TQ Aviation KTX2.0300 EASA.AP445 MAN @ KTX2.0300 MAN Operation and lnstallation Manual Doc.-No KTX2.A-MAN lssue: 0202 ECR-No KTX2.A-ECR.0202 Date: 2019-04-17 MoC: 0 Document Release Signature Function Name Date Prepared by Uwe Mathes 2019-04-17 Checked by Florian Holzner 2o1s-04-1r i.l/ Approved by Thomas Eilers 2019-04-17 KTX2.A-MAN.0202.en.docx @TQ-SystemsGmbH.Allinformãlionconta¡nedinth¡sdocumenlshavetoþetreatedstr¡ctlyconfident¡al.
TQ Aviation KTX2.0300 EASA.AP445 MAN KTX2 Mode-S Transponder Standard KTX2-S (Standard) with ADS-B with Part-No 304110 Operation and Installation Manual KTX2.A-MAN.0202.en._FCC geändert.docx Page 2 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential. The transfer of presentations and know-how to third parties requires the prior written consent of TQ-Systems GmbH.
TQ Aviation KTX2.0300 EASA.AP445 MAN Revision List Revision Date Topic 0100 24.03.2017 Initial Release 0101 20.02.2018 Amendments for extended Squitter and maintenance 0201 10.04.2019 Change due to new microcontroller and new functionalities according to EUROCAE ED-102A / RTCA DO-260B 0202 17.04.2019 Amendment of Software License Clearing and added Cap. 10 Service Bulletins (SB) Service Bulletins must be inserted in the manual and added to this table. No SB No Rev. KTX2.A-MAN.0202.en.
TQ Aviation KTX2.0300 EASA.AP445 MAN Change History Product Revision Date 0300 09.04.2019 KTX2.A-MAN.0202.en._FCC geändert.docx Description of Change Base version for KTX2-S (Standard) with ADS-B with Part-No 304110 Page 4 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential. The transfer of presentations and know-how to third parties requires the prior written consent of TQ-Systems GmbH.
TQ Aviation KTX2.0300 EASA.AP445 MAN Table of Contents 1. General ............................................................................................................................. 7 1.1. Symbols .................................................................................................................................... 7 1.2. Abbreviations ............................................................................................................................ 8 1.3.
TQ Aviation KTX2.0300 EASA.AP445 MAN 4.4.1. Battery Warning ............................................................................................................... 38 4.4.2. Antenna Warning ............................................................................................................. 38 4.4.3. TRX Warning ................................................................................................................... 39 5. Installation ...........................................
TQ Aviation KTX2.0300 EASA.AP445 MAN 1. General This manual contains information about the physical, mechanical and electrical characteristics, installation and operation of the Mode S Transponder KTX2. 1.1. Symbols DANGER: Advices whose non-observance can cause radiation damage to the human body or ignition of combustible materials. ATTENTION: Advices whose non-observance can cause damage to the device or other parts of the equipment. or reduce the correct functionality of the device.
TQ Aviation KTX2.0300 EASA.AP445 MAN 1.2. Abbreviations Abb.
TQ Aviation KTX2.0300 EASA.AP445 MAN 1.3. Customer Support In order to facilitate a rapid handling of returned shipments, please send your request at the email address below. Additional information and FAX number can be found on the TQ Avionics web portal: www.tq-avionics.com Any suggestions for improvement welcome. Contact: info@tq-avionics.com manuals are Information on software updates are available at TQ. www.tq-avionics.com KTX2.A-MAN.0202.en._FCC geändert.
TQ Aviation KTX2.0300 EASA.AP445 MAN 1.4. Features In order to operate the Mode-S transponder it is necessary to request (in time) an ICAO 24-Bit Aircraft Address at the responsible National Aviation Authorities. The received code must be configured within the transponder (see chapter. 3.1.2 “Flight-ID (FID) & Set-Up”).
TQ Aviation KTX2.0300 EASA.AP445 MAN 2. Operation 2.1. Controls and Display on the Screen Figure 1: Display Diagram KTX2.A-MAN.0202.en._FCC geändert.docx Page 11 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential. The transfer of presentations and know-how to third parties requires the prior written consent of TQ-Systems GmbH.
TQ Aviation KTX2.0300 EASA.AP445 MAN 2.1.1. Controls Key Designation ON/OFF VFR CHANGE Function Push = ON. This switch is mechanically locked until it is pushed a second time. Activate/deactivate VFR Squawk (press shortly) Store the standby Squawk as VFR/VFRWSquawk (press button 3 s) see chapter “2.6 VFR – Squawk”. 1. Exchange of the active and standby-Squawk 2. Works as cursor back button when entering values and also for navigating backwards through the configuration menu.
TQ Aviation KTX2.0300 EASA.AP445 MAN 2.1.2.
TQ Aviation KTX2.0300 EASA.AP445 MAN 2.1.3. Operation menu structure Figure 4: Operational menu structure KTX2.A-MAN.0202.en._FCC geändert.docx Page 14 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential. The transfer of presentations and know-how to third parties requires the prior written consent of TQ-Systems GmbH.
TQ Aviation KTX2.0300 EASA.AP445 MAN 2.1.4. ON/OFF The device is switched on/off by pushing the mechanically locked key. After power up, the display appears as follows (example): Device Name -- KTX2 -Software-Version e.g. V.0101 Firmware-Version e.g. FPGA: 6.0 After approx. 2 seconds the normal operation window appears and the transponder will enter the mode ALT. If a weight on wheels switch is installed and the aircraft is on ground the mode GND will be set. No GND switch installed KTX2.A-MAN.
TQ Aviation KTX2.0300 EASA.AP445 MAN In case that multiple Flight ID’s are present, the screen will first display the selection menu for one of the Flight ID’s: Select the correct Flight ID by rotating the rotary knob to the one you chose and confirm by pushing. The screen will switch automatically to the normal operation window. 2.1.5.
TQ Aviation KTX2.0300 EASA.AP445 MAN 2.1.6. Transponder-Modes The active mode is displayed at the bottom left corner. STBY Transponder is on but does not respond to any interrogation. GND Transponder responds to Mode-S interrogations. ON Transponder responds to all interrogations, only altitude is not transmitted. ALT Transponder responds to all interrogations. During the flight the Mode ALT should always be set, unless the air traffic control gives other instructions.
TQ Aviation KTX2.0300 EASA.AP445 MAN 2.1.8. Squawk Ident (ID, SPI) On request of the air traffic control, push the ID button (when not in the STBY mode). Transmission of the ID signal will last for 18 seconds and “IDT” is displayed above the mode and left side of the Flight ID. 2.1.9. Flight/Ground Indication Aircrafts with AIR/GROUND switches display “FLY” (Flight) or “GND” (Ground) in the lower right corner. This function must be activated in the set-up procedure (see chap. 3.1.4.2).
TQ Aviation KTX2.0300 EASA.AP445 MAN 2.2. Adjustable parameters in operation mode 2.2.1. Flight ID To modify the Flight ID during operation, push the ID button for at least 3 seconds. The parameters can be adjusted in the same way like described in chapter 3.1.2. 2.2.2. Flight ID To modify the display brightness during operation, push the VFR button for at least 3 seconds.
TQ Aviation KTX2.0300 EASA.AP445 MAN 2.2.3. GNSS Data The actual GNSS data can be displayed when pushing the toggle button for at least 3 seconds: KTX2.A-MAN.0202.en._FCC geändert.docx Page 20 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential. The transfer of presentations and know-how to third parties requires the prior written consent of TQ-Systems GmbH.
TQ Aviation KTX2.0300 EASA.AP445 MAN 2.2.4. Extended Squitter The Symbols for Extended Squitter show the current operational status of ES transmission: Indication Function Description Extended Squitter on. Letter “A” appears white ADS-B out function is active and transmitting messages Extended Squitter on.
TQ Aviation KTX2.0300 EASA.AP445 MAN 3. Set-Up Figure 6: Button functions in setup-mode KTX2.A-MAN.0202.en._FCC geändert.docx Page 22 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential. The transfer of presentations and know-how to third parties requires the prior written consent of TQ-Systems GmbH.
TQ Aviation KTX2.0300 EASA.AP445 MAN Figure 7: Setup menu structure KTX2.A-MAN.0202.en._FCC geändert.docx Page 23 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential. The transfer of presentations and know-how to third parties requires the prior written consent of TQ-Systems GmbH.
TQ Aviation KTX2.0300 EASA.AP445 MAN 3.1. Entering Set Up To enter setup mode, press ID button during system startup. The following menu appears: Rotation of the rotary knob moves to the desired menu item. Pushing the rotary knob selects the desired parameter to be modified. 3.1.1. Display brightness Push the rotary knob to enter brightness sub menu. Turning the rotary knob changes the value for brightness between 1 (lowest) to 5 (highest).
TQ Aviation KTX2.0300 EASA.AP445 MAN 3.1.2. Set Flight-IDentifier (FID) Rotate the rotary knob to select Flight ID. Push the rotary knob to enter Flight ID sub menu. Select “Add” to add a Flight ID, modify to modify or delete to delete a Flight ID by pushing the rotary knob. In the “Add” sub menu the following screen appears: Press and rotate the rotary knob to enter the Flight ID. Press to jump to the next digit, rotate to select the desired character until the Flight ID is complete.
TQ Aviation KTX2.0300 EASA.AP445 MAN ICAO regulations require Mode-S data to contain a valid flight identification (FID), to ensure automatic exchange of flight plan and radar data. Commercial flights usually have their own FIDs. General aviation FIDs should be the registration letters or numbers of the aircraft. The FID must not be confused with the 24-bit Aircraft Address. The FID is left aligned and shown in green characters.
TQ Aviation KTX2.0300 EASA.AP445 MAN 3.1.3. Aircraft Address (AA) Note: Before you can enter the Aircraft Address, the Flight ID needs to be defined. Rotate the rotary knob to select Flight ID. Push the rotary knob to enter Flight ID sub menu. Select “Add” by pushing the rotary knob. KTX2.A-MAN.0202.en._FCC geändert.docx Page 27 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential.
TQ Aviation KTX2.0300 EASA.AP445 MAN In the “Add” sub menu the following screen appears: Rotate the rotary knob to enter the AA-Code submenu. Press to jump to the next digit, rotate to select the desired character until the Aircraft Address is complete. When code is complete, turn rotary knob to move cursor to “Save”, save configuration by pushing the rotary knob. Leave the menu entering the first line (“Edit FID Param.”) and by pushing the rotary knob. 3.1.4.
TQ Aviation KTX2.0300 EASA.AP445 MAN In the “Add” sub menu the following screen appears: Rotate the rotary knob and push to enter the Device Parameter Submenu. The following screen appears: Page 1 Page 2 3.1.4.1. Aircraft Category Push the rotary knob to enter the “Aircraft Category submenu. The following screen appears: Page 1 Page 2 Make the selection which fits to the category of your aircraft by rotating to the appropriate category. Confirm by pushing the rotary knob.
TQ Aviation KTX2.0300 EASA.AP445 MAN Note: The KTX2 is not yet certified for A/C FixW>5.7t, speed >250kts and helicopters (RotorCr). Therefore, these items are not yet selectable. 3.1.4.2. Ground Switch The next submenu is activates / deactivates AIR/GND switch function. YES/NO can be selected by rotating the rotary knob, push to confirm. 3.1.4.3. Speed Category In the next submenu you should select the typical cruising speed range of your aircraft.
TQ Aviation KTX2.0300 EASA.AP445 MAN 3.1.4.4. Select GNSS Device In case the KTX2’s extended squitter function is used, an appropriate WAAS GPS source needs to be connected (see chapter 5 wiring). Note: In countries and airspace, where ADS-B (out) function is mandatory (e.g. USA) full compliance with those regulations (e.g. FAA 2020 mandate) is granted with the KTX2 in connection with the NexNav Mini WAAS GPS receiver. This normally is the right choice for TC’d aircraft.
TQ Aviation KTX2.0300 EASA.AP445 MAN When settings have been done, leave the menu by moving the cursor to the upper line by rotating the rotary knob and push. 3.1.4.5. Select Length/Width After entering the “length/Width” menu, the following screen appears. The values to be entered are in meters (rounded) for example: Aircraft length is 7,5m, the entry shall be 08. Aircraft width (wingspan) is 9,4m, the entry shall be 09.
TQ Aviation KTX2.0300 EASA.AP445 MAN • • Longitudinal offset: Enter the distance in meters of the GPS antenna from the NOSE of the aircraft. Lateral offset: Enter the lateral distance of the GPS antenna from the longitudinal (Roll) axis of the aircraft. For most small aircraft “00” is correct. In case an antenna offset is applicable, the position to the left side of the aircraft will require a negative sign, to the right a positive sign.
TQ Aviation KTX2.0300 EASA.AP445 MAN 3.1.6. Factory Reset In certain cases it may be necessary to perform a factory reset. If you select “Yes” and confirm by pushing the rotary knob, the system will do a factory reset. You will be prompted to restart the transponder. 3.1.7. Test Menu The Test Menu incorporates the following submenus: KTX2.A-MAN.0202.en._FCC geändert.docx Page 34 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential.
TQ Aviation KTX2.0300 EASA.AP445 MAN 3.1.7.1. Altitude offset 3.1.7.2. Test Mode The Test Mode displays three parameters: • Operating voltage (Battery) • DC Converter voltage • Altitude (in feet) 3.1.7.3. Device Info The submenu “Device Info” displays the checksum of the software / firmware and the serial number of the device. KTX2.A-MAN.0202.en._FCC geändert.docx Page 35 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential.
TQ Aviation KTX2.0300 EASA.AP445 MAN 4. Errors and Warnings The KTX2 distinguishes 3 types of anomalies: • Warnings • Setup Errors • Elementary Function Errors 4.1. Setup Error If no FID-Code (Flight ID) and the corresponding Aircraft Address (AA-Code) is entered or uncomplete, the following displays will appear after switching on the transponder: Enter appropriate FID and AA-Code in accordance with chapters 3.1.2 and 3.1.3.
TQ Aviation KTX2.0300 EASA.AP445 MAN 4.2.1. Error FPGA Severe failure. No access to FPGA. Send Unit for servicing. 4.2.2. Internal Communication failure Severe failure. Send Unit for servicing. 4.2.3. Do System Restart Switch device off and on again 4.3. General Failure No output of transponder. Severe failure. Check environment. If no root cause can be discovered, send unit for servicing. 4.3.1. CRC Failure KTX2.A-MAN.0202.en._FCC geändert.docx Page 37 of 49 © TQ-Systems GmbH.
TQ Aviation KTX2.0300 EASA.AP445 MAN Data from GPS source not sufficient (no or not enough satellites) 4.4. Warnings 4.4.1. Battery Warning In case the on board voltage falls below 11VDC, the following warning appears: Take appropriate measures before the unit fails due to low voltage. The KTX2 is designed to operate above 9 VDC. Do not operate the unit below 9 volts. 4.4.2.
TQ Aviation KTX2.0300 EASA.AP445 MAN 4.4.3. TRX Warning In case of weak transmitter signal, the following screen appears: Weak transmitter power – Output power limited. Degrading Failure. Check antenna installation including cable, plugs etc. In order to be serviced, a defective transponder needs to be shipped to the nearest service station. For addresses see the TQ General Aviation website: https://www.tq-general-aviation.com/en/Service KTX2.A-MAN.0202.en._FCC geändert.
TQ Aviation KTX2.0300 EASA.AP445 MAN 5. Installation 5.1. Equipment Connections 5.1.1. Electrical Connections The 15pin D-SUB connector at the rear side of the unit includes all electrical connections, except for the antenna. The plus cable must be protected with a 3A slow blow fuse! 5.1.2. Mutual Suppression Other equipment on board (e.g. DME) the transponder.
TQ Aviation KTX2.0300 EASA.AP445 MAN Connect the static air connection on the back of the transponder to the static port and ensure a tight connection with a suitable hose clamp. 5.1.5. Interface A GPS source can be connected to the serial interface (RS232) providing GPS position data (Extended Squitter) for use of ADS-B out. Requirements: • Required GPS hardware: o NexNav Mini (Part-No. 21.000) which turns the units into FAA 2020 mandate compliant device as required for TC’d aircraft.
TQ Aviation KTX2.0300 EASA.AP445 MAN 5.2. Wiring 5.2.1. Conductor Cross Section Power Supply (Power, GND): Signals: AWG20 (0,62 mm²) AWG22 (0,38 mm²) The conductors must be approved for aircraft use. Recommended Quality: MIL-Spec 22759/34, (Spec 55) 20AWG / 22AWG Crimped D-Sub connector is always preferred against soldered connectors. Original TQ harness comply with common aviation wiring standards. Consult your approved aviation shop for installation details. 5.2.2.
TQ Aviation KTX2.0300 EASA.AP445 MAN 6. Drawings Figure 9: Dimensions of KTX2-S Standard round format KTX2.A-MAN.0202.en._FCC geändert.docx Page 43 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential. The transfer of presentations and know-how to third parties requires the prior written consent of TQ-Systems GmbH.
TQ Aviation KTX2.0300 EASA.AP445 MAN 7. Technical Data 7.1. General Designation Authorization EASA.21O.10069784 Certification ETSO-C112d / TSO-C112d ETSO-C88a / TSO-C88a ETSO-C166b / TSO-C166b Compliance RTCA DO-181E /. ED-73E / Level 2els,Class 1 RTCA DO-178C/ ED-12C Level D RTCA DO-254 / ED80 Level C RTCA DO-160G / ED-14G RTCA DO-260B / ED102A Class B1S SAE AS8003 FCC ID: 2ANFF-KTX2S Dimensions KTX2 Weight Mounting Temperature ranges: Operation Storage MAX. flight level 63 x 62 x 149 (2.
TQ Aviation KTX2.0300 EASA.AP445 MAN 7.2. Transmitter - Receiver TRANSMITTER Receiver Characteristics: Sensitivity Reply transmission frequency RF Peak Power Output Squitter RF input power level resulting in a 90 % reply rate: MTL for ATCRBS and ATCRBS/Mode S AllCall interrogations: -74dBm ±3dB. MTL for Mode S interrogations: -74dBm ± 3dB. 1090 ± 1MHz ≥ 24dBW (250 W) at antenna base (with maximum cable attenuation of 1,5dB) Transmitted at random intervals uniformly distributed over the range from 0.
TQ Aviation KTX2.0300 EASA.AP445 MAN 8. FCC related issues 8.1. Radiofrequency radiation exposure Information: This transponder complies with FCC radiation exposure limits set forth for an uncontrolled environment. This transponder should be installed and operated with minimum distance of 200 mm between the radiator and your body. This transmitter must not be co-located or operating in conjunction with any other antenna or transmitter. 8.2.
TQ Aviation KTX2.0300 EASA.AP445 MAN 9. Maintenance 9.1. Periodic Maintenance The KTX2 Mode-S Transponder has been designed and manufactured to allow “on condition maintenance”. This means that there are no periodic service requirements necessary to maintain continued airworthiness, and no maintenance is required as long as it does properly perform its intended function. When service is required, a complete performance test shall be accomplished following any repair action.
TQ Aviation KTX2.0300 EASA.AP445 MAN 10. Software License Conformity Licensing conditions for Software which are developed or sold by the TQ Group companies, may contain free software components and open source software components. Specific software licensing conditions apply for these components. The license conditions which are relevant for the respective product can be found in the product documentation (e. g. order confirmation, product description, specification).
TQ Aviation KTX2.0300 EASA.AP445 MAN TQ-Systems GmbH Support E-mail: support.ktx@tq-group.com Internet: www.tq-avionics.com KTX2.A-MAN.0202.en._FCC geändert.docx Page 49 of 49 © TQ-Systems GmbH. All information contained in this documents have to be treated strictly confidential. The transfer of presentations and know-how to third parties requires the prior written consent of TQ-Systems GmbH.
