User`s manual - TL elektronic
Contents
1. 24 Information about Battery A i Ba i iadi i Oe ae ea ee 25 me Warning ds 26 INTEGRA Opera iii A A aa En a deea ai a ase 27 Description of complete EMS aiene dea nn AAEE ER EAEE EE E E ER 28 e Description of function EMS Mtm nenene aten e ar a An 30 Introduction TLELEKTRONIC Table of Contents Integra Mention stu essa St Get ee aac igen ld od le Da 32 Brightness tale apilar its 32 E E E A A EE E e Bea e E ai nec od de A a a a ela Oe ca 33 Statistics Tor BMS zi inae teet imo e HIR aIipetee aac eite ia 34 Configuration of Inte uc E aeia a 36 A A ci o ute LOS cod Do ts eft stato UT ud cadens 36 FTRLOWEr Otho O NS Xo Ao unc CE qM SO RS ACES Se Xo SN qr CRT eine red 37 e AADOUU seria DPCEU rre DECIDE rU 37 NIen uEntertamment teeth er eoe A E NUN TI cou ecc eade estt uie EERIE ET is ECR 38 ADDEFeVIAtlODS oes uci mamie videi Ete t Urso it n RT dos 44 Technical Parameters cach me ae Phor dante A AM m t p ECL MR Ma tA ME m t P ECL MEM Pat 46 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 C 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 Introduction2. 1 Highlight described menu option by rotating the knob 2 Press the knob When the manual says e g Press button Yes 1t means press the button with label Yes displayed on screen above the button Turning the INTEGRA ON Press the right hand knob to turn the Integra on and wait until the green backlight goes out NOTE The other knob and buttons are disabled when the INTEGRA is Shut Down Turning the INTEGRA OFF To turn off the INTEGRA and place it in Shut Down Mode 3 Press right knob 4 Select Power Off NOTE All settings and calibrations will be stored when the INTEGRA is Powered Off Page 17 Basic Operation TLELEKTRONIC The Integra Control Panel The INTEGRA Control Panel All INTEGRA instruments function with a common control panel with a user friendly interface of 4 buttons two knobs and a USB Data port O 9 9 09 0 INTEGRA Control Panel Knobs Control of all menus is really easy and simple The two knobs have two interfaces press and rotate These provide particular menu options on different pages and are used to e scroll through menus e adjust instrument parameters and settings Page 18 Basic Operation TL ELEKTRONIC The Integra Control Panel Buttons and Labels The Button and Knob Labels will appear as white on black writing in the default mode The Labels will be highlighted once the control panel is engaged by pressing a button or turning a knob The Prompt Lab
3. Warnings amp Cautions amp Notes WARNING WARNING CAUTION CAUTION CAUTION CAUTION CAUTION This product is not TSO approved as a flight instrument therefore the manufacturer will not be held responsible for any damage caused by its use The altitude calculated by the INTEGRA is geometric height above mean sea level and could vary significantly from altitude displayed by pressure altimeters in aircraft The 3D Terrain Map supplied with INTEGRA relies on GPS data this system is subject to changes which could affect the accuracy and performance of the INTEGRA s 3D Terrain map The electronic chart is an aid to navigation and is designed to facilitate the use of authorized government charts not replace them Land and water data is provided only as a general reference to your surroundings The positional accuracy of the land and water data is not of a precision suitable for use in navigation and it should not be used for navigation Only official government charts and notices contain all information needed for safe navigation and as always the user is responsible for their prudent use The Terrain feature is for supplemental awareness only The pilot crew is responsible for all terrain and obstacle avoidance using information not provided by the INTEGRA 3DTerrain feature Although the INTEGRA series are precision electronic Navigation AIDs NAVAID any NAVAID can be misused or misinterpreted and therefore beco
4. ROTOR RPM MAX Maximum rotor rotations per minute FUEL PRESS MIN Minimum fuel pressure FUEL PRESS MAX Maximum fuel pressure FUEL FLOW MIN Minimum fuel flow FUEL FLOW MAX Maximum fuel flow IAT MIN Minimum inside air temperature IAT MAX Maximum inside temperature OAT MIN Minimum outside air temperature OAT MAX Maximum outside air temperature EGT1 MAX Maximum exhaust temperature of cylinder 1 EGT2 MAX Maximum exhaust temperature of cylinder 2 EGT3 MAX Maximum exhaust temperature of cylinder 3 EGT4 MAX Maximum exhaust temperature of cylinder 4 CHT1 MAX Maximum temperature on cylinder 1 measured by thermocouple under spark plug CHT2 MAX Maximum temperature on cylinder 2 measured by thermocouple under spark plug CHT3 MAX Maximum temperature on cylinder 3 measured by thermocouple under spark plug CHT4 MAX Maximum temperature on cylinder 4 measured by thermocouple under spark plug Page 34 O Men TLELEKTRONIC Statistics for EMS IAT MAX 20 C If Statistics are displayed the basic menu is changed DAT MAX 17 T o CHT4 MAX 282 C E i iue is closed CHT2 MAX 275 C you can erase statistic values SS ee If you press Delete values INTEGRA ask you if Are you sure you want to delete statistic If you press Yes the statistic will be delete If you press No the statistic will be con
5. Page 22 Basic Operation SD card Installation SD card Installation Turn off INTEGRA Remove INTEGRA from mounting rack The slot for the SD card is situated on the top right side of INTEGRA Now insert SD card into the slot so that the front SD card label is facing you Carefully press the card down until you feel it click The SD is now installed in the INTEGRA If you want to remove the SD card first carefully press down and the card will eject You can then safely remove the card from the INTEGRA Page 23 Slot for SD card Basic Operation Brightness praises TLELEKTRONIC This controls the brightness of the LCD Press right knob and select Brightness Rotate the knob to choose the level of brightness Brightness The green strip specifies level of brightness This function is possible only if you have DIMMER SOURCE CONTROL Press right knob select Enter Setup When prompt Are you sure you want to enter to setup appears press button Yes Now the Integra is in Setup Mode Press right knob select Other Setting amp Calibration New menu will appear There select Backlight Control then select Dimmer Source Control Finally select Manual Now manual setting of display brightness is enabled Page 24 Basic Operation TLELEKTRONIC Information about Battery Information about Battery The INTEGRA utilizes a Lithium Polymer battery with the following characteristics
6. Log You can export your service log from the Integra to your flash disk Update Firmware 1 Create the TLE directory and then create the UPDATE directory inside the TLE on your flash drive So the path will be X tle update 2 Copy the file fwu tls to the UPDATE on your flashdrive 3 Put the flashdrive in the Integra and wait 10 seconds flashdrive is loading 4 MENU ENTER SETUP there will be displayed another label DATA PORT button just by USB port Press this button and choose UPDATE FIRMWARE 5 Integra will display Are you sure you want to update firmware Press yes There will be another warning message During operation do not power off instrument Press OK The display shows you Firmware update Please wait while download is finished while the firmware is loading Do not touch any button or knob while the firmware is loading The time for loading the firmware differs with every next firmware The firmware loading time varies from each software upgrade package A CAUTION Ensure sustaining voltage during updating if during updating fails the electric power supply the Integra can be damaged A CAUTION Keep the flash drive connected with the Integra during updating A CAUTION This data port is intended only to be used with a flash disk Do not try to connect it to another USB device Page 20 Basic Operation TLELEKTRONIC Battery Installation Battery Installation 7 WARNING Before
7. User s manual is subject to change without prior notice Page 1 Introduction unam Table of Contents Table of Contents Table of Contents PR mt 2 Record of COV i Sn M 4 Accessories and Packing b E mom 7 Mrersnrss i iari MEE EO comet 8 General description isnin rna 9 A ea ERRATE EE RE A EEE R AER A PA 10 E T tegraiFamily Menu coi e RR m 10 e Explanation of Possible C Ome Cini a ts 11 e Backup System Recommendati n mc p 12 Explanation or Priority setting for Data Sharing nio aou pee piis cinia od eats nadie eed aa 13 e The INTEGRA Glass Cockpit Instrument dad 14 A ee coos A E caplet eel Dek el OR eel ee eal noel Seneca cated 15 A o mc k 15 SNR e AA Um me 16 BASIC OPERATION soprano A X 17 E Operation AO ia 17 Turine the INTEGRA ON Dc 17 Tian the INTEGRA OFE ri A R A E E E EE A 17 The INTEGRA Control Pa di 18 In e o A 18 e Buttons al Labs ai eatoaeeest 19 Bo O ci Oia 19 B ttery Uns eA Ue Tren 21 e SDcard al EEAS ER EEO A EESE EEES EEE SEESE TESES Ubeauathatbeudaceusceeys 23 ie cis me E T E
8. experience and minimize INTEGRA information issues across a large number of installations Currently OEMs can customize access levels to the following settings on TL elektronic systems EMS SENSOR setup menu fuel calibration trim calibration flaps calibration GPS NAV setup menu screen configurations data logging and checklists data panels OEM distributors have the option of customizing some or all of these areas Please contact your aircraft s manufacturer if you have any questions about how your unit has been customized 7 WARNING TL elektronic Avionics products incorporate a variety of precise calibrated electronics Except for replacing the optional internal backup battery in INTEGRA based products per the installation guide our products do not contain any field user serviceable parts Units that have been found to have been taken apart may not be eligible for repair under warranty Additionally once a TL elektronic unit is opened up it will require calibration and verification at our factory before it can be considered airworthy Page 9 Introduction unam General Description 7 WARNING The INTEGRA is permanently supplied by the aircraft s power supply Therefore it is necessary to install a fuse to act as protection against a power surge This will protect against the risk of fire and resulting damage to the INTEGRA and or aircraft About this Guide This guide serves two purposes The first is to help you configure and
9. get acquainted with the INTEGRA s many functions The second is to give you quick access to vital information For detailed technical and installation information please refer to the INTEGRA Installation Guide In the electronic PDF version of this manual page and section references in the Table of Contents and elsewhere act as hyperlinks taking you to the relevant location in the manual The latest version of this manual may be downloaded from our website at www tl elektronic com Integra iFamily Connection The TL elektronic iFamily amp BUS If you have multiple TL elektronic products in your aircraft they can be networked together via the TL elektronic iFamily BUS 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 O NOTE That the failure of a unit in an iFamily 9 network may cause the loss of some or all data shared between units In the example below if the connected EMS TL 6724 were to fail the EFIS EMS would no longer be able to behave as an engine monitor Page 10 Introduction unam General Description Explanation of Possible Connections Here are a few Instrument connection Possibilities If you connect TL 6524
10. installing battery turn off INTEGRA e Remove INTEGRA from mounting rack e Unscrew the battery cover located on the right side of the unit e After screw out carefully take off a sheet metal cover e The cable is attached to a holder of the battery with the baling wire Cover this wire must be removed Screw Connector e The battery is intended to be used only with the INTEGRA The Battery has a one connector to link it to INTEGRA and two lugs which nicely lock it to the battery holder eae e Connect the cables located in the battery holder to the Back up battery The connector is notched so Lugs you cannot connect this cable incorrectly to the battery e Put the battery in to the INTEGRA battery holder so that the lugs fit into the round holes on the INTEGRA battery holder and the connector must be on the top You should obey this to prevent damage of the battery cabel caused by sharp edges of the battery holder Page 21 Basic Operation TLELEKTRONIC Battery Installation ANNANN VUUY u Cable for connecting INTEGRA with battery Before screwing the cover on make sure that the battery is not protruding and is properly placed in the INTEGRA battery holder Then screw battery cover back on to INTEGRA 7 WARNING To not apply pressure to the battery while re installing the cover Correct battery installation in Integra Incorrect battery installation in Integra ine Integra holder dii
11. to move up to the parent directory choose item and press left knob For replaying desired video file just choose appropriate item and press left knob The Integra should be replaying your video now For maximizing video presentation to full screen press button Maximize For returning to previous screen press any button NOTE The Integra only supports 3gp video format Other files video of different format or any other data aren t displayed in Select video file window Page 40 Entertainment Operation elapsed time of video remaining time of video Music Flight Data Exit buttons labels Open n Play ry Stop I7 Prev M Next Opens window for Plays currently Stops currently Plays previous Plays next selecting desired stopped video played video track track video file or folder Page 41 Entertainment Operation Option Music O NOTE The Integra only supports MP3 audio files elapsed time of track name of currently played track remaining time of track loop playing mode Flight Data Exit shuffle playing mode number of currently played track in list and total number of tracks in list buttons labels ES Open V3 Play im stop Ir Prev M Next Select Opens window for ie desired Plays currently Stops currently Plays previous Plays next track or folder stopped track played track track track Page 42 Entertainment Operation Option Flight Data This option soothes des
12. with TL 6724 you will be able to share the screen data between the two instruments o 1 0 e 1 0 EFIS TL 6524 EMS TL 6724 If you connect TL 6524 with TL 6824 you will be able to read the same data on TL 6824 as you have on TL 6524 i l EFIS TL 6524 REMOTE TL 6824 If you connect TL 6724 with TL 6824 you will be able to read the same data on TL 6824 as you have on TL 6724 o 1 0 o 1 0 EMS TL 6724 REMOTE TL 6824 If you connect TL 6624 with TL 6824 you will be able to read the same data on TL 6824 as you have on TL 6624 1 0 0 1 0 EFIS amp EMS TL 6624 REMOTE TL 6824 Page 11 Introduction General Description TL ELEKTRONIC Back up System Recommendation We recommend this configuration for safe panel system redundancy TL 6524 and 6624 In the case of instrument failure flight information will be available on the second instrument i 6 i 8 EFIS amp EM S TL 6624 EFIS TL 6524 Page 12 Introduction unam General Description Explanation of Priority setting for Data Sharing The priority for Data Sharing is set in Setup Mode separately for EMS data in EMS Setup Mode and for EFIS data in EFIS Setup Mode Although Setup Mode is subject of Configuration Manual we explain priority setting of Data Sharing here to make you understand whole Data Sharing function at once EFIS Data Sharing Data Sharing Priority means importance of specific data EFIS or EMS Low Priority set
13. 624 TL 6524 EFIS data Page 13 Introduction unam General Description The INTEGRA Glass Cockpit Instrument System Before operation the INTEGRA please check to see if there are any parts missing or damaged If you have not received all the necessary components or if there are damaged components please contact TL elektronic or your TLe dealer immediately The INTEGRA requires a Remote Compass and GPS Receiver to provide a full range of functions 7 WARNING Obstacle clearance is not assured in 3D Terrain or Highway in the Sky HITS approach mode AN CAUTION If any display unit in the chain is inoperable the display units will not be able to share information The pilot must account for this down graded mode of operation and expect data will not transfer between displays NOTE It is highly desirable to provide each display unit with its own connection to each source of data if possible This increases the redundancy of the system and reduces the amount of lost function in the event a display unit becomes inoperative NOTE Most but not all data contained within this manual is accurate Some differences may be observed when comparing the information in this manual to other instrument generation models Before You Fly We strongly recommended that you read this entire guide before attempting to use the INTEGRA in an actual in flight situation Additionally we encourage you to spend time on the ground familiarizin
14. Oi Eh Tele tol INTEGRA EMS TL 6724 USER MANUAL Non TSO approved 000034 00 00 00 FUEL FLOW ENGINE TIME TIMER 12 40 41 05 12 10 AIRCRAFT 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
15. Storage Temperature 20 C to 60 C 4 F to 140 F Recharge Life 300 400 cycles A Lithium Polymer battery operates without a memory effect meaning it can be recharged before it is completely discharged without affecting the energy capacity A CAUTION Keep the Battery Pack connector away from metallic objects Any tampering of the cell within the INTEGRA Battery Pack is strictly forbidden in any circumstances Do not immerse in water Do not place near a heat source Never heat the battery nor throw into a fire Do not expose the battery pack to temperatures in access of 60 C 140 F A CAUTION The Integra Battery Pack is intended for use only with Integra Products Disposal Procedures For Ecological and Environmental reasons it is advisable to consult with local authorities for disposal regulations Page 25 Basic Operation Warning Signals Warning Signals Gear is safety engaged Gear is safety protuberant Gear is pushing up or pushing in or there is any problem with gear Canopy is open A dangerous quantity of CO is in the cockpit The information on measured quantity is not available INTEGRA is connected to an external power supply INTEGRA is power supply from battery D NOTE Landing gear position is shown by status indicators Indicator should be used only as a backup It is provided to give the pilot a single location to view the aircraft configuration The Gear Light
16. ce the user is encouraged to try to correct the interference by relocating the equipment or connecting the equipment to a different circuit than the affected equipment Consult an authorized dealer or other qualified avionics technician for additional help if these remedies do not correct the problem Operation of this device is subject to the following conditions 1 This device may not cause harmful interference and this device must accept any interference received including interference that may cause undesired operation 2 The INTEGRA display lenses are coated with a special antireflective coating which is very sensitive to skin oils waxes and abrasive cleaners It is very important to clean the screen using an eyeglass lens cleaner which is specified as safe for anti reflective coatings and a clean lint free cloth To obtain accessories for your INTEGRA please contact your TL elektronic dealer Help us better support you by completing our on line registration form today Registration ensures that you will be notified of product updates and new products and provides lost or stolen unit tracking Please have the serial number of your unit handy connect to our web site www tl elektronic com and look for our Product Registration link on the home page 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 6 Introduction
17. cond MSA Minimum Safe Altitude MSG Message MSL Mean Sea Level mul Multicom NATNL National NAV Navigation NAVAID Navigational Aid NDB Non Directional Radio Beacon NM Nautical Miles NRST Nearest NUM Number OBS Omnibearing Selector OCN Oceanic PDA Premature Descent Alert P POS Present Position PROC Procedure s PROV Province PTK Parallel Track PWR Power RAD Radial RAIM Receiver Autonomous Integrity Monitoring REF Reference REQ Required Requirements RESTRICTD Restricted RNG Range RTC Required Terrain Clearance RX Receive SBAS Space Based Augmentation System SID Standard Instrument Departure Sml Small SPD Speed SQ Squelch SRFC Surface STAR Standard Terminal Arrival Route SUA Special Use Airspace SUSP Waypoint sequencing suspended T Degree True TACAN Tactical Air Navigation TAS True Airspeed TAT Total Air Temperature Pape tu TEMP Temperature TER Terrain TERM Terminal TKE Track Angle Error TMA ICAO Terminal Control Area TRANS Transition TRFC Traffic TRK Track also Ground Track Angle TRSA Terminal Radar Service Area TWR Tower TX Transmit UTC Coordinated Universal Time also GMT or zulu UTM UPS Universal Transverse Mercator Universal Polar Stereographic grids VAL Vertical Alarm Limit VAR Var
18. data which the Integra is sending to bus EMS Data Sharing For example ru EFIS Data Sharing The picture on right side shows three Integra units connected by bus High Priority set High Priority set Arrows linking the units express actual flow of information Connection of TL 6624 and TL 6524 creates EFIS data redundancy because both units have internal sensors for measuring EFIS data The both units sends EFIS data to the bus because their EFIS Data Sharing is On EFIS Data Sharing is not set to Off EFIS data from TL 6524 takes priority over EFIS data from TL 6624 on the bus because TL 6524 is set to higher EFIS Data Priority than TL 6624 Therefore TL 6824 receives EFIS data from TL 6524 But TL 6624 and TL 6524 displays their own EFIS data Own data of the Integra always takes priority over data from the bus Qo 9g 9 9Q Q9 909 90Q Because TL 6524 has no inputs for measurement of EMS data the only way to display EMS data on the unit is to receive EMS data from TL 6624 via the bus Therefore priority for TL 6624 EMS Data Sharing could be set to Low or High There is no difference because this unit is only EMS data source TL 6 824 TL 6824 hasn t got Data Sharing Setting It only receives data available on the bus according to priority setting of data sources previously described The only way to disable receiving and displaying data in IT 20 standard screen is to unplug the bus from TL 6824 EMS data TL 6
19. e free from defects in materials and manufacture for three years from the date of purchase TL elektronic will at its sole option repair or replace any components that fail in normal use Such repairs or replacement will be made at no charge to the customer for parts or labour The customer is however responsible for any transportation costs This warranty does not cover failures due to abuse misuse accident or unauthorized alteration or repairs THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE STATUTORY OR OTHERWISE THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS WHICH MAY VARY FROM STATE TO STATE IN NO EVENT SHALL TL ELEKTRONIC BE LIABLE FOR ANY INCIDENTAL SPECIAL INDIRECT OR CONSEQUENTIAL DAMAGES WHETHER RESULTING FROM THE USE MISUSE OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT SOME STATES DO NOT ALLOW THE EXCLUSION OF INCIDENTAL OR CONSEQUENTIAL DAMAGES SO THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU To obtain warranty service call the TL elektronic Customer Service 420 49 548 23 92 for a returned merchandise tracking number The unit should be securely packaged with the tracking number clearly marked on the outside of the package and sent freight prepaid and insured to a TL elektronic warranty service station A copy of the original
20. ed to ROTOR RPM for helicopters and other rotor aircraft The switch between the ROTOR RPM and MAP Press the right Menu Baro knob and select Enter Setup Press button with label Yes Press the knob and select Configuration amp Sensors Now you can choose MAP and Rotor RPM and you can choose in each menu of this sensor if you want to connect or not connect this sensor Indicator of ROTOR RPM Indicator of MAP Water Temperature can be switched to CHT Temperature The switch between Water Temperature and CHT Temperature Press the right Menu Baro knob and select Enter Setup Press button with label Yes Press the knob and select Other Setting amp Calibration and then Water CHT Temperature Label Then you can choose option Water for Water Temperature or CHT 88 Cylinder Head Temperature in meaning used by ROTAX technically the sensor is placed on engine block Water Temperature Page 29 Integra Operation Description of Function EMS TLELEKTRONIC Description of function EMS RPM Engine Revolutions Per Minute If you use INTEGRA in helicopter you can connect rotor RPM sensor to INTEGRA and this information will be Rotor RPM displayed Oil press Indicator shows you actual oil pressure Left and Right Indicator quantity of fuel in left and right tank Oil Temp Indicator oil temperature Page 30 Integra Operation Buttons Description Buttons desc
21. els turn red to match any urgent notice appearing on the screen Data Port The INTEGRA allows the pilot to enter checklists flight plans general information and update firmware through the USB port This data must be verified for accuracy by the pilot prior to flight If you want to work with data from an external source plug a flash disk memory stick into the USB port Allow 10 seconds for the Integra to read the disk Press right knob to enter the menu and select Enter Setup When prompt Are you sure you want to enter to setup appears press button Yes Now the Integra is in Setup Mode Button label Data Port is displayed Press that button Menu Data Port will appear containing the following e Menu DATA PORT Import Checklist Import Configuration Export Configuration Export Flight Data Export Service Log Update Firmware NOTE If you can t see Data Port button label in Setup Mode check correct flash disk connection Page 19 Basic Operation TL ELEKTRONIC The Integra Control Panel Import Checklist You can create your checklist on your computer and you can transfer this data into the Integra Import Configuration You can create your configuration on your computer and you can copy these settings to the Integra Export Configuration You can export your configuration from the Integra to your flash disk Export Flight Data You can export your flight data from the Integra to your flash disk Export Service
22. g yourself with the operation of the product While first learning to use the instrument in the air we recommend you have a backup pilot with you in the aircraft Finally we encourage you to keep this manual in the aircraft with you at all times This document is designed to give you quick access to information that might be needed in flight NOTE While in flight it is the pilot s responsibility to use this product and this guide prudently Page 14 Introduction unam General Description Capabilities The INTEGRA s robust design enables the use of a wide range of engines and sensors You may configure the INTEGRA system to meet your monitoring requirements The INTEGRA visual and audio warning systems give you immediate notification of any potential problem that might otherwise go unnoticed The accurate and reliable solid state sensors of the INTEGRA provide essential information with a user friendly interface Power The INTEGRA requires between 10 and 30 volts DC for operation and should be connected to an external backup power supply with keep alive voltage The INTEGRA can be turned on during engine start The INTEGRA can be ordered with an optional internal Li poly backup battery which allows the instrument to continue to operate in the event of an external power failure This lithium polymer battery is rechargeable and is charge maintained by the INTEGRA If the always on circuit is connected the INTEGRA continues to charge it
23. heck for tightness Engine Compartment Check Taxi Landing Light Check Preflight check instructions for a preflight check Induction Air fitter DINE clear A 7 Left Side Nose Strut amp Tire Check inflation wear Before start engine instructions on what is needed to check before starting your engine Static Port Check Starting engine the procedures to start the engine Laft Wing z E E Fuel Tank Guantity Check secure fuel cap Engine run up a list of what is required during engine run up Pitot Tube Check Before takeoff a list of what needs to be checked before a takeoff Stall Warning Check r A Fuel Vi Landing instruction about what is necessary before landing OS Abe After landing a list of what must be done after landing Leading Edge Nav Light amp Wing Tip Check Shut down instructions on what is needed to be done before shutting down ie NA o eee etna ie Tire Chock Remove Walk Around Airplane for Final Check For example Checklist of Preflight check for Cesna 152 Page 33 Integra Menu Statistics for EMS Statistics for EMS Statistics provides a summary of Engine Information EMS Statistics RPM MIN Minimum rotations per minute RPM MAX Maximum rotations per minute OIL PRESS MIN Minimum oil pressure OIL PRESS MAX Maximum oil pressure OIL TEMP MIN Minimum oil temperature OIL TEMP MAX Maximum oil temperature ROTOR RPM MIN Minimum rotor rotations per minute
24. iation VER Version VFOM Vertical Figure of Merit VFR Visual Flight Rules VLOC VOR Localizer Receiver VNAV Vertical Navigation VOL Volume VOR VHF Omnidirectional Radio Range VPL Vertical Protection Level VS Vertical Speed VSR Vertical Speed Required WAAS Wide Area Augmentation System WPT Waypoint WX Weather XTK Crosstrack Error Technical Parameters Technical Parameters Physical characteristic Width 192 mm 7 559 Height 148 mm 5 827 Depth 76 5 mm 3 012 Panel rectangle hole 185x143 mm 7 283x5 63 Weight without battery 1150 g 2 54 Ib Weight with battery 1250 g 2 76 lb General Specifications Operating Temperature Range 20 C to 60 C Humidity 95 non condensing Altitude Range 4600 meters max Power Range 10 0 to 32 0 Volts Max Signalization 30 Volts 1 Ampere Power Consumption 0 95 Ampere 14VDC without sensors Vibration 5 to 500 Hz Show Rate LCD Refresh Long term Memory and communication Storing Rate 15 fps depends on volume of information displayed 0 1 to 60 seconds user selectable Memory Capacity Scheck method Data Saved Endurance 30 years Rolling Memory life time 100 000 hours 1 second storing rate Page 46 Technical Parameters Communication up to 115 200 bps 12 Mb s 480 Mb s 1 Mb s Display parameters Resolu
25. ire for flight info of impatient and curious passengers It displays Airspeed Altitude and Time to arrival ENJOY YOUR FLIGHT Movie Airspeed 182 km h Altitude 1130 m Music Flight Data Time to arrival 1 59 hours Option Exit The option exits Entertainment Screen Page 43 Abbreviations ACTV Active ALT Altitude APR Approach APT Airport ARSPC Airspace ARTCC Air Route Traffic Control Center ARVL Arrival AUX Auxiliary AVGAS Aviation grade Gasoline AVTN Aviation BARO Barometric setting BRG Bearing To C Degree Celsius C V COM VLOC CAS Calibrated Airspeed CDI Course Deviation Indicator CLR Clear COM Communications Transceiver CRSR Cursor CTA ICAO Control Area CTAF Common Traffic Advisory Frequency CTR Center see ARTCC CUM Cumulative DB Database DEN Density DEP Departure DEPT Departure guidance DIS Distance Abbreviations DME Distance Measuring Equipment DTK Desired Track EFF Efficiency ELEV Elevation ENDUR Endurance ENR En Route ENT Enter EPU Estimated Position Uncertainty ESA En Route Safe Altitude ETA Estimated Time of Arrival ETE Estimated Time En Route F Degrees Fahrenheit FAF Final Approach Fix FF Fuel Flow FIR Flight Information Region FLTA Forward Looking Terrain Avoidance FOB Fuel On Board FPL Flight Plan fpm Feet Pe
26. me unsafe Use the INTEGRA at your own risk To reduce the risk of unsafe operation carefully review and understand all aspects of this Owner s 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 The INTEGRA series does not contain any user serviceable parts Repairs should only be made by an authorized TL elektronic service center Unauthorized repairs or modifications could void your warranty and authority to operate this device under FCC Part 15 regulations Page 5 Introduction unam Warnings amp Cautions amp Notes 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 O NOTE This device complies with Part 15 of the FCC limits for Class B digital devices This equipment generates uses and can radiate radio frequency energy and if not installed and used in accordance with the instructions may cause harmful interference to radio communications Furthermore there is no guarantee that interference will not occur in a particular installation If this equipment does cause harmful interferen
27. r Minute FREQ Frequency FSS Flight Service Station ft Feet G S Glideslope gl gallons GPS Global Positioning System GS Ground Speed HAL Horizontal Alarm Limit HDG Heading Page 44 HFOM Horizontal Figure of Merit hg Inches of Mercury HPL Horizontal Protection Level HITS Highway in the Sky HWY Highway IAF Intermediate Approach Fix ID Identifier ig Imperial Gallons ILS Instrument Landing System IND Indicated INT Intersection INTEG Integrity ITI Imminent Terrain Impact kg Kilograms kHz Kilohertz km Kilometers kph Kilometers Per Hour kt Knots L VNAV Lateral and vertical navigation guidance LNAV VNAV service level LAT LON Latitude Longitude Ib Pounds LCL Local LFOB Left over Fuel On Board LNAV Lateral Navigation only LNAV V Lateral Navigation with advisory vertical guidance LOC Localizer Abbreviations LPV Lateral Precision Performance with Vertical Guidance LRES Left over Fuel Reserve Time Lrg Large It Liters M Degrees Magnetic m Meters MAP Missed Approach Point MAHP Missed Approach Hold Point MAPR Missed Approach guidance mb Millibars of Pressure Med Medium MGRS Military Grid Reference System MHz Megahertz mi Statute Miles MOA Military Operations Area mph Statute Miles Per Hour mpm Meters Per Minute mps Meters Per Se
28. r favourite music or watch movies These multimedia possibilities of the Integra enrich passengers experience from flight To enter Entertainment Menu Press right knob select option Entertainment from menu When prompt Do you want to enter to Entertainment appears press button Yes Now the Integra is displaying Entertainment Screen Movie Music Flight Data Exit Part for displaying chosen option menu Page 39 Entertainment Unam Operation Handling the menu Rotate right knob for scrolling through menu Select desired function by pressing right knob O NOTE If you want to open multimedia file on plugged SD card you won t be able to have connected USB flash drive That s because the Integra will check primarily for connected USB flash drive Then if USB flash drive isn t found the Integra will check for SD card And if SD card is not neither plugged then the Integra will load files from internal memory Option Movie Probably you want to watch some movie on your USB flash drive or SD card To do this follow these instructions Press left knob Open Window will appear for selecting video file There you can scroll through currently viewed directory by rotating left knob Names of displayed subdirectories are closed in square brackets Playable files are displayed with postfix 3gp If you want to move down to some subdirectory choose desired subdirectory and press left knob If you want
29. ription There are 3 function buttons Timer Checklist and Statistic and 1 knob Menu Baro Checklist Statistic Menu Baro 9 9 OO Buttons description Page 31 integra Menu TLELEKTRONIC Introduction Integra Menu To enter a menu just press right knob with the Menu Label Turn the knob to scroll through the menu titles then press the knob when the title is highlighted Select the Back Arrow symbol to return to the previous menu or screen Each Menu has an EXIT MENU title at the bottom Press to select and exit the menu e MENU BARO Brightness Checklist Statistic Entertainment Enter to Setup Power Off About Exit Menu Brightness Instruction is therein before Page 23 Page 32 integra Menu TLELEKTRONIC Checklist Checklist The Checklist is your most valuable tool to insure a safe flight It is easy to miss a critical step in any phase of the flight latch the canopy drop the landing gear select the mains etc Each checklist is determined by your aircraft make and model and is installed into the INTEGRA to be easily recalled by the pilot at a moment s notice You can edit this checklist on your computer and then you can copy via USB port on INTEGRA e Menu CHECKLIST e Preflight check e Before start engine e Starting engine e Engine runup e Before take off Cesna 152 e Landing Preflight Checklist e After landing Cowling Intakes Prop amp Spinner Check e S h ut d own Alternator Belt C
30. s internal battery even if the instrument is turned off This ensures a full charge for your internal emergency battery Under normal conditions the internal battery should have a voltage between 11 1 and 12 6 volts A new fully charged internal battery is rated for a minimum 30 minute of normal operation with the INTEGRA If the INTEGRA has switched to its internal back up battery due to external power loss it is advisable that you land your aircraft as soon as possible NOTE Battery life is dependent on for example the brightness of the display and number of sensors which are battery powered etc Page 15 Introduction General Description TL ELEKTRONIC Theory of Operation The primary flight instruments on your EFIS display are generated using a group of calibrated sensors All of them are solid state that is there are no moving parts These sensors include accelerometers which measure forces in three directions rotational rate sensors which sense rotation of all three axis pressure transducers for measuring air data and magnetometers on all three axis for measuring magnetic heading NOTE This product is intended for experimental and Light Sport Aircraft categories and is not approved for installation in Certified Aircraft Page 16 Basic Operation Introduction BASIC OPERATION Operation terminology Term select in the context of Integra operation in this manual means this sequence of operation steps
31. s located on the aircraft instrument panel should be viewed before landing The INTEGRA can provide a gear up voice warning if the following functions are monitored Gear Position and Airspeed If Airspeed drops below a programmed level set for your aircraft and the Landing Gear is not down you will get a voice warning Page 26 Integra Operation General Description INTEGRA Operation Page 27 Integra Operation Description of complete EMS Description of complete EMS P P Oil Pressure indicator Tachometer Voltage and Ampere Information BATTERY Sd 12 3 V 30A PUMP PUMP 12 2V ee Cylinder Head AVIONICS AVIONICS Temperature 6 Y 279 measured by 207 thermocouples under spark plugs 277 not in meaning 208 used by ROTAX and Exhaust E 281 GasTemperature 3 E 198 Display and Further description on next page Water Temperature Oil Temperature indicator Manifold air pressure FUEL GUANTITY Wi E E 16 3 GAL FUEL PRESS m EA 6 is 10 12 20 14 10 10 TIME UTC DATE AIRCRAFT GAL USED GAL REMAIN 0000 34 00 00 00 ENGINE TIME TINTER Fuel consumption fuel pressure and fuel flow information Page 28 Internal air temperature Fuel used and remainin Fuel Values are compu by use of actual measur Fuel Flow value Time Integra Operation TL ELEKTRONIC Description of complete EMS Comment on specific EMS indicators MAP manifold air pressure can be switch
32. sales receipt is required as the proof of purchase for warranty repairs TL elektronic retains the exclusive right to repair or replace the unit or software or offer a full refund of the purchase price at its sole discretion SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY Page 8 Introduction unam General Description General description Thank you for purchasing the TL elektronic INTEGRA This section provides some important cautionary information and general usage instructions for this manual Before You Fly We strongly recommended that you read this entire guide before attempting to use the INTEGRA in an actual flying situation Additionally we encourage you to spend time on the ground familiarizing yourself with the operation of the product While first learning to use the instrument in the air we recommend you have a backup pilot with you in the aircraft Finally we encourage you to keep this manual in the aircraft with you at all times This document is designed to give you quick access to information that might be needed in flight AN CAUTION _ Ina flying situation it is the pilot s responsibility to use the product and the guide prudently OEM Installations If your INTEGRA is installed by an OEM aircraft producer you may find that you are unable to access some menus and settings Some TL elektronic distributors customize various areas of the INTEGRA firmware to maintain a consistent pilot
33. served CHT4 MAX 208 T Delete values Hide Page 35 Setup Menu Configuration Manual TL ELEKTRONIC Configuration of Integra Enter to setup In setup you can edit many parameters as you wish such as units configuration amp sensors limits other setting amp calibration and external devices Press right knob and select Enter Setup When prompt Are you sure you want to enter to setup appears press button Yes Are you sure you want to enter to setup Enter to setup NOTE More about SETUP menu you can find in CONFIGURATION MANUAL on the CD Page 36 eas TLELEKTRONIC Power Off and About Power Off You can turn the Integra off by pressing the Power Off button You have 20 seconds to cancel this operation Just press any knob or button NOTE When you power up the Integra and the Integra starts to shut off press any button and it is necessary to disconnect the Main Switch Signal Menu Setup Other Setting amp Calibration Main Switch Control About There you can find the information about your Integra HW version Information about the hardware version GUI version Information about the graphics interface Release Information about the firmware version Page 37 Entertainment About Menu Entertainment Page 38 Entertainment About amp Operation TLELEKTRONIC Menu Entertainment serves for access to multimedia functions of the Integra You can listen to you
34. tion 800x480 Brightness 800 cd m2 Integra support SD and SDHC memory card Page 47 Page 48 2010 TL elektronic y Alagi Ji 3 Va i WI or its subsidiaries NIEGHA ENS 1L0 4 USER MANUAL TLELEKTRONIC Europe United States of America Part Number TLD 6724X DU 001_RevE
35. unam Accessories amp Packing List Accessories and Packing List The INTEGRA represents TL elektronics continued commitment to providing you with the most advanced technology available today in an accurate easy to use design suitable for all of your flying needs Unless otherwise specified within this manual the term INTEGRA applies to the TL 6524 TL 6724 TL 6624 and TL 6824 Please note that the difference between these models is indicated in the Specifications section of this manual Before installing and getting started with your new system please ensure that your package includes the following items If any parts are missing or are damaged please contact your TL elektronic dealer Standard Package INTEGRA Unit nstallation Rack Accessories User and Configuration manual CD with software and Installation Manual Warranty Card Optional Accessories Internal back up Battery SD card with 3D Terrain Your aviation maintenance specialist should perform the installation and configuration of your new INTEGRA unit The INTEGRA should be secured in the installation rack with the proper wiring connections Be ready to anwer any questions that your maintenance specialist could have about the installation such as location of antennas or any connections to other equipment in the panel Page 7 Introduction unam Limited Warranty Limited warranty The TL elektronic company warrants this product to b
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