User`s manual - TL elektronic
Contents
1. Q 18 INTEGRA Control cuc eec 19 o n 19 Buttons BE EE 20 Ib gro m eee 20 Battery Install EE deenen 22 SD card PINS e EE 24 PUES P 25 Information about TS GIy PRI TE 26 Warning ST IN ALS E E TO E Oo ele ee ea ee se eS 247 INTEGRA Operation m 28 Description of EFIS SEO MER M A A da ieren 29 Descriptionof function EA da H A 30 Introduction unam Table of Contents Navigation SeCEIOIE io IRR QI DIR ROM AS IA NUI UNIO NIRE O UICE UNI EE 36 Description of VOR qe M E 37 Description OE LOC e e a e M e A ea ta Due a e e e M rt e e e N 39 Descuption GPS ii A A A A ES 41 NAMED GA ao 45 A NNMERO e 46 lem E rere 46 A RO 47 PT BEE 48 TAS BUG C asoa an e A ASA aa TE ais EN 48 Lee EE 49 HDG Ne ccc rar E 50 Integra IV Car PRSE r A e2. 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 72 Entertainment Unam About amp 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 to move up to the parent directory choose item and press left knob For replaying desired video file just choose appropriate item and press lef
3. Copyright 2010 TL elektronic Non TSO approved TL elektronic Airport Building 125 503 41 Hradec Kralove Czech Republic INTEGRA EFIS TL 6524 USER MANUAL Integra 299 240 1400 ang 050 Joao m D E 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
4. VOR station the course is to the left Full scale OBS represents 5 degrees off course That Bearing from the means 2 5 degrees on left side and 2 5 standby VOR station degrees on right Page 39 Navigation Section EXITO Description of LOC All data are valid Current Glide Slope is out of recommended range Glide Slope Indicator If glide slope is in recommended Glide Slope Indicator Red flag GS indicates range yellow arrow will appear to indicate current glide that current glide slope is out of recommended slope Full scale of the range represents 1 4 degree Mark in range half of scale represents ideal glide slope Page 40 Navigation Section Description of GPS Waypoint identifier Description of GPS Bearing To Waypoint BTW indicator GPS Distance to waypoint this ID LOWK OBS 163 can be expressed in Knots BTW 199 miles or kilometers see PHS section Units in ALT 3499 FT Configuration Manual SPD 191 KTS TRK 166 HDG 271 Altitude Ground spee Track indicator This indicates your direction over the ground as reported by the GPS It can differ from magnetic heading when crosswinds are present OBS Omni Bearing Selector Page 41 GPS label will be changed to yellow GPS NO ACTIVE label if the Integra doesn t get data about flight plan from GPS receiver If the Integra completely loses signal from GPS receiver label will change to red GPS NO DATA This field sho
5. 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 60 Autopilot About Autopilot optional function Page 61 Autopilot TLELEKTRONIC About The Integra Autopilot referenced below as the AP offers roll aileron pitch elevator and yaw rudder axis control The number of axes which can be controlled by AP is depending on your purchased Activation Key as well as variety of navigation abilities of AP See Price list for available AP Activation keys and their features HDG Full set of HDG TRK l e ALT VS Vertical primary flight horizontal ALT Control Horizontal Dedicated TRK Vertical TRK HDG Vertical NAV 2 axis 3 axis hold and Wheel GPS NAV Speed GPS i engine Nav radio or chance Steeiin Steerin Control ALT hold pre Steerin Radio or control control instruments GPS 9 9 9 j selected 9 GPS pre arm Integra with Premium Activation E 2 Key Integra with P aM e e e e e e e e e e e e Key Integra with Gold Activation e e e e e e e e e e e e e Key Main differences between Activation Keys Premium Aircraft is stabilized in flight altitude and heading Moreover the AP features ability of following flight path specifying only heading This flight path is determi
6. NAV The AP will be following heading and or altitude determined by selected navigation source VOR or GPS If you want to change navigation source press left knob and select option Nav Source There you can choose desired navigation source Cancel It cancels setting the AP Page 66 Autopilot TLELEKTRONIC Configuration After you ve finished this step the AP will be controlling the aircraft according to selected axis axes and its navigation controls ON state of the AP is indicated by button label AP EN Screen WENT Baro How to turn off the AP This part assumes that the AP is already in on state fmm PDG XPTN Screen MERO Baro Press button AP FN The button label has changed to AP OFF Press button AP OFF Now the AP is in off state Off state of the AP is indicated by button label AP MN MET PDG P Screen MERO Baro Page 67 Autopilot Configuration How to readjust the AP This part assumes that the AP is already in on state This part describes changing of controlled axis axes and navigation controls of the AP Change of controlled axis MET ADG XPTN Screen WERT Baro Press button AP FN HPCE RE PAE EE Then press button Axis The options are same as in step Selecting of controlled axes We er SNE wr tance After selecting desired option the button label has changed back to AP FN MER PDG KPTN Screen fien Baro EE The AP is controlling
7. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY Page 9 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 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 calibrat
8. YOUR FLIGHT IVlovie Airspeed 182 km h Altitude 1130m Music Flight Data Time to arrival 1 59 hours we Exit Option Exit The option exits Entertainment Screen Page 76 Abbreviations Abbreviations ACTV Active ALT Altitude AP the Integra Autopilot 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 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
9. 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 lepide 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 o eee etna ie Tire Chock Remove Walk Around Airplane for Final Check For example Checklist of Preflight check for Cesna 152 Page 52 Integra Menu Statistic for EFIS TLELEKTRONIC Statistic for EFIS Statistics provides a summary of EFIS Information ALTITUDE MIN Minimum altitude ALTITUDE MAX Maximum altitude SPEED MIN Minimum speed SPEED MAX Maximum speed VSI MIN Minimum VSI VSI MAX Maximum VSI ACCELERATION MIN Minimum acceleration ACCELERATION MAX Maximum acceleration 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 deleting If you press No the statistic will be conserved Page 53 Integra Menu Other Setting Entertainment The Entertainment feature gives you access to the internal media player See section Menu Entertai
10. 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 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
11. you have on TL 6524 e 1 6 CREO 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 0 1 0 0 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 o wan wm o wl wm 0 EFIS amp EMS TL 6624 REMOTE TL 6824 Page 12 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 13 introduction TLELEKTRONIC 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 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 lin
12. 0 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 16 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 17 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 it means press the button with label Yes displayed on screen above the button Turning the INTEGRA ON Press the right hand knob to turn t
13. 65 HDG 208 IDNT KFT FREQ AC 113 09 FREQ ST 11169 NAV gt 244 SBY O 280 label NAV NO ACTIVE indicates that OBS and CDI is not valid Needle of CDI is not displayed It means that SL 30 is connected and it s sending data to the Integra but data are incomplete So you can t rely on OBS Other data are valid Page 38 TLELEKTRONIC Only magnetic heading is valid If SL 30 failed or its cabel connection the red NAV NO DATA label will appear Only valid information is actual heading because Remote compass sends actual heading information not SL 30 OBS arrow will be pointing to actual heading Navigation Section Un Tm Description of LOC Description of LOC OBS description above lu IDNT identification Tess eT of VOR Heading Bearing from the Frequency to active VOR and standby VOR station Frequency to stand by VOR Bearing from an active VOR station Glide Slope Indicator Yellow arrow in picture is just pointing to ideal glide slope determined in half of full scale Full scale represents 1 4 degree If actual glide slope is out of range the yellow arrow will disappear and red GS flag will appear above scale Actual heading Indicator TO FROM The second part of the OBS is the CDI or Course Deviation Indicator The dotted line is scale of CDI The Needle deflects left or right to indicate where Bearing from an active the course is If the needle is to the left
14. Function Enable Deact The AP is deactivated Activation of the AP must The AP is temporarily deactivated After release of the button Only is set be performed by the AP buttons on the Integra the AP will follow the last configuration Prev Act The AP is activated with the last configuration The AP is temporarily deactivated After release of the button amp Deact Next pressing will deactivate the AP the AP will follow the last configuration is set Stab Act The AP is activated and the AP will hold current The AP is temporarily deactivated After release of the button amp Deact altitude and heading the AP will hold current altitude and heading is set Hold On Function Disable Deact The AP is deactivated Activation of the AP must o reaction Only is set be performed by the Integra buttons Prev Act The AP is activated with the last configuration no reaction amp Deact Next pressing will deactivate the AP is set Stab Act The AP is activated and the AP will hold current no reaction amp Deact altitude and heading is set Page 70 Menu Entertainment About Menu Entertainment Page 71 Entertainment About amp Operation TLELEKTRONIC 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
15. G S Glideslope gl gallons GPS Global Positioning System GS Ground Speed HAL Horizontal Alarm Limit HDG Heading Page 77 TLELEKTRONIC 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 Second MSA Minimum Safe Altitude MSG Message MSL M
16. User s manual is subject to change without prior notice Page 1 Introduction TLELEKTRONIC Table of Contents Table of Contents TAO og e 2 Record OF PEVISUON M 4 Accessories and Packing EC RT OD a renee 8 Limited warranty T T atest 9 General ilc ew Uri RETE E oo e M 10 About this CS M P 11 Intesra 1ESEUD 09 COMO lis 11 Explanation f Possible LOA OD sa cde eg ees ccs A ee a C i vndis Mte ie a aaa dale a id 12 Back up System Recommendation ii 13 Explanation of Priority setting for Data Sharing NE D 14 INTEGRA wei i equ m M 15 ecd EESE 16 Power SUpply MH pc aae aeieea eo XX M Q 16 Theory OF CU AM secos idus dte adiri me enar tust dU tM cme MA nsa mu aud d MM A MI ME th 17 BASIC OPERATION sup 18 K ertercher 18 Turning the INTEGRA ON Pc td 18 Tus the INTEGRO PET C
17. abels appear TE E El Press the appropriate button for choosing controlled axis or axes Both The AP controls both axes Roll and Pitch axis Aircraft is keeping up determined heading and altitude Target heading and altitude could be determined by one of three modes Selecting of desired mode is subject of next step Roll The AP controls only Roll axis Aircraft is keeping up determined heading Target heading could be determined by one of three modes Selecting of desired mode is subject of next step Pitch The AP controls only Pitch axis Aircraft is keeping up determined altitude Target altitude could be determined by one of three modes Selecting of desired mode is subject of next step Cancel It cancels setting the AP Page 65 Autopilot TLELEKTRONIC Configuration Step 3 Selecting of navigation controls In this step you ll choose mode for controlling previously selected axis axes NOTE If you selected Both in previous step same mode for controlling both axes will be used by AP This means that you can t select e g Stabilization mode for Roll and Bugs mode for Pitch After you selected axis axes for AP operation new button labels appear Mzation tgs PENE A Stabilization The AP will be following heading and or altitude that was actual in the moment in which you pressed Stabilization button Bugs The AP will be following heading and or altitude determined by Heading bug and or Altitude Bug
18. ation 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 20 Basic Operation TLELEKTRONIC 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 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 director
19. cations 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 Page 5 Introduction Warnings Cautions amp Notes N CAUTION NOTE NOTE 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 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 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 Page 6 Introduction unam Warnings Cautions amp Notes 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 a
20. different position of boresight Press left knob and select Boresight When is displayed Set weight you can rotate with the knob and set up boresight Page 46 Menu NAV HDG pariah TLELEKTRONIC NAV Source In this menu you can choose which source of navigation you want use All this navigations are described above H Menu NAV Source e Off e VOR LOC e GPS If you choose one of the sources of navigation above label NAV HDG is displayed a little legend which source of navigation is select HSI VORADC HSI GPS Menu HDG Menu HDG Menu HDG Source navigation is OFF Source navigation is VOR LOC Source navigation is GPS Page 47 Menu NAV HDG TLELEKTRONIC BUGS BUGS Bugs are a little helping signpost which indicated parameters of Altitude Airspeed and Heading as you wish Altitude and Heading bug can be set from Menu HDG If you select ALT Bug or IAS Bug option appropriate table will appear to indicate currently adjusted value of Altitude or Speed Bug You can change the value by rotating left MenueHDG knob If you want to accept currently value press left knob If you want to disable the bug press button Disable If you wan to revert to previous setting press button Cancel HDG in this menu you can only turn on or turn off because value of heading is set in default menu Described below BUGS na ALT BUG Altitude indicator IAS BUG Speed indicator Page 48 Barometer adjustment Atmos
21. ean Sea Level mul Multicom NATNL National NAV Navigation NAVAID Navigational Aid NDB Non Directional Radio Beacon N N N M Nautical Miles RST Nearest UM 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 Page 78 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 Mer
22. ectronic 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 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 11 Introduction unam General Description Explanation of Possible Connections Here are a few Instrument connection Possibilities If you connect TL 6524 with TL 6724 you will be able to share the screen data between the two instruments l i 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
23. ege 51 hRS 51 ChEeKlieb EE 52 SHEET ed EE E E EEE E E Mu e E E Uu 53 Entertainment EE 54 Other SEUS uni li ae ee EEA A A a Saa EES 54 COn SUOMI of Ate ecc RD c ERU 59 Entert set p moer A A A A A aa 39 A o E A Deskin PN 60 PMO risa fas cous EM Pd RE NE 60 AULD OE A bM oce Tr A e n RD MD EU T MT RN RE Mp 61 Adjusting th AP TH A a a A QN 63 Steps tor configuration and switching on the Te EE 64 OW to turn Oi TEE 67 How toweadjust tie XD eot ele Giese e neue ou a iu tat ru oc SN es 68 Setting the AP via External Butt Ed sito ft I an isce teu S tl ds 69 Menu Ent rtainment tina ipod cron vb Codi eem iba enin las A AA edema Fed i AAA v ueteri died sue A AA AAA AA dh ise AAA etn AAA 71 ADD IA OS a A iia 77 Technical Parameters ERR TL LU LT 79 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 122010 New functions added Hooma Language correction Page 4 Introduction Warnings Cautions amp Notes WARNING WARNING 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 alt
24. esign of user interface you can set very easily parameters of the AP NOTE Execute the steps below in defined sequence if the AP is in off state In that case the AP will begin to control flight after you finished last step in sequence If the AP is already in on state and you want to reset its parameters then you should follow How to readjust the AP On state of the AP is indicated by AP FN button label next to the left knob label in EFIS or EFIS EMS divided screen Page 63 Autopilot TLELEKTRONIC Configuration Step 1 Access to function of the AP Switch the Integra to EFIS Screen or any split screen In EMS full screen the AP button label isn t displayed If the Towing Menu is ON and the Integra is displaying split screen EFIS EMS EFIS VOR you won t be able to access the AP setting via the Integra buttons But if the AP is already activated it will remain activated but you won t be able to access its setting via the Integra buttons The Integra displaying modes in which setting of the AP is accesible ID LOWK OBS 131 BTW S 199 DTW 2886 28 NM ALT 3768 FT SPD 495 KTS TRK 134 HDG 224 dn i EFIS screen when Towing Menu is OFF or ON EFIS GPS screen when Towing Menu is OFF Page 64 Autopilot TLELEKTRONIC Configuration Step 2 Selecting of controlled axis axes In this part you ll set the axis axes which the AP controls MET ADG Rp PS MERO Baro Press button AP New button l
25. f 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 27 Integra Operation General Description INTEGRA Operation Page 28 Integra Operation UNE Tm Screen description of complete EFIS OBS HITS Roll indicator Turn Rate Indicator Heading Bore Sight Digital Speed 440 T Roll scale Indicator E x r Digital Altitude True Indicator Airspeed SEN e l Vertical Speed Outside Indicator Temperature pte he Water Line Temperature Aux E NEEDLE c Altitude Strip Temperature Pitch ladder Reference Pressure Accelerometer Airspeed Strip 1013 Status Indicator AOA Navigation Slip Indicator Source Indicator Page 29 Integra Operation Description of Function EFIS Description of function EFIS Bore Sight The position of the Arrow indicator or Bore Sight Indicator can be controlled by turning the left knob If the Arrow turns yellow for few seconds that indicates the Arrow is in the centre position Digital speed indicator Shows you actual speed Accelerometer Vertical Acceleration Indicator Pitch ladder Is shown by white horizontal lines with a 10 degree scale 10 340 Navigation Source Indicator Shows you actual source of navigation AOA Angle of Attack Indicator HITS H
26. g Screens in which Towing Buttons are available Screen in which Towing Buttons are unavailable Towing camera camera view view Qo9 o 9 90o Q9 909 90 Page 57 inni Menu TLELEKTRONIC Other Setting If you press Horizon the Integra displays maneuver indicators Roll indicator Roll scale Pitch ladder the Water line Bore Sight By pressing Horizon again they ll disappear eRe Abs Merent Maneuver indicators hidden Maneuver indicators displayed Page 58 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 O NOTE More about SETUP menu you can find in CONFIGURATION MANUAL on the CD Page 59 ces 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 O 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
27. he 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 18 Basic Operation TLELEKTRONIC The Integra Control Panel 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 cycle between screens e scroll through menus e adjust instrument parameters and settings NOTE ALT bug HDG bug and Press baro you can use fast rotate the units will change more quickly Page 19 Basic Operation TLELEKTRONIC 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 Labels turn red to match any urgent notice appearing on the screen Data Port The INTEGRA allows the pilot to enter checklists flight plans general inform
28. he 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 Setup Power Off About Exit Menu Brightness Instruction is therein before Page 25 Page 51 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 Check 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 E Fuel Tank Guantity Check secure
29. ick 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 15 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 Supply 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 3
30. ighway In The Sky Virtual boxes which are displayed in airspace They are tracing the flight path predetermined by GPS Page 30 Integra Operation unma Description of Function EFIS Indicates the airspeed To define the airspeed limits see Configuration Manual section EFIS Range and Limits The lower white end indicates minimum flight speed in landing configuration Vso The lower green white border indicates Vs Stall Speed The upper green white border indicates maximum speed for flaps extension V pg The yellow green border indicates maximum structural cruising speed Vno The red yellow border indicates never exceed speed Vye Airspeed strip The speed is also displayed numerically in the numerical airspeed indicator The units display knots kilometres miles as determined by the user The slip skid ball works much like a standard mechanical gauge It is a visual Slip Indicator representation of lateral acceleration If the ball is within the two vertical lines then you are in coordinated flight There is the reference pressure box underneath the altitude strip in milibar torr Reference pressure or inHg Rotate the Right Knob to set the value then confirm by pressing the Knob to Set Press The Water Line Is indicated by two silver oblong bars Page 31 Integra Operation TL ELEKTRONIC Description of Function EFIS Indicates the aircraft altitude based o
31. ion 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 10 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 el
32. it 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 1100 g 2 43 Ib Weight with battery 1200 g 2 65 Ib 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 79 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 su
33. it 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 wire must be removed Cover 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 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 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 22 Basic Operation TLELEKTRONIC Battery Installation Cable for connecting INTEGRA with battery ANANA UUUUUU 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 iz Integra holder nii Page 23 Basic Operation SD card Installation SD card Installation Turn off INTEGRA Remove INTEGRA from mounting rack The slot for the SD card is situated
34. itude 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 become unsafe Use the INTEGRA at your own risk To reduce the risk of unsafe operation carefully review and understand all aspects of this User s Manual and the Flight Manual Supplement and thoroughly practice basic operation prior to actual use When in actual use carefully compare indi
35. king 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 tenere standard screen is to unplug the bus from TL 6824 EMS data TL 6624 TL 6524 EFIS data Page 14 Introduction TLELEKTRONIC General Description INTEGRA Glass Cockpit Before operation the INTEGRA please check to see if there are any parts damaged If
36. n m s or ft min as determined by user and is indicated by a Grey Vertical Flag Digital Altitude Indicator Shows you actual altitude Roll scale 120 degrees of roll each line indicates 15 degrees variation Turn Rate Indicator OBS Omni Bearing Selector When using VOR LOC as Navigation source the OBS is shown as a green ball on the Heading Tape When GPS is used as a source the ball is blue and when Navigation source is OFF OBS is not displayed Pilot sets the OBS by rotating appropriate knob external knob or knob of the Integra Page 34 Integra Operation Description of Function EFIS Heading Stabilized heading tape and digital readout Located at the top of the EFIS page the heading indicator functions much like a standard slaved directional gyro North East South and West directions are labelled on the tape N E S and W respectively The digital readout displays your current heading while the surrounding tape scrolls beneath its arrow You may set a magenta bug on this tape as a heading reminder Like a conventional gyro stabilized magnetic compass magnetic heading reacts immediately to turn rate so that heading changes are reflected immediately Roll indicator Two little arrows in the middle of the Roll Scale Page 35 Navigation Section Switching Navigation Screens TLELEKTRONIC Navigation Section If EFIS VOR LOC split sc
37. n static air pressure There are three colours on the altitude strip these colours match the colours displayed by 3D terrain Green parallel to the barrel pointer indicates that the aircraft is 100 meters or more over terrain e Yellow indicates that within a 5km range there is terrain within 100m below Altitude Strip Heini Red indicates that within a 5km range there is terrain that is higher than the aircraft s flight level The pilot must alter aircraft altitude to avoid collision The altitude strip scrolls beside the numerical readout and arrow The digital simulation of an numerical altimeter scroll up and down giving an indication of of direction and movement Thousands of feet meters are displayed using large numbers to the left while hundreds of ft m are shown in smaller numbers to the right NOTE The altitude strip only has a 5km range in front of the aircraft Page 32 Integra Operation UNE Tm Description of Function EFIS 3D Terrain Colour display This picture is a logical scheme of the colour configuration of the 3D terrain map in comparison to aircraft altitude AS RB o ae Altitude of terrain in 5km range is NOTE This information will only be shown with the installation of 3D Terrain Page 33 Integra Operation Description of Function EFIS Vertical Speed Indicator The VSI scale is at the right hand side of the screen next to the altimeter strip Vertical speed i
38. ned by navigation source GPS VOR or LOC The AP with Premium Key cannot follow flexible flight altitude which is determined by navigation source The AP controls 2 axes roll and pitch Silver Aircraft is stabilized in flight altitude and heading Moreover the AP features ability of following flight path specifying flight altitude and heading This flight path is determined by navigation source GPS VOR or LOC The AP controls 2 axes roll and pitch Page 62 Autopilot TLELEKTRONIC About Gold Aircraft is stabilized in flight altitude and heading Moreover the AP features ability of following flight path specifying flight altitude and heading This flight path is determined by navigation source GPS VOR or LOC The AP controls 3 axes roll pitch and yaw The additional yaw axis control provides optimum performance during heading corrections controlled by the AP NOTE AP is no substitute for the pilot remaining in full control of aircraft AP is only addition in piloting of the aircraft You should not engage in other activities that reduce your attention to piloting Thanks to simple but genius engineering solution using servos with magnetic clutch you can seize control of the aircraft immediately whenever your action is needed Precise setting of servos slipping is required due to setting of the right amount of transmitted torque See Configuration Manual for setting servo slipping Adjusting the AP Due to clever d
39. nment on page 71 Other setting In this menu you can turn on or turn off 3D terrain 3D terrain show you ground below you in 3D picture NOTE 3D terrain is optional function e Menu OTHER SETTING e 3D terrain ON e 3D terrain OFF e Highway ON e Highway OFF e Towing Menu ON e Towing Menu OFF 3D terrain ON turn on 3D terrain 3D terrain OFF turn off 3D terrain Highway ON turn on HITS Highway OFF turn off HITS Towing Menu ON turn on Towing Menu Towing Menu OFF turn off Towing Menu Page 54 a Meni TLELEKTRONIC Other Setting 3D terrain ON OFF 3D terrain show you ground below you in 3D picture Highway ON OFF Highway show you square on display thereby show you way Towing Menu ON OFF This feature is useful specially for towing aircraft Pilot can visually monitor the glider during towing This is possible due to switching the Integra for displaying video from rear aircraft camera To turn Towing Menu ON or OFF Press right knob and select option Other Setting then select Towing Menu OFF or Towing Menu ON Page 55 Inara Menu TLELEKTRONIC Other Setting To make this feature available If Towing Menu is ON Towing Buttons will be displayed Remember that Towing Buttons are not displayed in EMS and EFIS full screen Switch the Integra to any split screen to make Towing buttons available Towing Camera View Wenn DG forzont Towing Buttons Page 56 Integra Menu TLELEKTRONIC Other Settin
40. on the top right side of INTEGRA Now insert SD card into the slot so that the front SD card label is facing you and the label text is upside down 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 24 Slot for SD card Basic Operation Brightness SN 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 25 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 effec
41. pheric pressure could be set easily by rotating of right knob If you rotate the knob the Baro table will be displaying actual adjusted pressure You can set actual value by press of the knob Or you can just wait a few seconds and new value will be used If you press button QFE current altitude will be set to zero This option is usually used when the aircraft is on runway and you want to altitude be referenced to level of the runway If you press button 1013 25 current altitude will refer to sea level ID LOWK OBS 236 BTW 199 DTW 2887 25 NM ALT 3388 FT SPD 102 KTS TRK 238 HDG 259 80 O IAT a AUXT C j 1026 ge 20 79 R FT min LI x100 mBar 60 Page 49 Menu NAV HDG eh TL ELEKTRONIC HDG Set headings is doing in default menu Just twist with left knob and a Heading table is displayed on screen Knob label Set Edit and button labels Disable and Cancel will appear If you want to accept current value press left knob If you want to disable the bug press button Disable If you want to revert to previous setting press button Cancel BUG is set on 250 deg BUG is set on 1300 m BUG is set on 180 km h integra Menu TLELEKTRONIC Introduction Integra Menu To enter a menu just press the 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 t
42. pport SD and SDHC memory card Page 80 2010 TL elektronic ITEP RA CEIC ah SN NIETO or its subsidiaries NICURA CFIS IL 02324 USER MANUAL TLELEKTRONIC CENE TTTTTT Part Number TLD 6524X DU 001 RevE
43. r is set as CONNECTED in Setup Mode but it is not sending data That means GPS receiver is not connected actually or GPS receiver failed or its cable connection failed Only valid data displayed by the Integra actual magnetic heading pre set Heading Bug OBS aligns with Heading Bug Page 44 GPS amp MENU HDG TL ELEKTRONIC Scales of CDI for GPS E enroute T terminal A approach 5 NM 1 NM 0 3 NM RE waypoint waypoint waypoint NAV HDG For enter to navigation just press left knob with label Menu HDG 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 HDG Heading Set Bore Sight Nav Source ALT Bug IAS Bug Exit Menu Page 45 Menu NAV HDG TL ELEKTRONIC Introduction Heading Set Is used to set a magenta bug to current heading value displayed by digital readout on Heading Tape Boresight Is used to compensate for a weight displacement due to an excessive payload in order to maintain a level horizontal flight path p ou Look at the pictures take note position boresight against the water line When the boresight is at one line with water line the boresight is yellow for a little time When you move with the boresight its colour is magenta Set weight Pictures with
44. reen or EFIS GPS isn t displayed press button Screen and then press that button again now it is labeled Next Next Now when the Integra is displaying split screen you can switch between VOR LOC and GPS screen by press of the button labeled wech or a VOR ERIS ll EFIS GPS LOG O9 0 090 90 O9 0 090 90 Page 36 Navigation Section Description of VOR OBS description above Description of VOR IDNT identification of VOR Frequency to active VOR and Frequency to stand by VOR Bearing from an active VOR station Actual magnetic heading Indicator TO FROM needle of Course Deviation Indicator OBS Page 37 Bearing from the standby VOR station Heading Bearing from the standby VOR station The red NAV flag will appear here if the INTEGRA doesn t get valid data from SL 30 The second part of the OBS is the CDI or Course Deviation Indicator This dotted line is scale of CDI The Needle deflects left or right to indicate where the course is If the needle is to the left the course is to the left Full scale represents 20 degrees off course That means 10 degrees on left side and 10 degrees on right Bearing from an active VOR station Navigation Section Description of VOR All data are valid OBS 39 HDG 274 IDNT KFT FREQ AC 113 09 FREG ST 11169 NAV o 344 SBY O 280 green label VOR indicates that VOR is valid OBS and CDI is not valid OBS
45. t 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 26 Integra Operation Warning Signals Warning Signals Landing Gear is retracted Landing Gear is extended Landing Gear is retracting or extending or there is a problem with the Landing Gear Canopy is open A dangerous quantity of CO is in the cockpit Information on measured quantity is not available INTEGRA is connected to an external power supply INTEGRA s is power supply from battery 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 Lights located on the aircraft instrument panel should be viewed before landing The INTEGRA can provide a gear up voice warning i
46. t 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 73 Entertainment TLELEKTRONIC About amp Operation elapsed time of video remaining time of video Music Flight Data Exit buttons labels Opens window for selecting desired video file or folder Plays currently Stops currently Plays previous Plays next stopped video played video track track Page 74 Entertainment About amp Operation Option Music NOTE The Integra only supports MP3 audio files name of currently played track elapsed time of track loop playing mode shuffle playing mode number of currently played track in list and total number of tracks in list buttons labels PS Open V3 Play m stop Opens window for selecting desired track or folder Plays currently stopped track Stops currently played track track Page 75 Plays previous remaining time of track Flight Data Exit MM Select Plays next track Entertainment About amp Operation Option Flight Data This option soothes desire for flight info of impatient and curious passengers It displays Airspeed Altitude and Time to arrival ENJOY
47. the aircraft according to just adjusted axis axes and previously adjusted navigation control Page 68 Autopilot TLELEKTRONIC Configuration Change of navigation controls MER PDG XPTN Screen WERT Baro Press button AP FN ea wn 0 e 11 1 Then press button Control The options are same as in step Selecting of navigation controls KAL Bids Rm SE esncel After selecting desired option the button label has changed back to AP FN LEBEN RPFN een Wen Baro 4 The AP is controlling the aircraft according to just adjusted navigation control and previously adjusted axis axes Setting the AP via External Button External button makes your setting of the AP more comfortable By press of this button you can deactivate the AP activate the AP with its previous settings deactivate the AP for a while by keeping the button pressed etc See Configuration Manual for further info Ask your aircraft maintenance specialist for built in the button with appropriate and handy location Recommended place for external button is on yoke control column or on central panel Page 69 Autopilot Configuration option of Menu External Button action of the button note Before any deactivation temporary or permanent of the AP performed by the external button the AP has to be activated by the AP buttons on the Integra at first press holding down press and immediate release Hold On
48. there are damaged components please contact TL elektronic or your TL elektronic 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 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 qu
49. vionics 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 7 Introduction 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 eas
50. ws the value for the Heading bug set by the pilot Actual magnetic heading Track indicator Course Deviation Indicator CDI When a flight plan is active in the GPS the CDI indicates how far to the left or right of your selected ground course you are Bearing To Waypoint BTW Scale indicator It determines what scale CDI is using See picture on page 43 Navigation Section Description of GPS All data are valid GPS All data are valid ID LOWK OBS 163 BTW 199 OBS is indicating bearing adjusted by pilot DTW 2886 60 NM ALT 34 99 FT SPD 424 KTS TRK 166 HDG 271 Other displayed data have same meaning as data described on previous page y i I l i 2 fe BTW is indicating next destination waypoint and DTW determines its distance 1 S 1 Page 42 Navigation Section UNE Tm Description of GPS Invalid data ID OBS CDI Scale indicator Flight plan is not available Waypoints in GPS receiver are not set or GPS receiver is ID LOWK OBS 191 sending incomplete data due its settings Check settings of the GPS receiver BTW 199 DTW 2996 37 NM Invalid data displayed by the Integra ALT 3391 FT are SPD 112 KTS nio TRK 193 HDG 259 DEW CDI Scale Indicator Other displayed data have same meaning as data described on page 39 and page 40 Page 43 Navigation Section Nn Tm Description of GPS Only valid data Magnetic Heading Heading Bug GPS receive
51. y 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 Putthe 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 AN CAUTION Ensure sustaining voltage during updating if during updating fails the electric power supply the Integra can be damaged AN CAUTION Keep the flash drive connected with the Integra during updating AN 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 21 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 un
52. y 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 8 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
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