User`s manual - TL elektronic
Contents
1. i 30 INTEGRA IOCIS ERN Eed 31 2 Description of complete EMS PR RU 32 Introduction unam Table of Contents Description of tuncion EMS aeos neque oie tete a Dont pego ERA TRIAL pa RUN RE 34 Integra Men s 35 A O II Cep E AEO E A ERO 35 mE eso dore pP TRES 36 gt Statistics tor EMS DEEP 37 Configuration A E O E E E E dui sua i a tie pd 39 2 GBIDtOSellpauset Ee NU n e use e eu e Se re 39 A sc LO nee ANA lan es 40 er AD T TX MEUS Ret aa haces 40 Ment Entertatibiiente ie peo rtr A Tuer aos ee Seege 41 A Mu iE E EA 43 2 Option MUSIC Sr P TR 45 Option Flight Dita ais cee ate A 46 A non milan nine ee 46 dl cos tunc SES ES TS I ML Ro MM LM Au E MM 47 MN a RS A Eid e D AN hate 49 Page 3 Introduction TLELEKTRONIC Record of Revision Record of revision Revision Revision Date Description ECO Insertion date By PrA 13 04 2013 Initial version Hovorka Page 4 Introduction 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 h2. Copyright 2013 TL elektroni EUN eT EE INTEGRA EMS TL 6760 USER MANUAL 12 40 41 05 12 10 AIRCRAFT TL elektronic Airport Building 125 503 41 Hradec Kralove Czech Republic O Copyright 2013 TL elektronic All Rights Reserved Except as expressly provided below no part of this manual may be downloaded transmitted copied reproduced disseminated or stored in any storage medium for any purpose without the express prior written consent of the TL elektronic company Address your questions about the technical information to TL elektronic Other information about sale distribution should be directed to our exclusive distributors see World Distributor list on our website Producer s address TL elektronic Inc Airport Building 125 503 41 Hradec Kralove Czech Republic Fax 420 49 548 23 94 E mail info tl elektronic com Web Site Address www tl elektronic com Please send your e mail address to customer tl elektronic com to receive the latest information about software upgrade Send your ideas to innovation tl elektronic com We will evaluate your suggestion and provide an update Windows is registered trademark of Microsoft Corporation All trademarks and registered trademarks are acknowledged SchecK is registered trademark of TL elektronic iFamily is registered trademark of TL elektronic sModern is registered trademark of TL elektronic All information in this User s manual is subject to change without prior noti
3. 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 D 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 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 O 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 the right hand knob 4 Select Power Off O NOTE All settings and calibrations will be stored when the IN
4. 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 Water Temperature Cylinder Head Temperature in meaning used by ROTAX technically the sensor is placed on engine block Page 33 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 i 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 34 Integra Menu TLELEKTRONIC Introduction Integra Menu To enter the menu just press the right hand 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 Other Setting Enter to Setup Power Off About Exit Menu Brightness Instruction is therein before pag
5. 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 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
6. mouse button over Integra buttons area The context menu will appear 20 FT min x100 Menu HDG Screen Menu Baro Measure simulator C e Checklist setting Demo PC application is same for all versions of the Integra Page 21 Basic Operation Data Port 2 Select Checklist setting from context menu The Checklist setting window will appear x Checklist Y Aircraft Help Left and right alignment is devided by inside of line Save as Example Seats Belts amp Harness Fasten amp Adjusted will look like Close Seats Belts amp Harness Fasten amp Adjusted Each line can contain max 60 characters and checklist can contain max 18 lines Edit actual checklist rap amp Spinner Check ck for tightness Check Cowling Intakes F Alternator Belt E name Compart T axi Landing L Induction Air F Left Side No Tire Check inflation wear Static Port Check Left Wing Fuel Tank Quantity Check secure fuel cap Pitot Tube Check Stall Warning Check Fuel Vent Checl Tie Down Remove Leading Ed ght amp Wing Tip Check Alleror rollers hinges weights Tire Brake lire Lhock Remove eck It iflation wear Walk Sround Airplane for Final Check version 0 2 2 Page 22 Basic Operation TL ELEKTRONIC Data Port 3 From drop down list Checklist choose desired checklist for editing Select check box Edit actual checklist
7. 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 interference 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 subje
8. to edit chosen checklist Now text of appropriate checklist changed from gray to black and you can edit it After you ll be satisfied with content of all checklists select button Save as to save complete set of checklists at once In Save as window choose root directory of your USB flash drive The second step Uploading checklists to the Integra 4 Plug a USB flash drive into the USB port of the Integra Allow 10 seconds for the Integra to read the drive Press the right hand 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 In menu Data Port select Import Checklist Page 23 Basic Operation TL ELEKTRONIC Data Port Update Firmware The first step PC operation 1 Create the tle directory and then create the update directory inside the tle on your USB flash drive So the path will be X tle update 2 Copy the file fwu tls to the update directory on your USB flash drive The second step Uploading firmware to the Integra 3 Plug USB flash drive into the USB port of the Integra Allow 10 seconds for the Integra to read the drive Press the right hand 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 Mo
9. 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 27 Basic Operation pios TL ELEKTRONIC Brightness This controls the brightness of the LCD Press the right hand knob and select Brightness Rotate the knob to choose the level of brightness Brightness The green strip specifies level of brightness O NOTE This function is available only if DIMMER SOURCE CONTROL is set to MANUAL Press the right hand 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 the right hand 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 28 Basic Operation TLELEKTRONIC Information about Battery Information about Battery The INTEGRA utilizes a Lithium Polymer battery with the following characteristics 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 stri
10. INTEGRA applies to the TL 6524 TL 6724 TL 6624 TL 6824 TL 6560 TL 6760 TL 6660 and TL 6860 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 Installation Rack Accessories User and Configuration manual CD with software and Installation Manual Warranty Card Optional Accessories nternal 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 answer 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 be 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 accide
11. Plays currently Stops currently Plays previous Plays next selecting desired stopped video played video track track video file or folder Page 44 Entertainment Operation Option Music NOTE The Integra only supports MP3 audio files elapsed time of track name of currently played track remaining time of track loop playing mode number of currently played track in list and total number of tracks in list Flight Data Exit shuffle playing mode buttons labels EN Open LE Play F Stop r7 Prev D Next UN Select Opens window for selecting desired track or folder Plays currently Stops currently Plays previous Plays next stopped track played track track track Page 45 Entertainment Unam Operation This option soothes desire 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 1130m Music Flight Data Time to arrival 1 59 hours The option exits Entertainment Screen Page 46 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 C
12. TEGRA is Powered Off Page 17 Basic Operation The Integra Control Panel The INTEGRA Control Panel The picture below shows Integra Control Panel Integra Control Panel includes 2 knobs 6 buttons and USB Data Port Left hand Buttons USB Buttons Right hand knob Data Port knob Page 18 Basic Operation TL ELEKTRONIC The 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 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 Labels turn red to match any urgent notice appearing on the screen Page 19 Basic Operation TL ELEKTRONIC Data Port 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 Access to Data Port function If you want to work with data from an external source plug USB flash drive into the USB port Allow 10 seconds for the Integra to read the drive Press the right hand knob to enter the menu and select Enter Setup When prompt Are you sure you want
13. ature on cylinder 3 measured by thermocouple under spark plug CHT4 MAX Maximum temperature on cylinder 4 measured by thermocouple under spark plug Page 37 Integra Menu Statistics for EMS IN 0 T MIN O MAX 280 MAX 277 MAX 278 T MAX 274 C IAT MAX 20 C DAT MAX 17 CHT1 MAX 282 T CHT2 MAX 275 T CHT3 MAX 244 CHT4 MAX 208 T Delete values Hide Page 38 If Statistics are displayed the basic menu is changed HIDE statistic screen is closed DELETE VALUES you can erase statistic values 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 deleted If you press No the statistic will be conserved Setup Menu Configuration of Integra 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 the right hand 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 Page 39 ioa M TL ELEKTRONIC Power Off and About Power Off You can turn the Integra off by pressing the Power Off button You have 20 seconds to cance
14. ce Page 1 Introduction unam Table of Contents Table of Contents DE CS A MR NO e UM MEME o MM EC RM MM 2 A E AAT ai 4 Accessories ww iudi ab TE eeg 7 LEE Ee 8 General descriptio eee eee em ne nea is 9 DEP oos lei C te ne E e O IO 10 lt T t gra ira VO Coat MID EO mmm 10 Compatibility of Integra Glass COC AA A ennui 11 e Explanation of Possible COMES TT TTE 11 amp Backup System Recon Ads 12 Explanation of Priority setting for Data Sharing iusso Prnt pii Pip RISQUE EUREN CLR ias 13 s TheINTEGRA Glass Cockpit Instr m nt S VS E 14 amp e TEE 15 EE D A E 15 TRACY of ETC IBI NET D Emm 16 BASIC OPERATION er H H 17 e Operation terminolo py ER mem 17 lt Turmne th INTEGRA ON ai 17 T rme the INTEGRA OFF a e E EERE EE EE A E A IA 17 s Ihe INTEGRA Control Panorama daa aseisiin Ee RES EUMD SEEE di AR ans 18 d o rrr eee eae PS 19 gt B ttons ARUBA G eia 19 SEE cd co erc lteiactue 20 Ecran mm 25 E A E 27 E a dodo es 28 M Intormation About Battery C 29 b BU DDR eiui MH A
15. ct 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 unam Accessories amp Packing List Accessories and Packing List The INTEGRA represents TL electronics 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
16. ctly 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 29 Basic Operation Warning Signals Warning Signals Gear 1s 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 1s 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 Lights 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 30 Integra Operation General Description INTEGRA O
17. ctor to link it to INTEGRA and two lugs which nicely lock it to the battery holder Lugs e Connect the cables located in the battery holder to the Back up battery The connector is notched so 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 O c and the connector must be on the top You should obey this to prevent damage of the battery cable caused by ed sharp edges of the battery holder Page 25 Basic Operation TLELEKTRONIC Battery Installation ANNANN UU 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 ns Integra holder SC Page 26 Basic Operation TLELEKTRONIC SD card Installation SD card Installation Slot for SD card 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 e If you want
18. de Button label Data Port is displayed Press that button In menu Data Port select Update Firmware 4 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 AN CAUTION Ensure sustaining voltage during updating if during updating fails the electric power supply the Integra can be damaged AN CAUTION Keep the USB flash drive connected with the Integra during updating AN CAUTION This data port is intended only to be used with USB flash drive Do not try to connect it to another USB device Page 24 Basic Operation TLELEKTRONIC Battery Installation Battery Installation 7 WARNING Before 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 this Cover wire must be removed Connector e The battery is intended to be used only with the INTEGRA The Battery has a one conne
19. e 28 Page 35 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 Follow instructions in section Data Port page 20 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 Shut down ee E Taxi Landing Light Check Preflight check instructions for a preflight check greet lip RR EE E 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 ge tini Dm PE 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 Landing instruction about what is necessary before landing dia Sue 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 do
20. e 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 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
21. e 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 either 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 the left hand knob Open Window will appear for selecting video file There you can scroll through currently viewed directory by rotating the left hand 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 the left hand knob If you want to move up to the parent directory choose item and press the left hand knob For replaying desired video file just choose appropriate item and press the left hand 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 43 Entertainment Operation elapsed time of video remaining time of video Music Flight Data Exit buttons labels Open D Play r Stop m Prev M Next Opens window for
22. eight 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 become 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
23. eplace your TL 6624 with TL 6660 without any modification of harness Here is table describing part numbers for Integra Glass Cockpits Funcional Part Number for Part Number for Integra with 7 display Integra with 9 display EFIS amp EMS TL 6624 TL 6660 EFIS TL 6524 TL 6560 EMS TL 6724 TL 6760 Remote Display TL 6824 TL 6860 Explanation of Possible Connections NOTE This section does not contain all possible connections Introduction of new Integra Glass Cockpits with 9 displays to market bring many new possible connections Here are a few Instrument connection possibilities es If you connect TL 6524 with TL 6724 you will be able to share the screen data between the two instruments 0 1 0 CY EXPE EFIS TL 6524 EMS TL 6724 Page 11 Introduction unam General Description 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 o wl wm 0 o ele e 0 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 1 CEE 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 2 1 0 Ii EFIS amp EMS TL 6624 REMOTE TL 6824 Back up System Recommendation We recommend this configuration for safe panel system redundancy TL 6524 and 6624 In the case of inst
24. hain 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 O 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 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 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 config
25. idance 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 Second 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 Ins
26. l 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 40 Entertainment About Menu Entertainment Page 41 Entertainment About amp Operation TL ELEKTRONIC Menu Entertainment serves for access to multimedia functions of the Integra You can listen to your favourite music or watch movies These multimedia possibilities of the Integra enrich passengers experience from flight To enter Entertainment Menu Press the right hand 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 IVlovie Music Flight Data Exit Part for displaying chosen option menu Page 42 Entertainment Unam Operation Handling the menu Rotate the right hand knob for scrolling through menu Select desired function by pressing the right hand knob 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 becaus
27. nt 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 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 th
28. ommunications 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 Per 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 47 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 gu
29. peration Page 31 Integra Operation nmm Description of complete EMS and Further description on next page Description of complete EMS Oil Pressure indicator Water Temperature Tachometer gt Oil Temperature indicator Manifold air pressure Internal air temperature Outside air temperature Voltage and 0 f ssl WATER j Ampere i 259 i e i Fuel used and remaining eu Fuel Values are computed Information j by use of actual measured GA e ee gi EE o Fuel Flow value BATTERY A 12 3 V Cylinder Head 122V 2 0 7 326 Stop watch Temperature din d s measured by thermocouples under spark plugs not in meaning used by ROTAX and Exhaust GasTemperature Display ENGINE TIME Engine time Date Time Fuel quantity fuel pressure and fuel flow information Page 32 Integra Operation TL ELEKTRONIC Comment on specific EMS indicators Comment on specific EMS indicators MAP manifold air pressure can be switched 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
30. rument failure flight information will be available on the second instrument 8 i e LEE EFIS amp EM S TL 6624 EFIS TL 6524 Page 12 Introduction 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 Low Priority set EMS Data Sharing Low or EFIS Data Sharing High Priority set High Priority set EMS data TL 6624 TL 6524 Qo9 9g9 9Q Q9 90 9 90Q EFIS data TL 6824 Q o o 0 oo Q NOTE Glass Cockpits on page 11 Data Sharing Priority means importance of specific data EFIS or EMS data which the Integra is sending to bus For example The picture on right side shows three Integra units connected by bus 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 1s set to higher EFIS Da
31. ta 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 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 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 standard screen is to unplug the bus from TL 6824 Explanation of priority setting is also applicable for Integra units with 9 displays please see section Compatibility of Integra Page 13 Introduction unam General Description The INTEGRA Glass Cockpit Instrument System Before operation the INTEGRA please check to see 1f 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 c
32. 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 amp 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 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 Compatibility of Integra Glass Cockpits New Integra Glass Cockpits with 9 displays have same software architecture as Integra Glass Cockpits with 7 displays This means that functionality is identical for both mentioned product lines The product lines are fully compatible with each other Practically this means that for example EFIS TL 6524 can be connected to TL 6760 via iFamily amp BUS Also HW solution for connection is identical for both product lines the connectors are identical so for example you can easily r
33. 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 e Import Checklist e Import Configuration e Export Configuration e Export Flight Data e Export Service Log e Update Firmware NOTE If you can t see Data Port button label in Setup Mode check correct USB flash drive connection 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 USB flash drive Export Flight Data You can export your flight data from the Integra to your USB flash drive Export Service Log You can export your service log from the Integra to your USB flash drive Update Firmware You can update the firmware of Integra Page 20 Basic Operation Data Port TL ELEKTRONIC The first step Integra Demo PC application To create or edit checklist Installed Integra Demo PC application is required You can obtain Integra Demo from TL elektronic web site Products gt LSA gt category EFIS amp EMS Integra gt TL 6x24 gt Downloads gt Demo PC application 1 Connect USB flash drive to your personal computer Run Integra Demo press right
34. trument 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 Page 48 TEMP Temperature TER Terrain TERM Terminal TKE Track Angle Error TMA ICAO Terminal Control Area TRANS Transition TREC 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 Variation 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 240 8 mm 9 480 Height 178 mm 7 008 Depth 75 5 mm 2 972 Panel rectangle hole 233 8x172 mm 9 205 x6 772 Weight without battery 1533 g 3 38 lb Weight with battery 1633 g 3 60 lb General Specifications Operating Temperat
35. ure Range 20 C to 60 C Humidity 95 non condensing Altitude Range 10000 meters max 32808 feet max Power Range 10 0 to 32 0 Volts Max Signalization 30 Volts 1 Ampere Power Consumption 1 15 Ampere 14VDC without ext sensors 1 83 Ampere when battery is charging 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 amp method Data Saved Endurance 30 years Rolling Memory life time 100 000 hours 1 second storing rate Page 49 Technical Parameters Communication up to 115 200 bps 12 Mb s 480 Mb s 1 Mb s Display parameters Resolution 800x480 Brightness 800 cd m2 Integra support SD and SDHC memory card Page 50 Page 51 Page 52 2013 TL elektronic or its subsidiaries Part Number TL X 6760X DU 001 PrA
36. ure 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 its 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
37. wn up i NA o dense Tire Chock Remove Walk Around Airplane for Final Check For example Checklist of Preflight check for Cesna 152 Page 36 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 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 temper
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