on the back of each hand erip The right hand button is a press to talk PTT switch and the left hand button allows quick autopilot disconnection As an option the sensitivity for both roll and pitch can be set by the user before a flight is commenced At the Aeroguidance start up screen main menu select Options then Preference and Devices tab an option for pitch and roll sensitivity can now be set for the desired performance 1 2 RUDDER TRIM The rudder control is of the pedal type and is conventional in operation with positive return to neutral pressure The sensitivity of the rudder increases with airspeed but does not become harder The rudder becomes slowly effective once the trainer exceeds about 2 knots but is not really useful below about 20 knots It works as if a castering nose wheel was fitted so that at low speeds turns are best achieved with asymmetric power Therefore a combination of rudder and some asymmetric power can be used to turn while on the ground to say line up for take off on a chosen runway heading On the ground such turns will give appropriate indications on the turn co ordinator and the balance ball as well as the Heading Indicator Compass and if tuned the ADF In the air the rudder is used in the conventional way primarily to make balanced turns and to offset asymmetric yaw effect
39. pressing either the T or 4 keys Window 2 This window 1s used to find the nearest seven WPTs for each of the WPT classes Pre selection is achieved by first selecting the WPT class using the lt and keys VOR shown here then using the T and J keys to select the actual WPT from the list displayed in this example WON and then within 10 seconds press the key If the WPT you want is not displayed probably because it is further away than those displayed simply press 4 no matter which WPT 1s pre selected then type your selection in Window 3 Window 3 In this window you can confirm the pre selection from Window 2 it will be displayed by simply pressing the key OR you can over type the pre selection with another choice then press l As soon as the key is pressed the display will revert to Window 1 and providing time out did not occur your new selection will be displayed along with the bearing distance and Estimated Time Interval ETD and the CDI will be centred MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 11 V4 2 Issue 2 Aug 2008 OM6TV4 2 Note that the CDI scale represents at its extremes an off course deviation of 5 NM Each division therefore represents 1 NM off course and off course deviations greater than 5 NM are indicated by an arrow at the scale extreme indicating the direction in which the pointer has moved off scale The CDI sense is the same as that used in a VOR That is the
40. rainer calibration settings are preserved If lost the trainer will revert to the setting used in the previous session which may require a re configuration at start up 3 The Instructor s Console may be used for other purposes which may be compromised if the correct procedure is not followed 4 Reinforces good shut down practise PROCEDURE 1 Type q ENTER on the Instructor s Console This will restore that computer to Windows 2 Type q ENTER on the Student s Console This action will display the current settings for VDO start Lat and Long relocate Lat and Long and control calibration constants to be recorded Three options are listed on the bottom of the screen Option 1 Typing q ENTER to quit Option to save Logfile Option 2 Typing p ENTER to print Option 3 F5 to adjust display format 3 GEAR down THROTTLES to idle PROPELLERS to full fine MIXTURES to idle cut off FUEL SELECTORS to off TRIMS to take off MKRS selected 4 Student computer shut down sequence to power off as required Student monitor power off If not controlled by computer power switch 5 Instructor computer shut down sequence to power off as required Instructor monitor power off If not controlled by computer power switch MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 22 V4 2 Issue 2 Aug 2008 OM6TV4 2 INSTRUMENT GROUND TRAINING SYLLABUS PART 1 G F P T TRAINING In accordance with t
41. s The HI DG will precess during operation The and keys with the SHIFT key can be used to periodically realign it Note In HSI mode if vacuum is available the instrument is slaved to the compass and does not require setting or re setting 11 8 AUTO PILOT The Auto Pilot fitted to VH IFR provides HEADING and ALTITUDE HOLD In the HEADING HOLD mode the trainer will couple to the heading bug on the HI Refer to section 11 8 for instructions on setting the Heading Bug ALTITUDE HOLD which can only be engaged if HEADING HOLD is already engaged will stabilise the trainer at the altitude at which it is engaged Note however that if the trainer is not trimmed properly before engaging ALTITUDE HOLD then a slow altitude creep will occur To engage HEADING HOLD press the F1 key The HEADING HOLD lamp will illuminate To engage ALTITUDE HOLD press the F2 key after HEADING HOLD is ON The ALTITUDE HOLD lamp will illuminate Either can be disengaged by the pilot by pressing the respective keys a second time but if the HEADING HOLD is disengaged while ALTITUDE HOLD is ON they will both be disengaged A button on the right hand yoke grip also provides a complete disengage The instructor may disengage the auto pilot auto pilot trip by entering at MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 13 V4 2 Issue 2 Aug 2008 OM6TV4 2 11 4 WIND VECTOR AND TURBULENCE SET UP 11 4 1 WIND Setting the Wind ve
42. sector entry on climb to 3300 From 3300 when ready make NDB approach At the MAPt overshoot as per procedure Exercise ends at top of overshoot MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 25 V4 2 Issue 2 Aug 2008 OM6TV4 2 SAMPLE VOR RECENCY EXERCISE CHARTS REQUIRED CHARLEVILLE YBCV QLD VOR Rwy 12 PLAN Take off CV intercept an outbound radial then intercept an inbound track to overhead then complete the CV RWY 12 VOR including the overshoot from the MAPt WEATHER CHARLEVILLE YBCV YBCV METAR YBCV 0530 10020KT CAVOK 21 MS05 1024 TAF YBCV 0214 12015KT CAVOK 20 22 17 10 1027 1025 1026 1027 EXERCISE COMMENCES Time 0535 Set wind to best information Set turbulence to 3 When ready take off CV runway 12 Intercept the CV VOR 085 radial before 5 miles and climb to 2900 At approximately 8 miles turn to intercept the VOR 120 radial inbound Manoeuvre as necessary for a direct entry to the Cat A initial leg of the CV RWY 12 VOR approach Carry out the Cat A approach At the MAPt carry out the missed approach procedure Exercise ends at top of the missed approach MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 26 V4 2 Issue 2 Aug 2008 OM6TV4 2 APPENDIX 1 EMERGENCY PROCEDURES REAL SMOKE OR FIRE FROM THE EQUIPMENT 5 If practical without any danger to the person immediately switch off the subject equipment This may be practical at either the equipme
43. ts controls to the student while still on the ground paying special attention to those items requiring keyboard entry since these will be new In particular it can be expected that many more mature students will be unfamiliar with key entry systems and require a little time to adjust Therefore tuning of Navaids and setting the Heading Indicator bug and OBS should be practised until reasonable competence is achieved 3 Demonstrate the use of the intercom and show how the press to talk button is used Explain that for simulated radio calls the press to talk must be used 4 Briefly explain those facilities available to the instructor and the way in which they will be used during this and future exercises 5 Patter the student through a start up take off cruise and approach including Navaid tuning until satisfied that he or she is familiar with the trainer functioning MARK 6 TWIN Synthetic Trainer Copyright AERO GUIDANCE 29 V4 2 Issue 2 Aug 2008 OM6TV4 2 APPENDIX 4 INSTRUCTOR ENDORSMENT To be carried out by the Operator PREREQUISITE If the instructor to be endorsed has not previously used the trainer as in the case of a new instructor joining the company he or she should first be given student endorsment to achieve familiarity with flying the trainer Then 1 Ensure the instructor is fully conversant with the emergency procedures real and understands that he or she is responsible for the student bein
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