FCC ID: 2ANFF-KTX2S KTX2-S

TQ Aviation KTX2.0300 EASA.AP445 MAN

@

KTX2.0300 MAN Operation and lnstallation Manual Doc.-No lssue:

ECR-No Date:

MoC:

KTX2.A-MAN 0202 KTX2.A-ECR.0202 2019-04-17 0 Document Release Function Name Date Signature Prepared by Uwe Mathes 2019-04-17 Checked by Florian Holzner 2o1s-04-1r i.l/

Approved by Thomas Eilers 2019-04-17

)rVW*

KTX2.A-MAN.0202.en.docx

@TQ-SystemsGmbH.Allinformlioncontanedinthsdocumenlshavetoetreatedstrctlyconfidental.Thelransferof presenlationsandknow-howtothrdparlies requres the prior wrlten consent of TO-Systems GmbH. Page 1 of49 TQ Aviation KTX2.0300 MAN EASA.AP445 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 gendert.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 MAN EASA.AP445 Revision List Revision Date Topic 0100 0101 0201 24.03.2017 Initial Release 20.02.2018 Amendments for extended Squitter and maintenance 10.04.2019 Change due to new microcontroller and new functionalities ac-

cording 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. Release date Date Added Name KTX2.A-MAN.0202.en._FCC gendert.docx Page 3 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 MAN EASA.AP445 Change History Product Revision Date Description of Change 0300 09.04.2019 Base version for KTX2-S (Standard) with ADS-B with Part-No 304110 KTX2.A-MAN.0202.en._FCC gendert.docx 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 MAN EASA.AP445 Table of Contents 1. General ............................................................................................................................. 7 1.1. Symbols .................................................................................................................................... 7 1.2. Abbreviations ............................................................................................................................ 8 1.3. Customer Support ..................................................................................................................... 9 1.4. Features .................................................................................................................................. 10 2. Operation ................................................................................................................................ 11 2.1. Controls and Display on the Screen ........................................................................................ 11 Controls ........................................................................................................................... 12 2.1.1. Indications ....................................................................................................................... 13 2.1.2. Operation menu structure ................................................................................................ 14 2.1.3. 2.1.4. ON/OFF ........................................................................................................................... 15 Adjusting the Squawk ...................................................................................................... 16 2.1.5. Transponder-Modes ........................................................................................................ 17 2.1.6. VFR Squawk ................................................................................................................ 17 2.1.7. 2.1.8. Squawk Ident (ID, SPI) .................................................................................................... 18 2.1.9. Flight/Ground Indication ................................................................................................... 18 2.2. Adjustable parameters in operation mode ............................................................................... 19 Flight ID ........................................................................................................................... 19 2.2.1. 2.2.2. Flight ID ........................................................................................................................... 19 GNSS Data ...................................................................................................................... 20 2.2.3. 2.2.4. Extended Squitter ............................................................................................................ 21 3. Set-Up ..................................................................................................................................... 22 3.1. Entering Set Up ....................................................................................................................... 24 Display brightness ........................................................................................................... 24 3.1.1. 3.1.2. Set Flight-IDentifier (FID) ................................................................................................. 25 3.1.2.1. Multiple Flight IDs and Aircraft addresses ....................................................................... 26 3.1.3. Aircraft Address (AA) ....................................................................................................... 27 3.1.4. Device Parameter ............................................................................................................ 28 3.1.4.1. Aircraft Category.............................................................................................................. 29 3.1.4.2. Ground Switch ................................................................................................................. 30 3.1.4.3. Speed Category .............................................................................................................. 30 3.1.4.4. Select GNSS Device ....................................................................................................... 31 3.1.4.5. Select Length/Width ........................................................................................................ 32 3.1.4.6. GNSS Antenna Offset ..................................................................................................... 32 3.1.5. Modify VFR ...................................................................................................................... 33 Factory Reset .................................................................................................................. 34 3.1.6. 3.1.7. Test Menu ....................................................................................................................... 34 3.1.7.1. Altitude offset ................................................................................................................... 35 3.1.7.2. Test Mode ....................................................................................................................... 35 3.1.7.3. Device Info ...................................................................................................................... 35 4. Errors and Warnings ............................................................................................................... 36 4.1. Setup Error .............................................................................................................................. 36 4.2. Critical Errors .......................................................................................................................... 36 Error FPGA ...................................................................................................................... 37 4.2.1. Internal Communication failure ........................................................................................ 37 4.2.2. 4.2.3. Do System Restart .......................................................................................................... 37 4.3. General Failure ....................................................................................................................... 37 4.3.1. CRC Failure ..................................................................................................................... 37 4.4. Warnings ................................................................................................................................. 38 KTX2.A-MAN.0202.en._FCC gendert.docx Page 5 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 MAN EASA.AP445 Battery Warning ............................................................................................................... 38 4.4.1. Antenna Warning ............................................................................................................. 38 4.4.2. TRX Warning ................................................................................................................... 39 4.4.3. 5. Installation ............................................................................................................................... 40 5.1. Equipment Connections .......................................................................................................... 40 5.1.1. Electrical Connections ..................................................................................................... 40 5.1.2. Mutual Suppression ......................................................................................................... 40 Ground Switch ................................................................................................................. 40 5.1.3. Static Air Port .................................................................................................................. 40 5.1.4. 5.1.5. Interface .......................................................................................................................... 41 5.2. Wiring ...................................................................................................................................... 42 5.2.1. Conductor Cross Section ................................................................................................. 42 5.2.2. Wiring Scheme ................................................................................................................ 42 6. Drawings ................................................................................................................................. 43 7. Technical Data ........................................................................................................................ 44 7.1. General ................................................................................................................................... 44 7.2. Transmitter - Receiver ............................................................................................................. 45 8. FCC related issues .................................................................................................................. 46 8.1. Radiofrequency radiation exposure Information: ..................................................................... 46 8.2. Notice ...................................................................................................................................... 46 8.3. Compliance ............................................................................................................................. 46 8.4. Modifications ........................................................................................................................... 46 9. Maintenance ........................................................................................................................... 47 9.1. Periodic Maintenance .............................................................................................................. 47 9.2. Repair ..................................................................................................................................... 47 9.3. Cleaning .................................................................................................................................. 47 10. Software License Conformity ................................................................................................... 48 List of Figures Figure 1: Display Diagram .................................................................................................................. 11 Figure 2: Controls .............................................................................................................................. 12 Figure 3: Indicators ............................................................................................................................ 13 Figure 4: Operational menu structure ................................................................................................. 14 Figure 5: Extended Squitter ............................................................................................................... 21 Figure 6: Button functions in setup-mode ........................................................................................... 22 Figure 7: Setup menu structure .......................................................................................................... 23 Figure 8: Wiring ................................................................................................................................. 42 Figure 9: Dimensions of KTX2-S Standard round format.................................................................... 43 Figure 10: Technical Data .................................................................................................................. 44 Figure 11: Transmitter receiver .......................................................................................................... 45 KTX2.A-MAN.0202.en._FCC gendert.docx Page 6 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 MAN EASA.AP445 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 dam-

age to the human body or ignition of combustible materi-

als. 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. INFORMATION KTX2.A-MAN.0202.en._FCC gendert.docx Page 7 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 MAN EASA.AP445 1.2. Abbreviations SPI AA AC Abb. Meaning Explanation FID Flight ID Special Position Identifica-

tion (ID) Flightplan Number or if not assigned Regis-

tration Number of aircraft Activation on request by controllers Squawk Ident, transmits SPI Pulse for 18 seconds, which highlights the respective traffic item on the controllers radar screen Aircraft Address Assigned ICAO 24 bit address Aircraft Category Defines aircraft type into specific catego-

ries RI Reply Information Classified air speed ADS-B Automatic Dependent Sur-

veillance Broadcast

-

KTX2.A-MAN.0202.en._FCC gendert.docx Page 8 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 MAN EASA.AP445 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 gendert.docx Page 9 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 MAN EASA.AP445 1.4. Features In order to operate the Mode-S transponder it is necessary to re-

quest (in time) an ICAO 24-Bit Aircraft Address at the responsible National Aviation Authorities. The received code must be config-

ured within the transponder (see chapter. 3.1.2 Flight-ID (FID) &

Set-Up). Class 1 Level 2els Non-Diversity Mode-S-Transponder for ground based inter-

rogations at 1030 MHz and response at 1090 MHz Replies to Secondary Radar Interrogations o Mode-A replies with a Squawk (one of 4096 possible Codes; e.g. flight plan number, Squawk assigned by a Controller or the VFR Squawk). o Mode C replies, including Encoded Flight Level. o Mode S replies, including Aircraft Address and Flight Level. o Event Squitter, containing Identification Information. o Extended Squitter, including position data. IDENT capability for activating the Special Position Identification- Pulse (SPI) for 18 seconds, which is requested by the Controller Squawk Ident Maximum flight level 30 000ft; maximum airspeed 250kt Display information contains Squawk code, mode of operation and pressure alti-

tude. Temperature compensated high precision piezo-resistive pressure sensor RS-232 data port enabling connection with mutual suppression and On the Ground (weight on wheels) inputs. In addition, an appropriate GPS receiver for extended squitter can be connected. 8 storable entries for AA-/AC-Code, FID, Ground-Switch support, RI-Code. KTX2.A-MAN.0202.en._FCC gendert.docx Page 10 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 MAN EASA.AP445 2. Operation 2.1. Controls and Display on the Screen Figure 1: Display Diagram KTX2.A-MAN.0202.en._FCC gendert.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 MAN EASA.AP445 2.1.1. Controls Key Designation Function ON/OFF Push = ON. This switch is mechanically locked until it is pushed a second time. VFR Activate/deactivate VFR Squawk

(press shortly) Store the standby Squawk as VFR/VFRW-

Squawk (press button 3 s) see chapter 2.6 VFR Squawk. CHANGE 1. Exchange of the active and standby-Squawk 2. Works as cursor back button when entering values and also for navigating backwards through the con-

figuration menu. IDENT Squawk Ident, sends Ident marking (SPI) for 18s (in normal mode) see chapter. 2.9 Flight- ID (FID) &

Set-Up MODE Select Transponder-Mode ACS, A-S or Standby (see chapter 2.4 Transponder-

Modes) Rotary knob 1. Enter values at current cursor position, select op-

tions; set standby Squawk 2. Works as cursor forward button when entering values and also for navigating forward through the configuration menu. Figure 2: Controls KTX2.A-MAN.0202.en._FCC gendert.docx Page 12 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 MAN EASA.AP445 2.1.2. Indications Indication Meaning Remark Appears per reply Appears per reply Appears at every addressed reply Status of Extended Squitter trans-

mission Transponder is transmitting Mode-A/C Replies on Inter-

rogations Transponder is transmitting Mode-S Replies on Inter-

rogations Transponder is locked by a ground station and will be directly addressed Extended Squitter Active Squawk Battery power too low Blinking Transmits IDENT- Marking ID (Squawk Ident) has been pressed active for 18s Flight Level Flight Level (in 100ft steps) Mode display

(STBY, ON, GND, ALT) see chapter. 2.1.6 Transponder-

Modes Standby-Squawk Can be changed with active Squawk by pushing the UP/DOWN

(toggle) button Figure 3: Indicators KTX2.A-MAN.0202.en._FCC gendert.docx Page 13 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 2.1.3. Operation menu structure Figure 4: Operational menu structure KTX2.A-MAN.0202.en._FCC gendert.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 MAN EASA.AP445 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 transpond-

er 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 GND-switch installed, on GND KTX2.A-MAN.0202.en._FCC gendert.docx Page 15 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 MAN EASA.AP445 In case that multiple Flight IDs are present, the screen will first display the selection menu for one of the Flight IDs:

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. Adjusting the Squawk When pushing the rotating knob in the normal operating mode, the first number of the stand-

by squawk turns green, and can be adjusted by rotating the rotary knob. Pushing the rotary knob will save the selected number and jump to the next digit which also will turn green dur-

ing adjustment. Continue with the remaining numbers in this way until the desired squawk is set. With the toggle button you can turn the stand-by squawk into the active squawk. The active squawk is always on the top line. KTX2.A-MAN.0202.en._FCC gendert.docx Page 16 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 MAN EASA.AP445 2.1.6. Transponder-Modes The active mode is displayed at the bottom left corner. STBY GND ON Transponder is on but does not respond to any interrogation. Transponder responds to Mode-S interrogations. Transponder responds to all interrogations, only altitude is not transmit-

ted. ALT Transponder responds to all interrogations. During the flight the Mode ALT should always be set, unless the air traffic control gives other instructions. While rolling on the ground the transponder should be set to GND, unless the installation in-

cludes a weight on wheels switch. In this case, the mode changes automatically. The Mode-selection is done by (repeatedly) pushing the MDE button. To enable or disable the Extended Squitter, press the MDE button for more than 3 seconds. 2.1.7. VFR Squawk The factory setting of the VFR transponder code is 7000. The VFR transponder code howev-

er can be defined in accordance with local requirements, see setup menu chapter 3.1.5. To activate the VFR-Squawk push the VFR button. VFR is then indicated on the display as the active squawk. KTX2.A-MAN.0202.en._FCC gendert.docx Page 17 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 MAN EASA.AP445 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). When this function is not activated, there are no indications on the display and modes must be manually selected in accordance with chapter 2.1.6. KTX2.A-MAN.0202.en._FCC gendert.docx Page 18 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. 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 sec-

onds. The menu appears, brightness can be adjusted by turning and pushing the rotary knob in the same way as described in setup menu (see chap. 2.1.1). KTX2.A-MAN.0202.en._FCC gendert.docx Page 19 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 2.2.3. GNSS Data The actual GNSS data can be displayed when pushing the toggle button for at least 3 sec-

onds:

KTX2.A-MAN.0202.en._FCC gendert.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 MAN EASA.AP445 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. Letter A appears yellow ADS-B out function is active but not transmitting messages Extended Squitter on Letter A appears red ADS-B out function is active and transmitting type ZERO position mes-

sages or no position messages due to missing position data (longitude, alti-

tude, latitude) Extended Squitter off Letter A disappears No transmitting data Figure 5: Extended Squitter KTX2.A-MAN.0202.en._FCC gendert.docx Page 21 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 MAN EASA.AP445 3. Set-Up Figure 6: Button functions in setup-mode KTX2.A-MAN.0202.en._FCC gendert.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 MAN EASA.AP445 Figure 7: Setup menu structure KTX2.A-MAN.0202.en._FCC gendert.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 MAN EASA.AP445 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). When selection is done, turn rotary knob to move cursor to Adjust Brightness. and leave menu by pushing the rotary knob. KTX2.A-MAN.0202.en._FCC gendert.docx Page 24 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 MAN EASA.AP445 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. When selection is done, turn rotary knob to move cursor to Save, save configuration by pushing the rotary knob. Leave the menu entering the first line (Edit FID Parameter) and by pushing the rotary knob. KTX2.A-MAN.0202.en._FCC gendert.docx Page 25 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 MAN EASA.AP445 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. The FID may not contain blanks however the non-used most right char-

acters must be blank. The FID must start with the nationality code. Enter FID left-aligned, without any blanks or dashes (!), e.g. DENWS for the marking D-ENWS. The last remaining digits shall be filled with blanks. FID containing blanks characters are invalid. Missing FID disables mode-S operation and A/C-mode only will be engaged. See chapter 4 Self-Test, Errors and Warnings 3.1.2.1. Multiple Flight IDs and Aircraft addresses In case, the KTX2 transponder is used for multiple aircraft (e.g. in a portable station as used in hot-air/gas filled balloons), up to eight FIDs can be stored in the KTX2 memory. To every Flight ID, of course the appropriate Aircraft Address must be assigned in the same way than for the use of one FID only. In case multiple FIDs are stored in the memory, the KTX2 will prompt you to select one of the stored FIDs each time it is turned on, before it goes into normal operating mode:

Further Flight IDs are to be stored in the same way, like under chapter 3.1.2 If all eight possible IDs have been stored, the following message appears:

KTX2.A-MAN.0202.en._FCC gendert.docx Page 26 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 3.1.3. 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 gendert.docx Page 27 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 MAN EASA.AP445 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. Device Parameter The submenu "Device Parameter" can also be accessed via the submenu "Flight ID":

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 gendert.docx Page 28 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 MAN EASA.AP445 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. Leave the menu in the usual way. KTX2.A-MAN.0202.en._FCC gendert.docx Page 29 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 MAN EASA.AP445 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 se-

lected 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. Select the appropriate value for your aircraft by rotating the rotary knob and push to confirm. Leave the menu by moving the cursor to the upper line by rotating the rotary knob and push. KTX2.A-MAN.0202.en._FCC gendert.docx Page 30 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 MAN EASA.AP445 3.1.4.4. Select GNSS Device In case the KTX2s 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 compli-

ance 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 TCd aircraft. Other aircraft voluntarily equipped with ADS-B like experimentals, gliders, ultralights etc. may be equipped with an appropriate low-cost WAAS GPS source. It is encouraged to use only GPS receivers recommended by TQ. After jump to the Select GNSS Device, the following screen appears:

If no WAAS GPS is connected, select No GNSS Device. If a NexNav mini is connected, select NexNav mini Approved Device shall be selected, if a recommended WAAS GPS source capable of the GPRMC-sentence (as defined in the NMEA 0183 protocol) which contains the position information as well as velocity, track, date and time is used. In the Approved device menu, there is another submenu, where the appropriate Baud Rate for the GNSS device can be selected:

KTX2.A-MAN.0202.en._FCC gendert.docx Page 31 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 MAN EASA.AP445 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 09.4 When the correct value has been entered, leave the menu by moving the cursor to the upper line by rotating the rotary knob and push. 3.1.4.6. GNSS Antenna Offset Within the antenna offset menu, the longitudinal and lateral position of the GPS Antenna is to be entered. While mainly important for large aircraft, the values can be entered for small air-

craft as well. KTX2.A-MAN.0202.en._FCC gendert.docx Page 32 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 MAN EASA.AP445 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. When the correct value has been entered, leave the menu by moving the cursor to the upper line by rotating the rotary knob and push. 3.1.5. Modify VFR In setup mode, move to Modify VFR by rotating the rotary knob and push to enter the submenu. The following menu appears:

Pushing and rotating the rotary knob selects and modifies the digits. Note:

Make sure, that you enter the correct VFR Squawk for the particular country where your air-

craft is operated. Examples:

Germany: VFR Squawk = 7000 USA: VFR Squawk = 1200 KTX2.A-MAN.0202.en._FCC gendert.docx Page 33 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 MAN EASA.AP445 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 gendert.docx Page 34 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 MAN EASA.AP445 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 gendert.docx Page 35 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 MAN EASA.AP445 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. Note:

As long no FID / AA is set, the transponder will operate in A/C mode only. 4.2. Critical Errors In case a critical error is present, the following messages can appear:

KTX2.A-MAN.0202.en._FCC gendert.docx Page 36 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 MAN EASA.AP445 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 dis-

covered, send unit for servicing. 4.3.1. CRC Failure KTX2.A-MAN.0202.en._FCC gendert.docx Page 37 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 MAN EASA.AP445 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. Antenna Warning In case of bad antenna adaption or antenna failure, the following message appears:

Check your antenna installation (cable, connectors etc.) to resolve the problem before next flight. KTX2.A-MAN.0202.en._FCC gendert.docx Page 38 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 MAN EASA.AP445 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 gendert.docx Page 39 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 MAN EASA.AP445 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 connec-

tions, 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) may transmit in the same frequency band as the transponder. If such a device is installed a single wire bus (Suppression = active at

+12V) shall be installed in order to protect the receiving parts of the different devices from in-band transmissions. Mutual suppression is a pulse that is sent to the other equipment to suppress transmis-

sion of a competing transmitter for the duration of the pulse train transmission. The tran-

sponder transmission may be suppressed by an external source and vice versa. To activate mutual suppression the SUPP_I/O requires a +12V source from the other equipment. Note:

All equipment connected to the suppression line must be re-inspected and reapproved before operation from a qualified avionic technician. Use shielded line. 5.1.3. Ground Switch If a Ground-Switch is connected (and activated in the Setup), the transponder is enabled to distinguish between weight-on-wheel (On the Ground) and (In-Flight) conditions. In the weight-on-wheel condition the transponder automatically enters the Standby mode. In order to complete this installation the input FLY-GND must be connected to a switch, which connects the input with GND in case there is weight on wheels, or remains open during flight. This option must additionally be activated in the Setup. For details on configuration please refer to chapter 3.1.4.2. 5.1.4. Static Air Port KTX2.A-MAN.0202.en._FCC gendert.docx Page 40 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 MAN EASA.AP445 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 man-

date compliant device as required for TCd aircraft. or o Standard NMEA0183 RMC data stream including the RMC-sub-format

(4800/9600/38400 Baud). GPS hardware needs to be connected to pins 2 and 13. Power supply needs to be provided separately considering the required operating voltage for the GPS hardware. Note:

For Connection to the NexNav Mini, a proprietary cable is available from TQ. Please contact you dealer for more information. If a standard NMEA0183 WAAS GPS source is sufficient for your aircraft (LSA, Ex-

perimental, Ultralight etc.) you should consider recommended brands by TQ to avoid incompatibilities or malfunctions. The WAAS GPS hardware used needs to be selected in the setup menu (see chap. 3.1.4.4). KTX2.A-MAN.0202.en._FCC gendert.docx Page 41 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 MAN EASA.AP445 5.2. Wiring 5.2.1. Conductor Cross Section Power Supply (Power, GND):

Signals:

AWG20 (0,62 mm) AWG22 (0,38 mm) 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 har-

ness comply with common aviation wiring standards. Consult your approved aviation shop for installation details. 5.2.2. Wiring Scheme Figure 8: Wiring KTX2.A-MAN.0202.en._FCC gendert.docx Page 42 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 MAN EASA.AP445 6. Drawings Figure 9: Dimensions of KTX2-S Standard round format KTX2.A-MAN.0202.en._FCC gendert.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 MAN EASA.AP445 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 63 x 62 x 149 (2.48 x 2.44 x 5.86) pure housing Weight KTX2 0.381 kg Mounting KTX2: cut-out 57 mm (2) Temperature ranges:

Operation Storage

-20 C to +55 C

-55 C to +85 C MAX. flight level 30 000ft Vibration DO-160G, Cat. S, Vibration Curve M Humidity RTCA DO-160G, Cat. A Shock operation 6G 20G crash safety RTCA DO-160F ENV. CAT. Power supply Power consumption

[C4Z]CAB[SM]XXXXXXZ[BBB][AC]TTB[B2F2]XXAX 9 VDC to 33VDC (test @ 12VDC) depending on the No of requests = 0.2 to 1.0A Illumination 0.02A Fuse External fuse required: 3A, slow-blow Compass security distance 300 mm Figure 10: Technical Data KTX2.A-MAN.0202.en._FCC gendert.docx Page 44 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 MAN EASA.AP445 7.2. Transmitter - Receiver TRANSMITTER Receiver Characteristics:

RF input power level resulting in a 90 % reply rate:

MTL for ATCRBS and ATCRBS/Mode S All-

Call interrogations: -74dBm 3dB. Sensitivity

MTL for Mode S interrogations: -74dBm 3dB. Reply transmission frequency 1090 1MHz RF Peak Power Output 24dBW (250 W) at antenna base (with maximum cable attenuation of 1,5dB) Squitter Transmitted at random intervals uniformly distributed over the range from 0.8 to 1.2 seconds, full self- veri-

fication of data and occurrence RECEIVER ICAO 24-bit Aircraft Address (Hex-Code) Aircraft Address as assigned by National Aviation Author-

ity FID Flight ID: Flight Plan call sign or aircraft registration marking Pressure Altitude Up to 30 000ft in 25ft increments in-flight / on-ground Flight Status Reports the available data and means by which the transponder can report. Figure 11: Transmitter receiver KTX2.A-MAN.0202.en._FCC gendert.docx Page 45 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 MAN EASA.AP445 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. Notice This transponder has been tested and found to comply with the limits for a Class B digital device, pursuant to Part 15 of the FCC Rules. These limits are designed to provide reasona-

ble protection against harmful interference in a residential installation. This transponder gen-

erates, uses and can radiate radio frequency energy and, if not installed and used in accord-

ance with the instructions, may cause harmful interference to radio communications. Howev-

er, there is no guarantee that interference will not occur in a particular installation. If this equipment does cause harmful interference to radio or television reception, which can be de-

termined by turning the equipment off and on, the user is encouraged to try to correct the in-

terference by one or more of the following measures:

Reorient or relocate the receiving antenna. Increase the separation between the equipment and receiver. Connect the equipment into an outlet on a circuit different from that to which the re-

ceiver is connected. Consult the dealer or an experienced radio/TV technician for help. 8.3. Compliance Notice: This device complies with Part 15 of the FCC Rules and with Industry Canada li-

cence-exempt RSS standard(s). Operation is subject to the following two conditions:

(1)

(2) this transponder may not cause harmful interference, and this transponder must accept any interference received, including interference that may cause undesired operation. 8.4. Modifications Note:

Changes or modifications made to this transponder not expressly approved by TQ-Systems GmbH may void the FCC authorization to operate this equipment. KTX2.A-MAN.0202.en._FCC gendert.docx Page 46 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 MAN EASA.AP445 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. Repairs shall only be carried out in accordance with TQ-Systems GmbH service procedures. 9.2. Repair Only exchange and flat repair of the equipment is permitted. In case of equipment malfunc-

tion, the unit must be sent to the manufacturer. Refer to section 1.2 Customer Service. 9.3. Cleaning Clean the display only with, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. KTX2.A-MAN.0202.en._FCC gendert.docx Page 47 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 MAN EASA.AP445 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 li-

censing 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). Information to TQ Systems software licenses can be found under https://www.tq-group.com/en/Licensing-conditions-for-Software For the Mode S Transponder KTX2 a software license clearing has been established in the TQ Systems license conformity review for the following. Zlib MIT BSD-3-Clause BSD-style BSD WebM Freeware ATT-style GPL-3.0+-with-GCC-exception TQSSLAv1.0.2 KTX2.A-MAN.0202.en._FCC gendert.docx Page 48 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 MAN EASA.AP445 TQ-Systems GmbH Support E-mail: support.ktx@tq-group.com Internet:

www.tq-avionics.com KTX2.A-MAN.0202.en._FCC gendert.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.

Test report no.: 1-8178/19-01-02_AnnexB Annex B This test report annex is electronically signed and valid without handwritten signature. For verification of the electronic signatures, the public keys can be requested at the testing laboratory. Test report annex authorized:

Karsten Geraldy Radio Communications & EMC Lab Manager CTC advanced GmbH Page 1 of 8 Test report no.: 1-8178/19-01-02_AnnexB Internal photos of the EUT Photo 1:

Photo 2:

CTC advanced GmbH Page 2 of 8 Test report no.: 1-8178/19-01-02_AnnexB Photo 3:

Photo 4:

CTC advanced GmbH Page 3 of 8 Test report no.: 1-8178/19-01-02_AnnexB Photo 5:

Photo 6:

CTC advanced GmbH Page 4 of 8 Test report no.: 1-8178/19-01-02_AnnexB Photo 7:

Photo 8:

CTC advanced GmbH Page 5 of 8 Test report no.: 1-8178/19-01-02_AnnexB Photo 9:

Photo 10:

CTC advanced GmbH Page 6 of 8 Test report no.: 1-8178/19-01-02_AnnexB Photo 11:

Photo 12:

CTC advanced GmbH Page 7 of 8 Test report no.: 1-8178/19-01-02_AnnexB Document histor y Version Applied changes Initial release Date of release 2019-04-05 CTC advanced GmbH Page 8 of 8

Test report no.: 1-8178/19-01-02_AnnexA Annex A This test report annex is electronically signed and valid without handwritten signature. For verification of the electronic signatures, the public keys can be requested at the testing laboratory. Test report annex authorized:

Karsten Geraldy Radio Communications & EMC Lab Manager CTC advanced GmbH Page 1 of 5 Test report no.: 1-8178/19-01-02_AnnexA External photos of the EUT Photo 1:

Photo 2:

CTC advanced GmbH Page 2 of 5 Test report no.: 1-8178/19-01-02_AnnexA Photo 3:

Photo 4:

CTC advanced GmbH Page 3 of 5 Test report no.: 1-8178/19-01-02_AnnexA Photo 5:

Photo 6:

CTC advanced GmbH Page 4 of 5 Test report no.: 1-8178/19-01-02_AnnexA Document histor y Version Applied changes Initial release Date of release 2019-04-05 CTC advanced GmbH Page 5 of 5

RTCA DO-180G/ED-14G Env Category

[CAZ]CAB[SM]XXXXXXZ[BBBIAC]TTBIB2F2]XxAX P/N 304110 KTX2 Mode-S Transponder S/N 20000052T 9-33 VDC - 0.84 Ib (0.381kg) ETSO: EASA.210.10069784 P/N 304110 - 00(00) - we ETSO-C8BA / TSO-C8BA (10.0001) ETSO-C112D / T80-C112D ff]

ETSO-C166b / TSO-C166b -

RTCA DO-264 / ED80 Level C TQ-Systems GmbH RTCA DO-178C / ED12C Level C 082229 Seefeld RTCA DO-181E / ED73E Ciags 1 Level 2eis = DE.21G.0041 RTCA DO-260B / ED102A Class B1S FCC ID:2ANFF-KTX2S

sosos Jo!

----

sg4 ---- Aw

.f ~-- ---- --

Joo EUROPEAN TECHNICAL STANDARD ORDER

(ETSO) AUTHORISATION EASA.21O.10069784 This European Technical Standard Order (ETSO) Authorisation is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European Union, its Member States and of the European third countries that participate in the activities of EASA under Article 129 of that Regulation, subject to conditions specified below, to TQ-SYSTEMS GMBH GUT DELLING MUEHLSTR. 2 82229 SEEFELD GERMANY in accordance with Commission Regulation (EU) No. 748/2012, Part 21, Section A, Subpart O and ETSO C112d, C166b, C88a for KTX2.0300 Mode S Transponder P/N: 304110-00()-00() DDP No. KTX2.A.DDP, ISSUE 0202 or Subsequent Revisions

'

Limitations:

The KTX2 is to be used for non-complex aircraft with a MTOW below 5700 kg and maximum cruising TAS <

250kts. The maximum altitude is limited to 30000ft. For other limitations see also the DDP. Additional Functionalities:

Additional functionality as listed in the DDP is not covered by the above mentioned ETSO standard(s) and is accepted on a non-interference basis. See Continuation Sheet(s) For the European Aviation Safety Agency Cologne, Germany, 06 May 2019

-

arco CAPACC Section Manager European Technical Standard Orders

"'

I

~

~

Aooyate turoeaurs TE.ETSO.00092-006 ) European Aviation Safety Agency. All rights reserved. ISO9001 Certified. 10055520 - EASA.210.10069784 EUROPEAN TECHNICAL STANDARD ORDER - 10069784 - TQ-SYSTEMS GMBH - 308240 Page 1 of 2

---

sonsom noons woosso

----- ---- e A Ao

---- --

s onnm am Conditions:

1. The above ETSO Authorisation holder is only authorised to identify an Article with this ETSO marking whilst remaining in compliance with the conditions retained for the Issue of this Authorisation. 2. This ETSO Authorisation does not constitute an installation approval. It is the responsibility of those installing this article to determine that the aircraft installation conditions are within the ETSO standards. This ETSO Authorisation shall remain valid until surrendered or revoked.

- End I I 10055520 - EASA.210.10069784 EUROPEAN TECHNICAL STANDARD ORDER - 10069784 - TQ-SYSTEMS GMBH - 308240 AAeoy othe turoen use TE.ETSO.00092-006 European Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 2 of 2

TQSystems GmbH Elektronische Baugruppen und Systeme TQSystems GmbH, Gut Delling / Mhlstrae 2, 82229 Seefeld, Germany FAA Federal Aviation Administration Office of Spectrum Policy and Management ASR-1, 800 Independence Ave., SW., Washington, DC 20591 United States of America Date:

Page:

POC:

Dept.:

Phone:

Telefax:

E-Mail:

2019.05.07 1 of 2 Eilers, Thomas TQ EWA DE

+49(0)8153 9308-469

+49(0)8153 9308-7469 thomas.eilers@tq-group.com Notification of FCC Equipment Certification Application for TQ-Systems KTX2-S Mode S Transponder FCC ID: 2ANFF-KTX2S Dear Ladies and Gentlemen, In accordance with FCC Rules and Regulations, CFR Title 47, Part 87, Chapter I; Part 87 - Aviation Services, notification is hereby given from TQ-Systems to file for FCC Equipment Certification for the TQ-Systems KTX2-S Mode S Transponder. Part numbers:

FCC ID:

ETSO authorisation number: EASA.21O.10069784 EASA ETSO Authorization:

2ANFF-KTX2S 304110 (Standard 57mm format) ETSO-C88 (TSO-C88), ETSO-C112 (TSO-C112), Frequency range:

Output Power:

Emission designator:

ETSO-C166b (TSO-C166b) 1090 1 MHz (Tx); 1030 1 MHz (Tx);

250W ( 24dBW) @ 9 to 33VDC 12M0M1D Additional detailed characteristic information is included in the documentation on the enclosed CD that supports this notification. The enclosed CD is labelled TQ-Systems KTX2-S Mode S Transponder FCC Documentation, and its contents are as listed in ATTACHMENT A. In case of any requests, please do not hesitate to contact me. Sincerely, TQ-Systems GmbH i.V. Thomas Eilers Head of Design Organisation EASA.AP445 TQSystems GmbH l Gut Delling l Mhlstrae 2 l 82229 Seefeld l Tel. +49 8153 93080 l Fax +49 8153 4223 l www.tqgroup.com l info@tqgroup.com Geschftsfhrer: Detlef Schneider, Rdiger Stahl, Stefan Schneider l Amtsgericht Mnchen l HRBNr. 105 018 l UStIdNr. DE 252 251 764 l WEEEReg.Nr. DE 46311528 Donner & Reuschel l BLZ 200 303 00 l Kto. 1 039 210 l DE28 2003 0300 0103 9210 00 l USD:Kto. 31 039 210 l DE87 2003 0300 3103 9210 00 l BIC CHDBDEHH HypoVereinsbank Mnchen l BLZ 700 202 70 l Kto. 85 603 205 l DE98 7002 0270 0085 6032 05 l USD:Kto. 885 627 056 l DE68 7002 0270 0885 6270 56 l BIC HYVEDEMM VR Bank Starnberg l BLZ 700 932 00 l Kto. 5 123 003 l DE65 7009 3200 0005 1230 03 l BIC GENODEF1STH l Es gelten unsere Allgemeinen Geschftsbedingungen ATTACHMENT A Included support Information 1. Test report no.: 1-8178/19-01-02 2. Test report no.: 1-8178_19-01-02_AnnexA 3. Test report no.: 1-8178_19-01-02_AnnexB 4. Test report no.: 1-8178_19-01-02_AnnexC 5. Test report no.: 1-8178_19-01-02_AnnexD 6. Test report no.: 1-8178_19-01-02_AnnexE 7. Schematics part 1: KTX2.DIG.SP.0500 Stromlaufplan(P007755922). 8. Schematics part 2: KTX2.HD.S.SP.0500 Stromlaufplan(P007764123) 9. Schematics part 3: KTX2.RF.SP.0500 Stromlaufplan(P007621659) 10. Schematics part 4: KTX2.RF.SP.0500 Stromlaufplan(P007621659) 11. KTX2-DIG.SLE.0500(P007757321) = Bill of Material 12. P008026812.V0.(F)_KTX2-S.V2-KPL.SL11.0100 = Bill of Material 13. KTX2.RF.SLE.0500(P007673340) = Bill of Material 14. KTX2-HD-S.SLE.0500(P007771434) = Bill of Material 15. KTX2 Mode S Transponder Architecture - Master Block Diagram 16. KTX2.A-MAN.0202.en.= Operation and Installation Manual KTX2-S Mode S Transponder 17. KTX2.A-DDP.0202 = Declaration of Design and performance (Operational Description) 18. Label = KTX2-S label Identification 19. KRT2.A-DDD.0100.pdf = Detailled Design Document 20. 21O.10069784_CERT_REV_0_20190506 = ETSO authorization certificate EASA.21O.10069784 21. Confidentiality Request for Certification Service in USA TQSystems GmbH l Gut Delling l Mhlstrae 2 l 82229 Seefeld l Tel. +49 8153 93080 l Fax +49 8153 4223 l www.tqgroup.com l info@tqgroup.com Geschftsfhrer: Detlef Schneider, Rdiger Stahl, Stefan Schneider l Amtsgericht Mnchen l HRBNr. 105 018 l UStIdNr. DE 252 251 764 l WEEEReg.Nr. DE 46311528 Donner & Reuschel l BLZ 200 303 00 l Kto. 1 039 210 l DE28 2003 0300 0103 9210 00 l USD:Kto. 31 039 210 l DE87 2003 0300 3103 9210 00 l BIC CHDBDEHH HypoVereinsbank Mnchen l BLZ 700 202 70 l Kto. 85 603 205 l DE98 7002 0270 0085 6032 05 l USD:Kto. 885 627 056 l DE68 7002 0270 0885 6270 56 l BIC HYVEDEMM VR Bank Starnberg l BLZ 700 932 00 l Kto. 5 123 003 l DE65 7009 3200 0005 1230 03 l BIC GENODEF1STH l Es gelten unsere Allgemeinen Geschftsbedingungen

CON FIDENTALITY REQU EST for Certification Service in USA Federal Communication Commission Equipment Authorization Division, Application Processing Branch 7435 Oakland Mills Road Columbia, MD 21048 2019-04-24 TO WHOM IT MAY CONCERN Pursuant to Paragraphs $0.457 and 0.459 of the Commission's Rules (47 C.F.R.) and Section S552(bX4) of the Freedom of lnformation Act, we requests confidentiality for the following products:

FCC ID 2ANFF-KTX25 Model name KTX2-S Mode S Transponder For the product stated above, we request permanent confidentiality for exhibits which contain Operational Description, Block Diagram, Schematics, Pads Lists or Tune Up lnformation. The above exhibits contain our trade secrets and proprietary information that could be of benefit to our competitors. lf you have any questions, please feel free to contact me at the address shown below.

*W*

i.V. Thomas Eilers Head of Design Organisation EASA.AP445 TQ-Systems GmbH Mhlstrae 2, Gut Delling, 82229 Seefeld, Germany Tel.: +498153 9308-469 Fax: +498'1 53 9308-7469 thomas.eilers@tq-qroup.com Amtsgericht Mnchen, HRB 105 018, UST-ldNr. DE 81 '1 607 913 Geschftsfuhrer: Dipl.-lng. (FH) Detlef Schneider, Dipl.-lng. (FH) Rdiger Stahl, Dipl.-lng. (FH) Stefan Schneider