Configuration manual
Contents
1. Servo Setup Servo Setup This submenu provides options for determining connected servos by user and its automatic detection e Menu Servo Setup e Servo Roll o Installed YES o Installed NO o Slip e Servo Pitch o Installed YES o Installed NO o Slip e Servo Yaw o Installed YES o Installed NO o Slip e Servo Detection Servo Roll Servo Pitch Servo Yaw You can see above that adjustable options for all servos are same Therefore these options are collectively described below and apply to all Servos Installed YES Installed NO You can choose just one of these options Installed YES or Installed NO That determines whether the appropriate servo is installed or not Page 28 Autopilot Section TL ELEKTRONIC Servo Setup Slip Option Slip provides adjusting of servo slipping That means that you can set amount of transmitted torque via magnetic clutch before slipping If you set higher number more torque could be transmitted and you will have to exert much more force in case of manual adjustment when the AP is active There is no drag which could be exerted by turned off AP on yoke and rudder pedals Range of maximum transmitted torque is from 0 to 100 with 5 step Servo Detection You will have to execute this procedure because it s necessary to assign servos to appropriate controlled axes Follow the instructions which will appear on screen Servo Deflection Calibration This submenu serves for calibrat2. The Min Air Speed must be set to at least 30 above Vs This is default setting of Min Air Speed value Max Air Speed Max Air Speed is maximum airspeed at which you can activated the AP If actual airspeed is higher than set Max Air Speed the AP will pitch the aircraft up to decrease actual airspeed If aircraft s altitude is higher than altitude determined by Altitude Bug or Navigation source VOR or GPS and the AP can t pitch the aircraft down without Max Air Speed get exceed the Integra will display message REDUCE POWER The Max Air Speed must be set to at most 95 of Vne This is default setting of Max Air Speed value Page 35 Autopilot Section TL ELEKTRONIC Ptch Axis Setup amp Enter Re Activation 7 WARNING Default values of Min Air Speed and Max Air Speed are set according to Vs Stall Speed and Vne never exceed speed values which are set in menu EFIS Range and Limits see on page 11 Proper readjustment from default values of Min Air Speed and Max Air Speed isn t watched by the Integra So make sure that you know what you are doing Enter Activation Enter Reactivation The last option in menu Autopilot Setup is Enter Activation or Enter Reactivation Enter Activation is displayed when Activation Key hasn t been entered In that case the Autopilot function isn t enable When you ve already entered Activation Key option Enter Reactivation is displayed If you want to upgrade your Acti
3. This menu contains settings for sensors of temperature e Menu Configuration amp Sensors e e OAT e AUXT IAT Internal Air Temperature OAT Outside Air Temperature AUXT Auxiliary Temperature After you choose option for setting IAT OAT or AUXT from the menu you ll get list of available sensors You can assign one of them to selected temperature or disable displaying of selected temperature by option Not Connected Page 10 EFIS Setup Menu esac and Lin TLELEKTRONIC EFIS RANGE and LIMITS In this menu you can set airspeed values Airspeed limits Menu Range and Limits kts Airspeed Vne Never exceed 210 Vne never exceed Vno Maximum structural cruising 170 e Vno maximum structural cruising Vfe Maximum flap extended 70 e Vfe maximum flap extended Vs Stall speed 50 e Vs stall speed y i S so Min speed in landing config 30 e Vso minimum flight speed in landing configuration 9 9 NOTE The limits of one each Vne Vno Vfe Vs or Vso cant overlap each other If you try decrease for example Vne and it is impossible so you need to decrease Vno at first and than you can set Vne to lower value Page 11 EFIS Setup Menu Range and Limits Vne Never exceed speed Change the underlined by rotating the right Knob After you get required number just press the knob and the underscore skips on to the next number Press Set to enter the value Press Cancel to s
4. ug e EE 18 EFIS EXTERNAL DEVICES E 19 EE 20 LINA COM se ise ces coves dial 20 REMOTE COMPASS ss se ce olt alea gooey cei a dt li suds a E dt alu aii 21 GUARDIAN ai 22 EFIS DATA SHA ANE 23 ASAS EE 24 MACIAS In RO 24 Page 2 Introduction TLELEKTRONIC Table of Contents AUTOPILOT OPTIONAL FUNCTION E 26 SERVO SETURB te e ca AM Meer e O e Mara e e tee e ee ae pate E 28 SERVO DEFLECTION CALIBRATION Es 29 EXTERNAL BUITON ns e aia a a a 30 ER EN rr re ai a a a eimi red 32 PITGHRAXIS A So d aia dt it E a d See dal i a ada a dt a alas a ia aaa a aa aia aes ese ane 34 ENTER ACTIVATION ENTER REACTIVATION eegene ss d i a E i a ai a a nn a dt i at EE a a a ia atat EE 36 Page 3 Introduction TLELEKTRONIC Record of Revision Record of revision Revision Revision Date Description ECO Insertion date By A 1 10 2008 Initial version 0001 Jezek B 2 2 2009 Language correction Jezek 14 7 2009 New function added Jezek D 1 10 2009 New function added Jezek E 5 12 2010 New functions added Hovorka Page 4 Introduction Warnings Cautions amp Notes 7 WARNING If setup or calibration data is inadvertently or improperly changed there could be inaccurate readings that may lead to improper operation of the aircraft or engine This could result in engine damage and or an emergency situation
5. AN CAUTION Use the INTEGRA at your own risk To reduce the risk of unsafe operation carefully review and understand all aspects of this Configuration Manual and the Flight Manual Supplement and thoroughly practice basic operation prior to actual use When in actual use carefully compare indications from the INTEGRA to all available navigation sources including the information from other NAVAIDS visual sightings charts etc For safety always resolve any discrepancies before continuing navigation NOTE It is the pilot s responsibility for initial missed approach guidance in accordance with published procedure The unit may not provide correct guidance until established on a defined leg NOTE GPS level of service annunciations are not applicable to the external CDI or HSI when VLOC is active TL elektronic is fully committed to your satisfaction as a customer If you have any questions regarding the INTEGRA please contact our customer service department Page 5 EFIS Setup Menu Introduction EFIS Setup Menu Page 6 EFIS Setup Menu unam Units O NOTE This manual assumes that you have read User Manual and you ve mastered operation of the Integra In this menu you can set up many parameters mainly for flight settings Access to this menu Press right knob select Enter Setup in menu When prompt Are you sure you want to enter to setup appears press Yes There in Setup mode switch screen to EFIS
6. Control Sensitivity Mode Turn Rate Mode Bank Angle Max Bank Angle Turn Rate Target Control Sensitivity This parameter specifies how fast the AP reacts to deviations between target heading and actual heading If the parameter is adjusted too high the aircraft will be itchy Fast hardline adjustments of heading will appear If the parameter is adjusted too low the aircraft will leisurely responds to heading deviations Range of values of the parameter is from 1 to 24 Value 1 refers to low sensitivity value 24 refers to high sensitivity Default value is 10 Page 32 Autopilot Section TL ELEKTRONIC Roll Axis Setup Mode Turn Rate Mode Bank Angle These options are entitled here together because they are two options of one switch metaphorically told That means that you can choose Mode Turn Rate or Mode Bank Angle Mode Turn Rate If you select this mode the AP will control the aircraft according to parameter Turn Rate Target described below and Max Bank Angle described below Mode Bank Angle If you select this mode the AP will control the aircraft according to parameter Max Bank Angle Max Bank Angle The parameter determines maximum bank angle of the aircraft during AP s controlled turns Range of adjustable values of the parameter is from 5 to 45 degrees Default value is 15 degrees and it is adjustable in 1 degree increments Turn Rate Target The parameter determines average target turn rate of the aircraft
7. Menu Remote compass e Not connected e Connected e Settings e Declination e Inclination e Total Mag Field 350 000 010 e Build In ME e Calibration If Remote Compass is not connected you will not have Heading data If Remote Compass is connected on Integra but Remote Compass is missing or there is a problem with communication heading data display ERROR If Remote Compass is connected properly you will have correct Heading data 220 228 240 Menu Settings To calibrate your Remote Compass you must input your location s current magnetic inclination angle and intensity Before doing this you must obtain these two values for the geographic location where you will be performing the calibration Note that this procedure only needs to be done once prior to magnetic calibration Moving the aircraft to another location does not require repeating this procedure Obtaining Magnetic Inclination and Intensity 1 TL elektronic recommends The National Geophysical Data Centre NGDC of the National Oceanic amp Atmospheric Administration website at http www ngdc noaa gov geomagmodels IGRFWMM jsp to obtain inclination and intensity Select your country and your city Click on Compute Magnetic Field Values button at the bottom of the page to obtain values needed for the EFIS INTEGRA Set up in Integra DECLINATION INCLINATION and TOTAL FIELD in agreement with this website Set up in Integra posi
8. Press right knob again you should see Menu EFIS Setup now e Menu EFIS Setup Units Configuration amp Sensors Range and Limits Other Settings amp Calibration External Devices EFIS Data Sharing Autopilot Setup Language Demo Mode Exit Menu Page 7 EFIS Setup Menu Units UNITS You can choose between metric and imperial units or you can define your own unit settings e Menu UNITS e Metric e Imperial UK e Imperial US e Custom Metric INTEGRA display units in metric system km h m mBar km m s Imperial UK INTEGRA display units in metric and imperial system kts ft mBar nm ft min Imperial US INTEGRA display units in imperial system kts ft inHg nm ft min Custom you can choose individual units for each measure e Menu Custom Airspeed Altitude Baro pressure Distance VSI You can choose between metric and imperial units or you can define your own unit settings You can try changing some units Take note EFIS screen is changed by how you modified values to metric or imperial Page 8 EFIS Setup Menu Units Available units for measured quantities d Selectable units Quantities Digital speed indicator km h kts mph Airspeed strip km h kts mph Baro pressure inHg mBar Altitude strip feet metre Digital altitude indicator feet metre Vertical speed indicator ft min kts m s Page 9 EFIS Setup Menu unam Configuration amp Sensors EFIS Configuration amp Sensors
9. Turn Rate target is specified in angular degrees per second That means for example when Turn Rate Target is 1 degree per sec then aircraft s turn of 90 degrees will be performed in 90 seconds Remember that adjustable value of the parameter is only average value which could be exceed due flight dynamics and the time for turn initialization Range of adjustable values is from 0 5 degree to 3 degrees per sec Default value is 1 5 degree per sec and it is adjustable in 0 1 degree per sec increments Page 33 Autopilot Section TL ELEKTRONIC Pitch Axis Setup Pitch Axis Setup This submenu provides settings of the AP performance during controlled change of altitude e Menu Pitch Axis Setup e Control Sensitivity e Mode Vertical Speed Mode Longitudinal Angle Max Longitudinal Angle Max Climb Speed Max Descent Speed Min Air Speed Max Air Speed Control Sensitivity This parameter specifies how fast the AP reacts to deviations between target altitude and actual altitude If the parameter is adjusted too high the aircraft will be itchy Fast hardline adjustments of altitude will appear If the parameter is adjusted too low the aircraft will leisurely responds to altitude deviations Range of values of the parameter is from 1 to 24 Value 1 refers to low sensitivity value 24 refers to high sensitivity Default value is 10 Mode Vertical Speed Mode Longitudinal Angle These options are entitled here together because they are two op
10. amp CALIBRATION This menu allows you to modify settings and calibrations e Menu OTHER SETTINGS amp CALIBRATION e Aircraft Identification e Time e Date e Pitch Setting e Backlight control e AUX Input Output e Main Switch Control Aircraft identification The Aircraft ID Box has Letters A Z numbers 0 9 blanks and symbol The ID can also be ENS shortened to fewer than 8 digits AIRCRAFT The underlined letter you can change just rotate with the right knob If you get required letter just Position press the knob and the underscore will skip on to the next letter Then press Set to enter the new value Press Cancel to skip previous menu Page 15 EFIS Setup Menu Other Setting amp Calibration Time You can set the time The underlined numbers you can change just rotate with the right knob If Time you get required time just press the knob and the underscore will skip on to the next number Then press Set to enter the new value Press Cancel to skip previous menu cance O NOTE It is necessary to set UTC Zulu time on the INTEGRA Clock Date You can set the date The underlined numbers you can change just rotate with the right knob If Date you get required time just press the knob and the 18 02 09 underscore will skip on to the next number Then press Set to enter the date Please insert date in Cancel Set Position the form of DD MM YY or day month year P
11. a Eee INTEGRA EFIS TL 6524 CONFIGURATION MANUAL Non TSO approved LEKTRONIC 220 230 240 1400 TL elektronic Airport Building 125 503 41 Hradec Kralove Czech Republic Copyright 2008 2010 TL elektronic All Rights Reserved Except as expressly provided below no part of this manual may be downloaded transmitted copied reproduced disseminated or stored in any storage medium for any purpose without the express prior written consent of the TL elektronic company Address your questions about the technical information to TL elektronic Other information about sale distribution should be directed to our exclusive distributors see World Distributor list on our website Producer s address TL elektronic Inc Airport Building 125 503 41 Hradec Kralove Czech Republic Fax 420 49 548 23 94 E mail info tl elektronic com Web Site Address www tl elektronic com Please send your e mail address to customer tl elektronic com to receive the latest information about software upgrade Send your ideas to innovation tl elektronic com We will evaluate your suggestion and provide an update Windows is registered trademark of Microsoft Corporation All trademarks and registered trademarks are acknowledged SchecK is registered trademark of TL elektronic iFamily is registered trademark of TL elektronic sModern is registered trademark of TL elektronic All information in this User s manual i
12. ion of deflections of servos and their subsequent test e Menu Servo Deflection Calibration e Deflection Calibration e Deflection Test Deflection Calibration This procedure identifies range of motion of each servo and it should be executed before servo Deflection Test Just follow the instructions on the screen for successful completion of calibration Deflection Test By using this option you can test servos assignment to controlled axes and verify correctness of direction of movement for flight control surfaces Select Deflection Test option and avoid touch the yoke during the test Follow the instructions on the screen Page 29 Autopilot Section TLELEKTRONIC External Button This option enables extension of the ways for activation and deactivation of the AP Moreover it simplifies the setting of Altitude bug and Heading bug and makes setting of bugs more comfortable Of course external button with appropriate and handy position is needed Recommended place for external button is on yoke control column or on central panel e Menu External Button e Autopilot Activation Deact Only e Autopilot Activation Prev Act amp Deact e Autopilot Activation Stab Act amp Deact e Hold On Function Enable e Hold On Function Disable Page 30 Autopilot Section External Button option of Menu External Button action of the button note Before any deactivation temporary or permanent of the AP performed b
13. itch If you have Integra connected directly to battery power choose NOT CONNECTED in this menu Page 18 EFIS Setup Menu External Devices TLELEKTRONIC EFIS EXTERNAL DEVICES You can add any external device such as GPS SL30 nav com Remote Compass and CO Guardian e Menu EXTERNAL DEVICES GPS e 5130 nav com External devices e Remote compass e CO Guardian GPS Port COM1 Baud rate 19200 Protocol NMEA SL30 Port COM2 Remote compass Connected CO Guardian Not connected Page 19 EFIS Setup Menu unam GPS amp SL30 nav com GPS In this menu you can set access point baud rate and protocol First you can choose between COMI or COM2 Now you can set baud rate from 4800 to 115200 And now you can choose protocol between NMEA and ARNAV e Menu GPS Not connected Com 1 Com 2 Baud 115200 Baud 57600 Baud 38400 Baud 19200 Baud 9600 Baud 4800 Protocol NMEA Protocol ARNAV NOTE If you select baud rate which is not supported by your GPS receiver baud rate 4800 will be automatically set SL30 nav com The SL30 is a VHF Navigation Communications Transceiver You can connect SL30 with INTEGRA via COMI or COM2 e Menu SL30 nav com e Not connected e Coml e Com2 Page 20 EFIS Setup Menu unam Remote Compass amp CO Guardian Remote compass TL elektronic Remote Compass is exclusive source of magnetic heading information for the Integra The connection to Integra is via CAN BUS e
14. kip previous menu Cancel Vno Maximum structural cruising speed or maximum speed for normal operations Vno speed Change the underlined by rotating the right Knob 315 kmh After you get required number just press the knob and the underscore skips on to the next number Press Set to enter the Cancel Position value Press Cancel to skip previous menu Page 12 EFIS Setup Menu Range and Limits Vfe Maximum flap extended speed Change the underlined by rotating the right Knob After you get required number just press the knob and the underscore skips on to the next number Press Set to enter the value Press Cancel to skip previous menu Position Vs Stall speed or minimum steady flight speed in which the aircraft is still controllable Change the underlined by rotating the right Knob After you get required number just press the knob and the underscore skips on to the next number Press Set to enter the Cancel value Press Cancel to skip previous menu Page 13 EFIS Setup Menu Range and Limits Vso Minimum flight speed in landing configuration Change the underlined by rotating the right Knob After you get required number just press the knob and the underscore skips on to the next number Press Set to enter the value Press Cancel to skip previous menu Cancel Page 14 Setup Menu TLELEKTRONIC Other Setting amp Calibration EFIS OTHER SETTINGS
15. ment that you ve select Save Setting option NOTE Running of Demo Mode is indicated by changing of color of the Integra buttons sequence red orange green and red displayed message Demo Mode Page 25 Autopilot Section Introduction Autopilot optional function Page 26 Autopilot Section TL ELEKTRONIC Introduction The Integra Autopilot referenced below as the AP offers roll aileron pitch elevator and yaw rudder axis control The number of axes which can be controlled by AP is depending on your purchased Activation Key as well as variety of navigation abilities of AP See Price list for available AP Activation keys and their features Available features of the Integra Autopilot includes control of the aircraft axes with the aid of Altitude and Heading Bug or dynamic control supported by VOR or GPS comfortable Autopilot setting via your chosen external button settings of Autopilot servos including sensitivity setting slip setting adjustment of monitored limits as maximum bank angle turn rate control maximum climb descent speed etc Access to Autopilot Setup Select option Autopilot Setup in Menu EFIS Setup e Menu Autopilot Setup Servo Setup Servo Deflection Calibration External Button Roll Axis Setup Pitch Axis Setup Enter Activation Enter Reactivation On following pages you ll find description of each option listed above of menu Autopilot Setup Page 27 Autopilot Section TL ELEKTRONIC
16. ress Cancel to skip previous menu Page 16 EFIS Setup Menu Configuration amp Sensors TLELEKTRONIC Pitch Setting If the INTEGRA is not mounted at a right angle in relation to the pitch of the aircraft this function can be used to compensate for this variation 7 WARNING If you are unfamiliar with pitch calibration please obtain qualified assistance An incorrect calibration of horizon may result in death or serious injury Backlight Control This menu has 2 submenus Dimmer Source Control and Button Color e Dimmer Source Control Button Color Manual You can set brightness manually e Green You can set green backlighting e External You can set external dimmer Red You can set red backlighting Max5V Orange You can set orange backlighting e Max 12V Max 24V e Auto You can set brightness automatically Page 17 EFIS Setup Menu Configuration amp Sensors AUX INPUT OUTPUT This menu contains other external inputs and outputs In every menu you can choose if you want to NOT CONNECT or YES HI or YES LO CNPY Canopy status open close These sensors can be only TENE NOT CONNECTED Gear UP Undercarriage is retracted CI m ae Gear DOWN Undercarriage is extended Main Switch Control e Menu Main Switch Control e Not Connected Connected If you have Integra connected via external main switch set in this menu CONNECTED So you can power on or power off integra via main sw
17. s subject to change without prior notice Page 1 Introduction unam Table of Contents Table of Contents TABLE OF CONTENTS PR 2 RECORD REVISION cC 4 A ME 6 A 8 EFIS CONFIGURATION amp OEIL 6T Hcc 10 INN INIA sssussuccbasca cass ousbiseeeeeessbecvs vacesesusactascsceevassssesuesuessceuccsuceusesecassesabesousseusucbaesacesesseseasbecossesssevusensesses 11 EFIS OTHER SETTINGS amp 15 AIRCRAFT IDENTIFICATION ia A cde c a a i awa a ee 15 RUE 16 DATE esse aie sala ete bess a i alo o ta la eae a a a ae Abe as is 16 PITCH ERR e 17 BACKLIGHT CONTROL eric ala d p OO Kee a is 17 AUX INPUTOUTPU KEE 18 PAD else E E
18. so available in Integra Demo PC application which you could obtain from TL elektronic web site After you ll start up Demo Mode by selecting Demo On the Integra will be reading input data of sensors from loop in internal memory After time of loop is up loop will be automatically start up again e Menu Demo Mode Demo ON Demo OFF Integra Type Reset Time Save Setting Demo ON Demo OFF These two options switch between on state and off state of Demo Mode Integra Type In this submenu you can choose simulated Integra unit of specific version Options are EMS refers to TL 6724 EFIS refers to TL 6524 EFIS EMS refers to TL 6624 and Remote Display refers to TL 6824 Page 24 EFIS Setup Menu unam Demo Mode NOTE To exit the Remote Display Demo Mode you ll have to press right knob and then immediately left knob This is only way because Menu Enter Setup isn t available for TL 6824 Remote Display Reset Time This submenu serves for setting reset time of loop Range is from 30 seconds to 10 minutes Save Setting If you select Save Setting complete settings of the Integra will be saved That includes the settings in standard screens e g set of Towing Menu Highway Baro Pressure Nav Source and in Setup Mode sensors setting units etc After count down of Reset Time reaches zero all settings that you ve made after the Save Setting option selection will be lost In other words settings will revert to state in mo
19. tion of Remote Compass Build In according to its placing in the aircraft Ur 0 Page 21 EFIS Setup Menu unam Remote Compass amp CO Guardian AN CAUTION Is requiring setting magnetic inclination angle and intensity Menu Calibration In this menu you can calibrate your Remote Compass Orient your plane in a known direction preferably on a compass rose at the airport Turn aircraft to the north direction Stabilize the aircraft at horizontal position and keep the aircraft in this position during all calibration Press OK Integra start with calibration Turn aircraft in agreement with instruction on Integra You will turn aircraft to the west south and east After calibration will be displayed information about status of calibration There can be some mistake during calibration Integra show you error message with error description CO Guardian You can connect and disconnect the external CO Guardian device on port COM lor COM 2 CO guardian monitors the quantity of CO in the cockpit If the quantity of CO exceeds the safety limit the e Menu CO Guardian INTEGRA will show you an alert message e Not connected Coml e Com2 Page 22 EFIS Setup Menu unam EFIS Data Sharing EFIS Data Sharing If you have multiple TL elektronic products in your aircraft they can be networked together via the TL elektronic iFamily amp CanBUS Units networked via iFamily 9 have the ability to share information with each other Any prod
20. tions of one switch metaphorically told That means that you can choose Mode Vertical Speed or Mode Longitudinal Angle Mode Vertical Speed If you select this mode the AP will control the aircraft according to parameters Max Climb Speed and Max Descent Speed both described below Page 34 Autopilot Section TL ELEKTRONIC Pitch Axis Setup Mode Longitudinal Angle If you select this mode the AP will control the aircraft according to parameter Max Longitudinal Angle described below Max Longitudinal Angle The parameter determines angle between longitudinal axis of the aircraft in horizontal flight and longitudinal axis of the aircraft when the AP pitches the aircraft up or down during controlled altitude change If Mode Longitudinal Angle is set parameter Max Longitudinal Angle is activated Max Climb Speed Max Descent Speed If Mode Vertical Speed is selected Max Climb Speed and Max Descent Speed will be used for reduction of Vertical Speed during climb or descent of the aircraft Min Air Speed Min Air Speed is minimum airspeed at which you can activated the AP If actual airspeed is lower than set Min Air Speed the AP will pitch the aircraft down to increase actual airspeed If aircraft s altitude is lower than altitude determined by Altitude Bug or Navigation source VOR or GPS and the AP can t pitch the aircraft up without dropping below Min Air Speed the Integra will display message ADD POWER
21. uct s data can then be viewed on any other screen in the iFamily network For example an EFIS has the ability to display engine monitor information if it is connected to an EMS TL 6724 The iFamily systems allows you to connect autopilot servos and remote compass NOTE See Integra iFamily Connection part and Explanation of Possible Connections in User Manual for more information e Menu EFIS Data Sharing 9 Off e Low Priority e High Priority Off The Integra doesn t send EFIS data to bus The Integra is not source of EFIS data for other Integra units connected to bus The Integra only receives EFIS data from bus Low Priority The Integra is set as data source with low priority for EFIS data shared by bus High Priority The Integra is set as data source with high priority for EFIS data shared by bus Page 23 EFIS Setup Menu unam Language and Demo Mode Language You can switch between languages the Integra will display button labels menus prompts etc in selected language Options are English Czech German French Russian Demo Mode O NOTE Run of Demo Mode during flight is strictly prohibited because the Integra isn t displaying actual flight parameters but values from internal memory loop This option provides opportunity for trying out features of other versions of the Integra TL 6524 EFIS TL 6724 EMS TL 6824 Remote Display Of course the opportunity for trying out features of other versions is al
22. vation Key e g Premium Activation Key to Gold Activation Key just select Enter Reactivation and enter your new Activation Key Page 36 2010 TL elektronic or its subsidiaries TLELEKTRONIC Europe United States of America Part Number TLD 6524X DS 001_RevE
23. y the external button the AP has to be activated by the AP buttons on the Integra at first press holding down press and immediate release Hold On Function Enable Deact The AP is deactivated Activation of the AP must The AP is temporarily deactivated After release of the button Only is set performed by the AP buttons on the Integra the AP will follow the last configuration Prev Act The AP is activated with the last configuration The AP is temporarily deactivated After release of the button amp Deact Next pressing will deactivate the AP the AP will follow the last configuration is set Stab Act The AP is activated and the AP will hold current The AP is temporarily deactivated After release of the button amp Deact altitude and heading the AP will hold current altitude and heading is set Hold On Function Disable Deact The AP is deactivated Activation of the AP must no reaction Only is set performed by the Integra buttons Prev Act The AP is activated with the last configuration no reaction amp Deact Next pressing will deactivate the AP is set Stab Act The AP is activated and AP will hold current reaction amp Deact altitude and heading is set Page 31 Autopilot Section TL ELEKTRONIC Roll Axis Setup Roll Axis Setup This submenu provides settings of the AP performance during a roll of the aircraft e Menu Roll Axis Setup
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