Configuration Manual
Contents
1. be 59 EMS EX TERNAL DEVICES ot Vasa io ue aaa eeu ve va e ce Vae 60 UNES 60 EMS DATA SHARING rcs 61 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 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 a2. mBar ROTOR RPM Rotor RPM rpm Oil Pressure Dil Press Oil Temperature Oil Temp Water CHT Temperature Water CHT C Water Aux Temperature Water Aux Left Total tank Left Total tank gal Right tank Right tank gal e Fuel pressure Fuel Press bar Fuel flow Fuel flow e e CHT CHT C Voltage 1 Voltage 1 V e sent Current 1 Voltage 2 Voltage V Current Current 2 A e Voltage V Voltage 3 Current 3 Range and Limits for Water Temperature and CHT are same This CHT refers to temperature measured on engine block ROTAX meaning of the word CHT Current refers to temperatures measured by thermocouples under spark candles Page 46 EMS Setup Menu TLELEKTRONIC Range and Limits NOTE The limits of one each values can t overlap each other If you try decrease for example ALARM and it is impossible so you need to decrease WARN at first and than you can set ALARM to lower value Available Limits Configuration Table You can set Indicator Range Min Alarm Min Warn Norm Warn Alarm RPM X X X X MAP X X X Rotor RPM X X X X X Oil Pressure X X X X X Oil Temperature X X X X X X Water CHT Temperature X X X X Water Aux Temperature X X X X Left tank Total Tank X X Page 47 EMS Setup Menu Range and Limits
3. ute ete ne teen a 35 EIMSiSEPUBRLMENU 36 ra edes doc eda lesa deett ra Ee ESE Ea 37 EMS CONFIGURATION amp SENSORS 5 2 2 3 5 5 3 3 uio e redeo rh eaae sa e ole oo e Da ERo deua eda esca boat bene aede Ee pa bros se eet ol eae eene eta 39 EMS RANGE AND Us aE E EEOAE IS SE aS ass a eons 46 Available Config r ation Nr 47 EMS OTHER SETTING amp CALIBRATION cacsscscccsecscsvscscovsncsccosccsccscvssssecsecesssccsescscccsccsecccsccsscssccessscocnasscscascsessossesssssecessccossasacsesseseccoscesecssenssescosuavasssees 52 Aeran identification zinc been eec be ole EN AEBS ESRB EAL ARE EBB AE REE AaB 52 d Er 52 EE 52 jore iri COM M 52 52 UG PIO AE EEEE AAE E E EEEE EE E ET E A E EE 53 Fuel pressure set Zerova a Sort A cmd 54 Water GHT Temperature Label iecit tates a a ife PY eee ca es ict ey ea o cx eret oy Ree eee nionem 59 a tipi ed ie ea cete e
4. Introduction unam Table of Contents Table of Contents TABLE 9 0 M OM EeePC 2 INDGUHUEOUHOMNJLOE HMM 4 EFIS SETUP ELO EU n 6 10 ui X D M o OA 8 EFIS CONFIGURATION amp 5 5 10 EFIS RANGE AND LIMULUS REEL 10 EFIS OTHER SETTINGS amp CALIBRATION sssssssssssosssosssssssosososososososososososososososososososososososososososososososososososososososososososososososososssosososososososssosssosososs 14 Cal ON REDE E A O E EET esas 14 15 15 PMT SUS at 16 Backlisht Control 16 AUX INPUT OTP 17 17 EFIS EXTERNAL DEVICES wccccscssicccccssccscncsctecsscsuesdsccsebececusvenccnassessescdvosccseseietacedvescanesscseascdseabenadecesacedseasacndcscescedseaccssdeiebacsSueudavescces
5. Voltage 3 Current 1 Current 2 Current 3 used 4x 6624 39 6624 39 BATTERY used PUMP used AVIONICS used BATTERY used PUMP used AVIONICS used Current 1 label Page 44 The underlined letter you can change by rotating right knob If you get the required letter just press the knob and the underscore will skip on to the next letter Press Set to accept the new label Press Cancel to skip to previous menu Press Default to reset to default label For Current 1 is default label BATTERY for Current 2 PUMP for Current 3 AVIONICS 5 Configuration amp Sensors EGT CHT setting You can choose and assign Thermocouple and Sensors to EGT and CHT In this menu choose one EGT or one of CHT Press the knob and discovers next menu Now select Input In this menu select desired thermocouple Now selected EGT or CHT is associated with this thermocouple You can do it the same way for every EGT and CHT Thermocouple 1 Sensor Type 6624 03 Type K CHT described here means Cylinder Head Temperature measured by thermocouples under spark plugs not in meaning used by ROTAX Page 45 EMS Setup Menu TLELEKTRONIC Range and Limits EMS RANGE AND LIMITS In this menu you can set minimum and maximum critical values minimum and maximum warning values and normal values e Menu RANGE AND LIMITS RPM RPM rpm MAP
6. Available Limits Configuration Table You can set Indicator Range Min Alarm Min Warn Norm Warn Alarm Right tank X X Fuel pressure X X X X X Fuel flow X X EGT X X X CHT X X X Voltage 1 X X X X X Current 1 X X X X X Voltage 2 X X X X X Current 2 X X X X X Voltage 3 X X X X X Current 3 X X X X X Page 48 EMS Setup Menu Range and Limits Example of differences between set values Default values are defined RANGE ME MIN WARN NORM WARN E 3000 500 2700 2800 New values are defined RANGE ME MIN WARN NORM WARN E 5000 1000 3000 4000 Page 49 EMS Setup Menu Range and Limits Indicator Function Recommendation Warning Oil Pressure Warning Limit Useful as a reminder to reduce RPM when warming a cold engine especially in winter conditions to avoid excessive oil pressure As recommended by engine manufacturer Alarm Minimum Oil Pressure Minimum Oil Pressure This Warns of loss of oil pressure This is serious Consider you situation carefully This may lead to complete engine seizure or it may only be instrument or sensor failure It requires immediate action but not over reaction As recommended by engine manufacturer Oil Temperature Warning Yellow indicator As recommended by engine manufacturer Maximum Oil Temp Consider setting this limit lower than the maximum to get early war
7. UK e Imperial US Custom Metric Imperial UK Imperial US Custom e Menu Custom Airspeed Altitude Distance VSI Baro pressure INTEGRA display units in metric system km h m INTEGRA display units in metric and imperial system kts ft INTEGRA display units in imperial system kts ft you can choose individual units for each measure 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 mBar km mBar nm inHg nm m s ft min ft min EFIS Setup Menu Units Available units for measured quantities q 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 C amp S and R amp L EFIS Configuration amp Sensors This menu contains settings for sensors of temperature e Menu Configuration amp Sensors AT OAT 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 No
8. 10 Page 31 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 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 32 Autopilot Section TL ELEKTRONIC Pitch Axis
9. Configuration amp Sensors Range and Limits Other Setting amp Calibration External Devices EMS Data Sharing Autopilot Setup Language Demo Mode Exit Menu EMS UNITS You can choose between metric and imperial units or you can define your own unit settings e Menu UNITS Metric e Imperial UK e Imperial US Custom Metric INTEGRA display units in metric system Bar C Pa litre Imperial US INTEGRA display units in metric and imperial system Bar C Pa gallons Imperial UK INTEGRA display units in imperial system inHg F psi gallons Custom you can choose individual units for each measure Page 37 EMS Setup Menu Units e Menu Custom e MAN pressure e Temperature e Pressure e Quantity Available units for measured quantities Quantities Selectable Units Indicator press of oil bar psi Indicator oil temperature Celsius Fahrenheit Internal air temperature Celsius Fahrenheit Outsider air temperature Celsius Fahrenheit Temperature of cylinders Celsius Fahrenheit Information about fuel fuel pressure bar kg cm2 psi Consumption fuel flow and fuel quantity Litre GAL Manifold air pressure mBar torr inHg Page 38 5 Configuration amp Sensors EMS CONFIGURATION amp SENSORS In this menu you can properly set all connected sensors Menu CONFIGURATIONS amp SENSORS e RPM MAP Rotor RPM Oil pressure Oil Te
10. a maximum limit or based on experience Warning Cylinder Head Temperature Often engines will T Set according to engine CHT Warning normally operate significantly lower than the engine cite manufacturer s recommendation manufacturer s limit CHT AI Consider setting this limit lower than the maximum to get early Set according to engine warning of abnormal CHTs manufacturer s recommendation Page 51 EMS Setup Menu Other Setting amp Calibration EMS OTHER SETTING amp CALIBRATION e Menu OTHER SETTING amp CALIBRATION e Aircraft Identification e Time e Date Backlight Control AUX Input Output e Fuel Flow Fuel Press set zero pressure e Fuel Calibration e Set Unexhaustible Fuel e RPM Setting e Rotor RPM Setting Engine Time Threshold Water CHT Temperature Label Main Switch Control Aircraft identification Itis the same as in EFIS Time Itis the same as in EFIS Date Itis the same as in EFIS Backlight Control It is the same as in EFIS AUX INPUT OUTPUT It is the same as in EFIS Page 52 EMS Setup Menu Fuel Flow Fuel flow You can set K factor and Time of aver flow e Menu Fuel flow K factor You can manually adjust the K Factor The K Factor is a measurement of the pulses e K Factor per gallon that the flow transducer outputs Due to variations in the installation of the e Time of Average Flow flow transducer it may be necess
11. 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 23 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 moment 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 24 Autopilot Section Introduction AUTOPILOT OPTIONAL FUNCTION Page 25 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 w
12. 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 reaction Only is set be 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 the AP will hold current no reaction amp Deact altitude and heading is set Page 30 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 e Control Sensitivity Mode Turn Rate Mode Bank Angle e Max Bank Angle e 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
13. want to continue and two labels are displayed YES or NO If you press YES a list will be shown with possible sensors choices Page 40 5 Configuration amp Sensors Fuel Pressure This sensor monitors fuel pressure Fuel flow This sensor monitors Fuel Flow EGT CHT Number You can set the Cylinder Number to 2 4 or 6 IAT This sensor monitors internal air temperature OAT This sensor monitors outside air temperature Page 41 5 Configuration amp Sensors VoltageX Yes Select when Voltage 1 2 Menu Voltage or 3 is used Voltagel Yes Voltagel No VoltageX No ae e um Voltagel Label Select when Voltage 1 2 Voltage gauge voltage monitoring m ms i d Menu for Voltage is the same DUREE as for Current Voltage2 Label VoltageX Yes Voltage3 Yes Select when you want to e Voltage3 No set label of Voltage 1 2 or Voltage3 Label 3 See next page for description CurrentX Yes Menu Current Select when Current 1 2 Currentl Yes or 3 is used C tl N You can choose where battery patio p CurrentX pump avionics etc you want urn yos Select when Current 1 2 gauge current monitoring or 3 is not used Current Current2 No Menu for Current is the same as for Voltage Current2 Label Current3 Yes Current3 No Current3 Lab
14. HT measured by thermocouples under spark plug Main Switch Control It is the same as in EFIS Page 59 EMS Setup Menu External Devices TLELEKTRONIC EMS EXTERNAL DEVICES External devices are devices which you can connect on port COMI or 2 e Menu EXTERNAL DEVICES Guardian External devices CO Guardian Not connected 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 quantity of CO exceeds the preset safe limit the INTEGRA will show you an alert message Page 60 EMS Setup Menu TLELEKTRONIC EMS Data Sharing EMS 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 have the ability to share information with each other Any product 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 EMS Data Sharing 9 Off Low Priority e High Priority Off The Integra doesn t send EMS data to bus The Integra is not source of EMS data
15. If this function is not used then preset reduction ratio to 1 00 Page 57 EMS Setup Menu Rotor RPM amp Engine Time Threshold Rotor RPM settingYou can set number of pulses Menu Rotor RPM setting e Pulses Per Rev Engine time Threshold The underlined number you can change by rotating the right knob If you get the required number just press the knob and the underscore will skip on to the next number Press Set to enter the new value Press Cancel to skip previous menu The underlined number you can change by rotating the right knob If you get the required number just press the knob and the underscore will skip on to the next number Press Set to enter the new value Press Cancel to skip previous menu Page 58 Eng active RPM 300 fem Cancel Set Position EMS Setup Menu Water Temp and Main Switch TLELEKTRONIC Water CHT Temperature Label You can choose whether you want to display WATER TEMPERATURE and or Cylinder Head Temperature ROTAX meaning of the word e Menu Water CHT Temperature Label e WATER e CHT Water Temperature and CHT depiction as it is Water Temperature and CHT depiction as it is displayed on EMS screen when Towing Menu is OFF displayed on EMS screen when Towing Menu is ON The CHT described here represents value measured on engine block with resistance sensor That s the meaning of CHT used by ROTAX Don t confuse this CHT with C
16. M die ele INTEGRA EFIS amp EMS TL 6624 CONFIGURATION MANUAL Non TSO approved TL elektronic Airport Building 125 503 41 Hradec Kralove Czech Republic Copyright 2008 2010 TL elektronic 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 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 information in this User s manual is subject to change without prior notice Page 1
17. Setup Pitch Axis Setup This submenu provides settings of the AP performance during controlled change of altitude e Menu Pitch Axis Setup Control Sensitivity 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 options 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 33 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 betw
18. Source Control e Button Color Manual You can set brightness manually Green You can set green backlighting e External You can set external dimmer e Red You can set red backlighting e Max 5V e Orange You can set orange backlighting e Max 12V e Max 24 e Auto You can set brightness automatically Page 16 EFIS Setup Menu Other Settings amp Calibration TLELEKTRONIC 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 Gear UP Undercarriage is retracted Gear DOWN Undercarriage is extended Main Switch Control 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 switch If you have Integra connected directly to battery power e Menu Main Switch Control choose NOT CONNECTED in this menu e Not Connected Connected Page 17 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 e GPS SL30 nav com External devices Remote compass e CO Guardian GPS Port COM1 Baud rate 19200 Protocol NMEA SL30 Port COM2 Remote compass Connected CO Guardian Not connected Page 18 EFIS Setup Menu unam GPS amp SL30 nav com GPS In th
19. acedueddencdscesacedscacendesss 18 Gllc n 19 RESISTIT TULIP 19 Remote 9 1016 Se 20 CO Guardia t AL m 21 EFIS DATA SHARING oioesicesertssisseeosssiseeessssseeesessseses sasori obesas rosor ooe a e bE SS E ESS roO rr DCSE eooo USSR Uo 22 E N E E EE E AREE OOE E EEA EE EA 23 Introduction TLELEKTRONIC Table of Contents DEMO MODE v o oS Osb Stos b ba So Saros 23 AUTOPILOT OPTIONAL EUNCTIQONN eere tho eo earn o sao erae een suona oe ee eoo nei Uo noon orae pe oi tora on te Reese e ea soon anges 25 Servo Se ond us i dit ttd tete 27 Servo Deflection Calibration eee res a ree tet sane el eT 28 External Button eee MEE lu eter Ee PD M Ee ta mc bi 29 ud c vp adea 31 Pitch viri 33 Enter Activation Enter ReactIVation
20. 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 in the cockpit If the quantity of exceeds the safety limit the e Menu CO Guardian INTEGRA will show you an alert message Not connected Coml Com2 Page 21 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 product 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 and explanation e Menu EFIS Data Sharing e Off Low Priority High Priority Off The Integra doesn t send EFIS data to bus The Integra is not source of EFIS data for other I
21. alue 742 Sensors Press Set to store new value Page 54 EMS Setup Menu Fuel Calibration Fuel calibration e Menu Fuel calibration e Left tank Right tank Right tank is enable Or e Total tank Right tank is disable Because the shape of the tank can be asymmetric therefore petrol in fuel tanks may not be level You can set up to 15 steps of fuel calibration First you choose left or right tank for calibration and press the knob Now is displayed label and you can choose number of steps merely rotate the knob When you have set number of steps press You can cancel this operation if you press the Cancel button NOTE You can set count of calibration steps in range from 3 to 15 NOTE If you want to change the capacity of the tank Enter to Setup Range and Limits Left Total Tank and set the RANGE Left tank calibration If you press button the next label with Start calibration is displayed Be sure before starting the calibration that your fuel tank is full Page 55 Left tank calibration Total tank capacity 500 I Select count of calibration steps 7 Cancel Edit value Total tank capacity 50 0 Start calibration TLELEKTRONIC Set Unexhaustible Fuel A CAUTION The INTEGRA must be calibrated to the aircraft fuel system and the INTEGRA s accuracy must be verifie
22. ary to adjust the K Factor for the first few flights in order to get an accurate fuel remaining fuel used and flow reading The K Factor should be changed only when the fuel tanks have been filled accurately on level ground After a few adjustments of the K Factor the K factor fuel remaining and the fuel used as calculated 884p by the INTEGRA should be within a few gallons or less of actual and should not need further adjustment Use the following fields as necessary to correct the K Factor The underlined numbers you can change by rotating the right knob If you get the required number just press the knob and the underscore will skip on to the next number Press Set to enter the new value Press Cancel to skip previous menu Position Shown value Real value x Last K FACTOR K FACTOR Last K FACTOR Real value Page 53 EMS Setup Menu TLELEKTRONIC Fuel Pressure Time of Average Flow You can set time duration for how long T you want average flow of fuel After this 24 time the INTEGRA will show you average fuel flow The numbers of seconds you can change just rotate with the right knob If you get required number just press Set Press Cancel to skip previous menu Position NOTE Maximum displaying time which you can set 15 10 seconds Fuel press zero calibration Fuel pressure set zero This is function for correction of variance between Offset v
23. avoid touch the yoke during the test Follow the instructions on the screen Page 28 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 Autopilot Activation Deact Only Autopilot Activation Prev Act amp Deact Autopilot Activation Stab Act amp Deact Hold On Function Enable Hold On Function Disable Page 29 Autopilot Section External Button option of Menu External Button action of the button note Before any deactivation temporary or permanent of the AP performed by 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 be 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 15 temporarily deactivated After release of the button amp Deact Next pressing will
24. be set to at most 9596 of Vne This is default setting of Max Air Speed value Page 34 Autopilot Section TL ELEKTRONIC Pitch 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 10 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 Activation Key e g Premium Activation Key to Gold Activation Key just select Enter Reactivation and enter your new Activation Key Page 35 EMS Setup Menu Introduction EMS Setup Menu Page 36 EMS Setup Menu TLELEKTRONIC Units 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 EMS You should see Menu EMS Setup In this menu you can set up many parameters mainly for engine and sensor settings Menu EMS Setup Units
25. d before flying the aircraft The accuracy and proper operation of each function displayed on the INTEGRA should be verified before the aircraft is released for flight Set unexhaustible fuel Your fuel tank may contain fuel that cannot be consumed In this step you may set the quantity of Left unexh fuel e Menu Set Unexhaustible Fuel this fuel Left tank In first step you choose left or right tank Now the Right tank underlined number you can change just rotate with Cancel Postion Right tank is enable the right knob If you get the required number just press the knob and the underscore will skip on to Or the next number Press Set to enter the new value Repeat the same procedure for the second tank Total tank Right tank is disable Page 56 EMS Setup Menu RPM Setting RPM setting You can set number of pulses per rev and you can set reduction ratio RPM pls rev Menu RPM setting In both cases the underlined number you can change by 4 e Pulses Per Rev e Reduction ratio NOTE rotating the right knob If you get the required number just press the knob and the underscore will skip on to Cancel Set Position the next number Press Set to enter the new value Press Cancel to skip previous menu If you are unable to install a sensor directly on your engine and the location of your sensor is affected by a reduction ratio It is then necessary to enter the correct reduction ratio
26. een 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 The Min Air Speed must be set to at least 3096 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 15 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
27. el CurrentX Yes Select when you want to set label of Current 1 2 or 3 See page 44 for description Page 42 5 Configuration amp Sensors RPM MAP Rotor RPM Oil press Dil temp Water CHT Water Aux Left tank Right tank Fuel press Setting Voltage label Sensors used Fuel flow 6624 33 EGT CHT not used IAT 6624 40 DAT 6624 05 Voltage 1 6624 05 Voltage 2 6624 17 Voltage 3 6624 21 Current 1 6624 22 Current 2 6624 37 Current 3 used 4x 6624 39 6624 39 BATTERY used PUMP used AVIONICS used BATTERY used PUMP used AVIONICS used Voltage 1 label Page 43 The underlined letter you can change by rotating right knob If you get the required letter just press the knob and the underscore will skip on to the next letter Press Set to accept the new label Press Cancel to skip to previous menu Press Default to reset to default label For Voltage 1 is default label BATTERY for Voltage 2 PUMP for Voltage 3 AVIONICS 5 Configuration amp Sensors RPM MAP Rotor RPM Oil press Dil temp Water CHT Water Aux Left tank Right tank Fuel press Setting Current label used 6624 33 not used 6624 40 6624 05 6624 05 6624 17 6624 21 6624 22 6624 37 Sensors Fuel flow EGT CHT IAT DAT Voltage 1 Voltage 2
28. ell 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 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 26 Autopilot Section TL ELEKTRONIC 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 Slip e Servo Pitch o Installed YES o Installed NO Slip e Servo Yaw o Installed YES o Installed NO 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 Y
29. erscore will skip on to the next letter Then press Set to enter the new value Press Cancel to skip previous menu Page 14 EFIS Setup Menu Other Settings 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 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 Press Cancel to skip previous menu Page 15 EFIS Setup Menu Other Settings amp Calibration 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 Dimmer
30. for other Integra units connected to bus The Integra only receives EMS data from bus Low Priority The Integra is set as data source with low priority for EMS data shared by bus High Priority The Integra is set as data source with high priority for EMS data shared by bus Autopilot Setup See separated Autopilot Section on page 25 Page 61 62 63 Page 64 2010 TL elektronic or its subsidiaries TLELEKTRONIC Europe United States of America Part Number TLD 6624X DS 001_RevE
31. is menu you can set access point baud rate and protocol First you can choose between COMI or 2 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 Not connected e Coml e Com2 Page 19 EFIS Setup Menu unam Remote Compass 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 Menu Remote compass Not connected Connected e Settings e Declination Inclination Total Mag Field 350 000 010 Build In ME 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 220 298 240 Menu Settings To calibrate your Remote Compass you must input your location s current magnetic inclination ang
32. le 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 TOTAL FIELD in agreement with this website Set up in Integra position of Remote Compass Build In according to its placing in the aircraft Ur Js OO Page 20 EFIS Setup Menu unam Remote Compass amp CO Guardian A 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
33. lways 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 Introduction 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 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 EFIS UNITS You can choose between metric and imperial units or you can define your own unit settings e Menu UNITS e Metric e Imperial
34. mperature Water CHT Temperature Water Aux Temperature Left Total Tank Right Tank Fuel Pressure Fuel Flow EGT CHT number EGT CHT setting Voltage Current Page 39 5 Configuration amp Sensors In every menu you can choose if you want to CONNECT or NOT CONNECT a sensor and in some menus you will have a list of sensors in which to choose the appropriate sensor RPM This sensor monitors RPM MAP This sensor monitors manifold pressure Rotor RPM This sensor monitors Rotor RPM Oil Pressure This sensor monitors oil pressure Oil Temperature This sensor monitors oil temperature Water CHT Temperature This sensor monitors CHT Temperature in meaning used by ROTAX technically the sensor is placed on engine block To enable displaying of this info see section Other Setting amp Calibration Water CHT Temperature Label Water Aux Temperature This sensor monitors water temperature To enable displaying of this info see section Other Setting amp Calibration Water CHT Temperature Label Left Total tank This sensor monitors fuel level in left tank Right tank You can disconnect this tank so the left tank This sensor monitors fuel level in right tank will be the only one and the main tank A CAUTION After left or right tank is chosen a warning message is displayed After change sensor you have to recalibrate fuel tank do you
35. ning of abnormal oil temp As recommended by engine manufacturer Normal Oil Temperature Intended for troubleshooting Can also indicate reminder that the engine is not warm enough Set according to engine manufacturer s recommendation or set based on experience Set according to engine RPM Alarm Max Red Line Warns when the engine has reached maximum RPM manufacturer s recommendation RPM Warning Yellow Indicator Set Based on experience RPM Normal Green indicator manufacturer s recommendation Page 50 EMS Setup Menu Range and Limits Fuel Right and Left Tank Alarm Minimum Fuel Quantity Set for at least enough useable fuel to provide for 30 60 minutes of flight at cruise power Fuel Right and Left Tank range Indicates each tanks capacity Setting Fuel Tank Range requires Fuel Tank Calibration Generates a warning when the fuel flow rate of fuel burn exceeds this limit Useful for detecting badly leaking fuel lines Account for max fuel flow rate at Fuel Flow loose connections to fuel injectors etc Very useful safety feature full takeoff set max 10 20 for all engines but especially fuel injected engines Be sure to use above max rate it Set limit according to engine Maximum Exhaust Gas Temp Not all engines have published EGT Warning manufacturer recommendation limits nor do all engines require
36. ntegra 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 22 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 also 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
37. ou can choose just one of these options Installed YES or Installed NO That determines whether the appropriate servo is installed or not Page 27 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 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 calibration 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
38. ress 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 12 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 13 TLELEKTRONIC Other Settings amp Calibration EFIS OTHER SETTINGS amp CALIBRATION This menu allows you to modify settings and calibrations e Menu OTHER SETTINGS amp CALIBRATION Aircraft Identification Time Date Pitch Setting Backlight control AUX Input Output Main Switch Control Aircraft identification The Aircraft ID Box has Letters A Z numbers 0 9 blanks and symbol The ID can also be Aircraft ID AIRCRAFT The underlined letter you can change just rotate shortened to fewer than 8 digits with the right knob If you get required letter just Cancel Position press the knob and the und
39. t Connected EFIS RANGE and LIMITS In this menu you can set airspeed values Airspeed limits e Menu Range and Limits kts Airspeed e Vne never exceed Vne Never exceed 210 Vno maximum structural cruising Vno Maximum structural cruising 170 Vfe maximum flap extended Vfe Maximum flap extended 70 e Vs stall speed Vs Stall speed 50 Vso minimum flight speed in landing configuration Vso Min speed in landing config 30 NOTE The limits of one each Vne Vno Vfe Vs or Vso can t 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 10 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 skip previous menu Cancel Vno Maximum structural cruising speed or maximum speed for normal operations Change the underlined by rotating the right Knob After you get required number just press the knob and the underscore skips on to number Press Se t Enter the s value Press Cancel to skip previous menu Page 11 EFIS Setup Menu Range and Limits Vfe Maximum flaps extended speed Change the underlined by rotating the right Knob After you get required number just p
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