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User Manual | Users Manual | 2.89 MiB | February 09 2019 | |||
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Label | ID Label/Location Info | 121.86 KiB | February 09 2019 | |||
| 1 | Block Diagram | Block Diagram | September 02 2019 | confidential | ||||
| 1 | BoM Digital Board | Parts List/Tune Up Info | September 02 2019 | confidential | ||||
| 1 | BoM Head Board | Parts List/Tune Up Info | September 02 2019 | confidential | ||||
| 1 | BoM RF Board | Parts List/Tune Up Info | September 02 2019 | confidential | ||||
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Confidentiality Request Letter - Permanent | Cover Letter(s) | 48.17 KiB | February 09 2019 | |||
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Notification Letter to the FAA | Cover Letter(s) | 113.20 KiB | February 09 2019 | |||
| 1 | Operational Description | Operational Description | September 02 2019 | confidential | ||||
| 1 | Test Setup Photos | February 09 2019 | ||||||
| 1 | Schematics Digital Board | Schematics | September 02 2019 | confidential | ||||
| 1 | Schematics Head Board | Schematics | September 02 2019 | confidential | ||||
| 1 | Schematics RF Board | Schematics | September 02 2019 | confidential | ||||
| 1 | Test Report | February 09 2019 | ||||||
| 1 | Test Report | February 09 2019 |
| 1 | User Manual | Users Manual | 2.89 MiB | February 09 2019 |
TO Avaton EASA.AP445 KTX2-F.01 00 MAN KTX2-F.0001 MAN Operation and lnstallation Manual Doc.-No. KTX2-F.A-MAN lssue:
0001 ECR-No. KTX2.F.A-ECR.O204 Date:
MoC:
2019-07-03 0 Document Release lFunction Name ate Signature Prepared by Thomas Whner 2019-07-03 Checked by Florian Holzner 2019-07-03 Approved by Thomas Eilers 2019-07-03
/, iV w,1,,-
z KTX2-F.A-MAN.0001.docx
@ TQ-Systems GmH. All nformaton contained n ths documents have to be treated strictly confdential. The transfer of presentations and know-how to third parties requres the pror wrtlen consent of TQ-Systems GmbH. Page 1 of74 TQ Aviation EASA.AP445 KTX2-F.0100 MAN KTX2-F.A-MAN.0001.docx Page 2 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 KTX2-F Mode-S Transponder Flat (160mm) format KTX2-F (flat 160mm format) with ADS-B with Part-No 295153 Operation and Installation Manual KTX2-F.A-MAN.0001.docx Page 3 of 74 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-F.0100 MAN EASA.AP445 Revision List Revision Date Topic 0100 2019-02-07 Initial Release 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-F.A-MAN.0001.docx Page 4 of 74 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-F.0100 MAN EASA.AP445 Change History Product Revision Date Description of Change KTX2-F.A-MAN.0001.docx Page 5 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 Table of Contents 2.2 2.1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 1. General ..................................................................................................................................... 9 Purpose ............................................................................................................................. 9 Scope ................................................................................................................................ 9 Terminology ....................................................................................................................... 9 Symbols ............................................................................................................................ 9 Abbreviations ................................................................................................................... 10 Customer Support ........................................................................................................... 14 Features .......................................................................................................................... 15 Safety-Conscious Utilization ............................................................................................ 16 Restriction for Use ........................................................................................................... 16 2. Operation ................................................................................................................................ 17 Controls and Display ....................................................................................................... 17 2.1.1 Controls ....................................................................................................................... 18 2.1.2 Display Indications ....................................................................................................... 19 Normal Operation Menu Structure ................................................................................... 20 2.2.1 ON/OFF Switching ....................................................................................................... 21 2.2.2 Transponder-Modes .................................................................................................... 22 2.2.3 Squawk Code Change ................................................................................................. 23 2.2.4 VFR Squawk ............................................................................................................. 24 2.2.5 Squawk Ident (ID, SPI) ................................................................................................ 25 2.2.6 Airborne/Ground Indication .......................................................................................... 25 2.2.7 ADS-B Status Indication .............................................................................................. 27 2.2.8 Adjustable parameters in normal operation mode ........................................................ 28 2.2.9 GNSS Data .................................................................................................................. 30 3. Setup Mode ............................................................................................................................. 31 Controls and Display ....................................................................................................... 31 Entering Set Up ............................................................................................................... 33 Controls ........................................................................................................................... 33 3.3.1 Selection ...................................................................................................................... 33 3.3.2 Return to parent menu ................................................................................................. 33 3.3.3 Cancel/Discard ............................................................................................................ 33 Setup Menus ................................................................................................................... 34 3.4.1 Brightness ................................................................................................................... 34 3.4.2 Flight-Identifier (Flight ID) ............................................................................................ 37 3.4.3 Modify VFR .................................................................................................................. 47 3.4.4 Factory Reset .............................................................................................................. 49 3.4.5 Test Menu ................................................................................................................... 49 4. Errors, Warnings and Notifications .......................................................................................... 53 Degrading failures ........................................................................................................... 53 4.1.1 Low Battery Voltage ..................................................................................................... 54 4.1.2 Very Low Battery Voltage ............................................................................................ 55 Limiting failures ............................................................................................................... 56 Severe failures ................................................................................................................ 56 Notifications ..................................................................................................................... 58 4.4.1 GNSS Data CRC Failure ............................................................................................. 58 4.4.2 Do System Restart ....................................................................................................... 58 Installation ............................................................................................................................... 59 Equipment Connections ................................................................................................... 59 5.1.1 Electrical Connections ................................................................................................. 59 5.1.2 Mutual Suppression ..................................................................................................... 59 5.1.3 Ground Switch ............................................................................................................. 59 Page 6 of 74 4.2 4.3 4.4 3.1 3.2 3.3 KTX2-F.A-MAN.0001.docx 3.4 4.1 5.1 5. 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-F.0100 EASA.AP445 MAN 7.1 7.2 5.1.4 Static Air Port ............................................................................................................... 60 5.1.5 GNSS Interface ........................................................................................................... 60 5.1.6 Antenna Connector ...................................................................................................... 60 5.2 Wiring .............................................................................................................................. 64 5.2.1 Conductor Cross Section ............................................................................................. 64 5.2.2 Wiring Scheme ............................................................................................................ 64 6. Drawings ................................................................................................................................. 65 7. Technical Data ........................................................................................................................ 67 General ........................................................................................................................... 67 Transmitter Receiver .................................................................................................... 69 8. FCC related issues .................................................................................................................. 70 8.1 Radiofrequency radiation exposure Information: .............................................................. 70 8.2 Compliance ..................................................................................................................... 70 8.3 Modifications ................................................................................................................... 70 9. Maintenance ........................................................................................................................... 71 Periodic Maintenance ...................................................................................................... 71 Repair .............................................................................................................................. 71 Cleaning .......................................................................................................................... 71 EXCLUSIVE LIMITED WARRANTY and LIMITATIONS ON LIABILITY ............................... 72 Software License Conformity ............................................................................................... 73 9.1 9.2 9.3 10. 11. List of Tables Table 1: Transponder Modes ................................................................................................................. 22 Table 2: GND Switch Support ................................................................................................................ 40 Table 3: Certitified GNSS Units .............................................................................................................. 42 Table 4: Approved GNSS Units .............................................................................................................. 42 Table 5: List of supported GNSS Devices .............................................................................................. 43 Table 6: Degrading Failures ................................................................................................................... 54 Table 7: Severe Failures ........................................................................................................................ 57 Table 8: L-Band Antennas ..................................................................................................................... 61 Table 9: Common Antenna Cables ........................................................................................................ 62 Table 10: Technical Data ....................................................................................................................... 68 Table 11: Transmitter Data .................................................................................................................... 69 Table 12: Receiver Data ........................................................................................................................ 69 Table 13: General Data .......................................................................................................................... 69 List of Figures Figure 1: Display Diagram ...................................................................................................................... 17 Figure 2: Controls .................................................................................................................................. 18 Figure 3: Indicators ................................................................................................................................ 19 Figure 4: Operational menu structure ..................................................................................................... 20 Figure 5: Initial Display ........................................................................................................................... 21 Figure 6: Normal Operation .................................................................................................................... 22 Figure 7: VFR-Squawk ........................................................................................................................... 24 Figure 8: Squawk Ident .......................................................................................................................... 25 Figure 9: Airborne/Ground Indication "FLY" ........................................................................................... 26 Figure 10: Airborne/Ground Indication "GND" ........................................................................................ 26 Figure 11: ADS-B Indication ................................................................................................................... 27 Figure 12: Change Flight ID ................................................................................................................... 28 Figure 13: Change Brightness................................................................................................................ 28 Figure 14: GNSS Data Display ............................................................................................................... 30 Figure 15: Button functions in Setup Mode............................................................................................. 31 KTX2-F.A-MAN.0001.docx Page 7 of 74 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-F.0100 MAN EASA.AP445 Figure 16: Setup mode menu structure .................................................................................................. 32 Figure 17: Setup Menu 1 ........................................................................................................................ 33 Figure 18: Setup Menu 2 ........................................................................................................................ 33 Figure 19: Setup Brightness Menu ......................................................................................................... 34 Figure 20: Button Illumination Mode "Off"............................................................................................... 35 Figure 21: Button Illumination Mode "On"............................................................................................... 35 Figure 22: Button Illumination Mode "Auto" ............................................................................................ 36 Figure 23: Flight ID configuration ........................................................................................................... 37 Figure 24: FID Limitation Notification ..................................................................................................... 37 Figure 25: Flight ID Edit Menu ................................................................................................................ 38 Figure 26: Device Parameter Configuration Menu.................................................................................. 39 Figure 27: Aircraft Category Selection Menu .......................................................................................... 40 Figure 28: Ground Switch Setup Menu .................................................................................................. 40 Figure 29: Maximum Speed Category Selection Menu........................................................................... 41 Figure 30: GNSS Device Selection Menu .............................................................................................. 42 Figure 31: Baud Rate Selection Menu .................................................................................................... 43 Figure 32: Aircraft Length/Width Configuration Menu ............................................................................. 44 Figure 33: GNSS Antenna Offset Configuration Menu ........................................................................... 45 Figure 34: Delete Flight ID Menu ........................................................................................................... 46 Figure 35: Multiple Flight ID Selection Menu .......................................................................................... 47 Figure 36: Modify VFR Code Menu ........................................................................................................ 47 Figure 37: Factory Reset Menu .............................................................................................................. 49 Figure 38: Test Menu ............................................................................................................................. 49 Figure 39: Altitude Offset Calibration Menu ............................................................................................ 50 Figure 40: Test Mode Menu ................................................................................................................... 51 Figure 41: Device Info Menu .................................................................................................................. 52 Figure 42: Low Battery Voltage .............................................................................................................. 54 Figure 43: Very Low Battery Voltage ...................................................................................................... 55 Figure 44: Missing AA-Code .................................................................................................................. 56 Figure 45: Critical Error (Example) ......................................................................................................... 56 Figure 46: GNSS CRC Failure ............................................................................................................... 58 Figure 47: System Restart ..................................................................................................................... 58 Figure 48: Wiring.................................................................................................................................... 64 Figure 49: Dimensions of KTX2-F Standard round format ...................................................................... 65 Figure 50: Panel Cut-Out ....................................................................................................................... 66 KTX2-F.A-MAN.0001.docx Page 8 of 74 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-F.0100 EASA.AP445 1. General MAN 1.1 Purpose This manual contains information about the physical, mechanical and electrical characteristics, installation and operation for the KTX2-F Mode S Transponder. Additionally it describes the ADS-B functionality for a compliant ADS-B Out installation using Extended Squitter (ES). 1.2 Scope This manual applies to the operation and installation of the KTX2-F Mode S Transponder. At the publication date of this manual the software version is 0100 and the FPGA version is 0042. The software and FPGA versions are subject to change without further notice. 1.3 Terminology Except where specifically noted, references made to the Unit or the Installation will apply to the transponder defined in 1.2. Referenced Documents where the respective document is identified by document number, document title and issue. The word MUST in the text denotes a mandatory instruction. A deviation is not permissible. The word SHOULD in the text denotes a recommendation or advice. Such recommendations or advice is expected to be followed unless good reasons are stated for not doing so. The word MAY in the text denotes a permissible practice or action. Note: Background information contained in this document is always indicated by using an italic character font. 1.4 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. INFORMATION:
Supplemental information for operating the device. KTX2-F.A-MAN.0001.docx Page 9 of 74 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-F.0100 EASA.AP445 1.5 Abbreviations MAN Abbr. Meaning Explanation AA AC ADC ADF ADS-B Aircraft Address Assigned ICAO 24 bit address Advisory Circular Information and guidance publication Analog Digital Converter Automatic Direction Finder Navigation equipment Automatic Dependent Surveillance Broadcast ALT Altitude The transponder will respond to all interrogations and transmits ABS-B messages. ATC Air Traffic Control ATCRBS Air Traffic Control Radar Beacon System BAT Battery BNC CFR Bayonet Neill-
Concelman Code of Federal Regulations COMM Communication(s) CRC DME EASA ECR Cyclical Redundancy Check(s) Distance Measuring Equipment European Aviation Safety Agency Engineering Change Request A RF connector type. EEPROM Electrically Erasable Programmable Read-Only Memory KTX2-F.A-MAN.0001.docx Page 10 of 74 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 EASA.AP445 Abbr. KTX2-F.0100 MAN Meaning Explanation ENV Environment ES Extended Squitter ETSO European Technical Standard Order FAA FAX FCC Federal Aviation Administration Facsimile Federal Communications Commission FID Flight ID Number of flight plan if assigned, else Registration number of aircraft FLY Flight The aircraft is in Flight Mode FPGA Field-Programmable Gate Array GND Ground The transponder will respond to Mode S ground interrogations from surface movement radar. ABS-B messages are transmitted (Surface messages). GNSS Global Navigation Satellite System GPS ICAO IDT LSA Global Positioning System International Civil Aviation Organization Identify Light Sport Aircraft MAN Manual MCU Microcontroller Unit MIL MTL Military Minimum Triggering Level KTX2-F.A-MAN.0001.docx Page 11 of 74 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 EASA.AP445 Abbr. NMEA ON RMC RSS RTCA SAE SMA KTX2-F.0100 MAN Meaning Explanation National Marine Electronics Association Transponder Mode On The transponder will respond to all interrogations, but altitude reporting is suppressed. ABS-B messages are transmitted. Recommended Minimum Sentence C NMEA sentence Radio Standards Specifications
(Canada) Radio Technical Commission for Aeronautics Society of Automotive Engineers Sub-Miniature A Connector SPI Special Position Identification (ID) If activated on request by air traffic controller (Squawk Ident) a SPI Pulse is transmitted for 18 seconds. This highlights the respective traffic item on the radar screen of the air traffic controller. STBY Standby The transponder is on, but will not reply to any interrogations or transmit any ADS-B out messages. SUB Subminiature SUPP Suppression Threaded Neill-
Concelman A RF connector type. TNC TSO USA Technical Standard Order[
United States of America VFR Visual Flight Rules KTX2-F.A-MAN.0001.docx Page 12 of 74 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 EASA.AP445 Abbr. VSWR WAAS KTX2-F.0100 MAN Meaning Explanation Voltage Standing Wave Ratio Wide Area Augmentation System (GPS) KTX2-F.A-MAN.0001.docx Page 13 of 74 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-F.0100 EASA.AP445 1.6 Customer Support MAN In order to facilitate a rapid handling of returned shipments, please send your request to the email address below. Additional information and FAX number can be found on the TQ Avionics web portal:
https://www.tq-avionics.com/
Any suggestions for improvement of our manuals are welcome. Contact: info@tq-avionics.com Information on software updates are available at TQ. https://www.tq-avionics.com/
KTX2-F.A-MAN.0001.docx Page 14 of 74 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-F.0100 EASA.AP445 1.7 Features MAN In order to operate the Mode-S transponder it is necessary to request an ICAO 24-Bit Aircraft Address at the responsible National Aviation Authorities. The received code must be configured within the transponder (see chapter 3.4.2.1.2). Class 1 Level 2els Non-Diversity Mode-S-Transponder for ground based interrogations 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 IDENT capability for activating the Special Position Identification- Pulse
(SPI) for 18 seconds, which is requested by the Controller Squawk Ident ADS-B out:
o Airborne Position o Identification and Category o Airborne Velocity o Operational Status o Extended Squitter Aircraft Status Maximum flight level 30 000ft; maximum airspeed 250kt Display information contains Squawk code, mode of operation and pressure altitude 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 GNSS receiver for ADS-B can be connected 8 storable entries for AA-/Aircraft-Code, FID Ground-Switch support KTX2-F.A-MAN.0001.docx Page 15 of 74 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-F.0100 EASA.AP445 1.8 Safety-Conscious Utilization MAN For safe operation of the transponder the following notices have to be observed:
The installation of the transponder into an aircraft should be carried out only by an authorized installation company. The country regulations always have to be observed. Use the transponder only within the specified conditions, see chapter 7. Power supply:
Do not connect the transponder to AC sources. Make sure that the transponder is connected to the mandatory DC source, see chapter 7. Do not connect the transponder with reversed polarity to the DC source. Circuit breaker:
The transponder should be protected from the aircraft power supply by a dedicated 3 A circuit breaker or fuse (slow-blow). Excessive pulses on the DC bus of the aircraft may cause damage on electrical circuits of any installed instrument. Do not switch ON the transponder during engine start or shutdown. 1.9 Restriction for Use The transponder is to be used only inside the declared limits. KTX2-F.A-MAN.0001.docx Page 16 of 74 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-F.0100 EASA.AP445 2. Operation MAN 2.1 Controls and Display Figure 1: Display Diagram KTX2-F.A-MAN.0001.docx Page 17 of 74 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-F.0100 EASA.AP445 2.1.1 Controls MAN This chapter describes the use of the buttons and knobs during normal operation. The usage while in setup mode is described in chapter 3.3. Button Designation Function ON/OFF Press to switch the transponder on and off. This switch is mechanically locked until it is pressed a second time VFR 1. Activate/deactivate VFR Squawk 2. Pressing the button for more than 3 seconds will show the Brightness menu (see 2.2.8.2) CHANGE 1. Exchange of the active and standby-Squawk 2. Pressing the button for more than 3 seconds will show the GNSS data menu (see 2.2.9) IDENT 1. Squawk Ident, a SPI Pulse is transmitted for 18 seconds
(in normal mode). 2. Pressing the button for more than 3 seconds will show the Flight-ID menu (see 2.2.8.1) MODE 1. Select Transponder-Mode STBY, GND, ON or ALT. 2. Pressing the button for more than 3 seconds will toggle the ADS-B mode (On/Off) Rotary knob 1. Enter a new Squawk (see 2.2.2) 2. Enter values and select options in submenus (see 3.3) 3. Confirm Warnings and Notifications Figure 2: Controls KTX2-F.A-MAN.0001.docx Page 18 of 74 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 EASA.AP445 KTX2-F.0100 MAN 2.1.2 Display Indications Indication Meaning Transponder is transmitting Mode-A/C Replies on Interrogations Transponder is transmitting Mode-S Replies on Interrogations Transponder is locked by a ground station and will be directly addressed Remark Appears per reply and persists for some time Appears per reply and persists for some time Appears at every addressed reply and persists for some time ADS-B out Status Status of ADS-B transmission Active Squawk Is shown at upper position Battery power too low Appears above Standby-Squawk Failure indication See 4 IDENT- Marking is transmitted ID (Squawk Ident) has been pressed active for 18s Current Flight Level Flight Level (in 100ft steps) Mode display
(STBY, ON, GND, ALT) see chapter. 2.1.6 Transponder-
Modes Standby-Squawk Flight ID Is shown at lower position. Can be exchanged with active Squawk by pressing the UP/DOWN (Change) button Only shown if a Flight ID is configured with a valid Aircraft Address VFR indication Shown while VFR squawk is used Transponder is in airborne mode Transponder is in ground mode Only shown if Ground Switch support is configured. Only shown if Ground Switch support is configured. Figure 3: Indicators KTX2-F.A-MAN.0001.docx Page 19 of 74 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-F.0100 MAN EASA.AP445 2.2 Normal Operation Menu Structure Figure 4: Operational menu structure KTX2-F.A-MAN.0001.docx Page 20 of 74 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-F.0100 EASA.AP445 2.2.1 ON/OFF Switching MAN To switch on the transponder press the ON/OFF button once. The button will be locked in its ON position. Press the button again to switch it off. The initial display is shown shortly after the transponder is switched on (see figure below). Figure 5: Initial Display The initial display shows the current software and FPGA version. After approx. two (2) seconds the transponder switches either to its normal operation display or a selection menu is shown if multiple Flight IDs are configured. If a failure is detected during start-up a fault notification is displayed. In that case see chapter 4 for details. 2.2.1.1 Multiple Flight ID selection If multiple Flight IDs are configured a selection menu is displayed. 2.2.1.2 Normal operation The normal operation always starts in standby mode. The normal operation display is shown as follows:
KTX2-F.A-MAN.0001.docx Page 21 of 74 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 EASA.AP445 KTX2-F.0100 MAN Figure 6: Normal Operation Note:
The Flight ID is not displayed if no valid Flight ID is configured. 2.2.2 Transponder-Modes The currently active mode is displayed at the lower left corner of the display. Mode STBY GND ON ALT Explanation Transponder is switched on but does not respond to any interrogation. ADS-B out is disabled. Transponder responds to Mode-S interrogations. ADS-B out is enabled (Surface Squitter). Transponder responds to all interrogations, but altitude is not transmitted. ADS-B out is enabled. Transponder responds to all interrogations. ADS-B out is enabled. Table 1: Transponder Modes During the flight the Mode ALT should always be set, unless the ATC gives other instructions. While rolling on the ground the transponder should be set to GND. If the installation includes a weight on wheels switch and it is correctly configured then the mode is changed automatically. To change the mode press the MODE button until the desired mode is displayed. The MODE button is also used to enable or disable the ADS-B out function. Press the MODE button for at least 3 seconds until the ADS-B indication changes (see 2.2.7). Note:
The ADS-B out function is enabled by default if a GNSS device is configured (see 3.4.2.1.3.4). KTX2-F.A-MAN.0001.docx Page 22 of 74 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-F.0100 EASA.AP445 2.2.3 Squawk Code Change MAN To change the squawk code perform the following procedure:
1. Press the rotary knob. The first digit of the standby squawk turns green. 2. Turn the rotary knob to change the value. 3. Press the rotary knob again to save the selected digit. The next digit turns green. 4. Repeat steps 2 and 3 until all four (4) digits are set to desired squawk code. 5. Press the Change button. The standby squawk code is exchanged with the currently active squawk code. Note:
The top line shows always the active squawk. KTX2-F.A-MAN.0001.docx Page 23 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 2.2.4 VFR Squawk To set the active squawk to a predefined code press the VFR button. The VFR-squawk code is now shown as active squawk. VFR is indicated on the right hand side of the display and the former active squawk becomes the standby squawk. Figure 7: VFR-Squawk Press the VFR button again to restore the previous squawk code as active squawk. The VFR indication disappears. The factory setting of the VFR-Squawk code is 7000. The VFR-squawk code can be configured in accordance with local requirements using the setup mode (see 3.4.3). KTX2-F.A-MAN.0001.docx Page 24 of 74 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-F.0100 MAN EASA.AP445 2.2.5 Squawk Ident (ID, SPI) Press the IDENT button if the ATC requests you to send Ident or Squawk Ident. For 18 seconds the Ident Pulse is activated in the transponder replies. This is indicated by IDT on the left hand side of the display. Figure 8: Squawk Ident 2.2.6 Airborne/Ground Indication If the aircraft is equipped with a weight on wheels switch or has an automatic air/ground system the transponder can be configured to use it for Airborne/Ground mode switching (see 3.4.2.1.3.2). Depending on the status either FLY (Flight) or GND (Ground) is shown on the display in the lower right corner. KTX2-F.A-MAN.0001.docx Page 25 of 74 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 EASA.AP445 KTX2-F.0100 MAN Figure 9: Airborne/Ground Indication "FLY"
Figure 10: Airborne/Ground Indication "GND"
Note:
If this function is not activated, no indications are displayed and the mode must be manually selected (see 2.2.2). KTX2-F.A-MAN.0001.docx Page 26 of 74 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-F.0100 EASA.AP445 2.2.7 ADS-B Status Indication MAN The current operational status of the ADS-B is shown on the display as follows:
Indication Function Description ADS-B enabled. Letter A appears in white color. ADS-B out function is active and transmitting messages. ADS-B enabled. Letter A appears in yellow color. ADS-B out function is active but not transmitting messages. ADS-B enabled. Letter A appears in red color. ADS-B out function is active and transmitting type ZERO position messages or no position messages due to missing position data
(longitude, altitude, latitude). ADS-B disabled. No letter A displayed. No ADS-B data is transmitted. Figure 11: ADS-B Indication Note: Above images show the upper left section of the display only. KTX2-F.A-MAN.0001.docx Page 27 of 74 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-F.0100 MAN EASA.AP445 2.2.8 Adjustable parameters in normal operation mode Some parameters can be changed while in normal operation mode. The changes are effective immediately after confirmation, but will remain only until the transponder is powered off. Note:
To make changes permanently the parameters have to be changed in setup mode (see 3). 2.2.8.1 Flight ID To modify the Flight ID press the ID button for at least 3 seconds. Figure 12: Change Flight ID The Flight ID can be adjusted in the same way as described in chapter 3.4.2.1. Note:
The AA-Code is shown for information only and cannot be changed. 2.2.8.2 Brightness To modify the display brightness and the button illumination press the VFR button for at least 3 seconds. Figure 13: Change Brightness To change the display brightness select Display and press the rotary knob. Turn the rotary knob to change the value for brightness between 1 (lowest) to 5 (highest). Press the rotary knob to save the new value. KTX2-F.A-MAN.0001.docx Page 28 of 74 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-F.0100 EASA.AP445 2.2.8.3 Button Config MAN To change the button illumination select Btn-Mode and press the rotary knob. The button illumination has three (3) modes: Off, On and Auto. Turning the rotary knob will change the mode. Press the rotary knob again to confirm the mode. Depending on the selected mode further parameters can be configured. 2.2.8.3.1 Button Illumination Mode Off If this mode is selected the button illumination is switched off. No further parameters can be configured. 2.2.8.3.2 Button Illumination Mode On If this mode is selected the button illumination is switched on. To change the illumination level select Level and press the rotary knob. Turn the rotary knob to change the value between 1 (dark) to 5 (bright). Press the rotary knob to save the new value. 2.2.8.3.3 Button Illumination Mode Auto If this mode is selected the button illumination is switched between a day and night setting depending on the ambient light sensor. No further parameters can be configured. The settings can only be configured in setup mode, see chapter 3.4.1. KTX2-F.A-MAN.0001.docx Page 29 of 74 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-F.0100 EASA.AP445 2.2.9 GNSS Data MAN Press the Change button for at least 3 seconds to display the actual GNSS position data. Figure 14: GNSS Data Display Press the rotary knob to return to the normal operation display. KTX2-F.A-MAN.0001.docx Page 30 of 74 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-F.0100 EASA.AP445 3. Setup Mode MAN 3.1 Controls and Display Do not use Setup Mode in flight. Check with your avionics installer before changing the configuration. On / Off Setup Display Ambient Ambient Light Light Sensor Sensor Figure 15: Button functions in Setup Mode Enter Setup Mode Cancel Discard Rotary knob with push button for navigation, selection and editing KTX2-F.A-MAN.0001.docx Page 31 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 Figure 16: Setup mode menu structure KTX2-F.A-MAN.0001.docx Page 32 of 74 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-F.0100 EASA.AP445 3.2 Entering Set Up MAN To enter the setup mode, press the IDENT button while switching on the transponder and the setup menu appears as shown below. Figure 17: Setup Menu 1 3.3 Controls 3.3.1 Selection Turning the rotary knob moves to the desired menu item. Press the rotary knob to select the desired parameter for configuration or to enter a submenu. If a menu consists of several pages, e.g. the setup menu, the next page can be accessed by turning the rotary knob clockwise until the next page is shown. To go back turn the rotary knob counterclockwise until the previous page is displayed. Figure 18: Setup Menu 2 3.3.2 Return to parent menu Any menu showing an arrow left of the headline can be left by selecting the headline and pressing the rotary knob. The previous menu will be displayed. 3.3.3 Cancel/Discard The IDENT button can be used for cancelling, discarding or returning. KTX2-F.A-MAN.0001.docx Page 33 of 74 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-F.0100 MAN EASA.AP445 While editing pressing the IDENT button briefly will cancel the current editing. The previous configuration value is restored. While in a submenu pressing the IDENT button briefly will return to the previous menu. Pressing the IDENT button for at least 3 seconds will discard any unsaved changes and return to the main setup menu. 3.4 Setup Menus 3.4.1 Brightness To change the display brightness select Display and press the rotary knob. Turn the rotary knob to change the value for brightness between 1 (lowest) to 5 (highest). Press the rotary knob to save the new value. Figure 19: Setup Brightness Menu 3.4.1.1 Button Config To change the button illumination select Button Config and press the rotary knob. A menu for configuring the button illumination and its modes is displayed. The button illumination has three (3) modes: Off, On and Auto. To change the mode select Mode and press the rotary knob. Turning the rotary knob will change the mode. Press the rotary knob again to confirm the mode. Depending on the selected mode several parameters can be configured. 3.4.1.1.1 Button Illumination Mode Off If this mode is selected the button illumination is switched off. No further parameters can be configured. KTX2-F.A-MAN.0001.docx Page 34 of 74 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 EASA.AP445 KTX2-F.0100 MAN Figure 20: Button Illumination Mode "Off"
3.4.1.1.2 Button Illumination Mode On If this mode is selected the button illumination is switched on. To change the illumination level select Level and press the rotary knob. Turn the rotary knob to change the value between 1 (dark) to 5 (bright). Press the rotary knob to save the new value. Figure 21: Button Illumination Mode "On"
3.4.1.1.3 Button Illumination Mode Auto If this mode is selected the button illumination is switched between a day and night setting depending on the ambient light sensor. To change the illumination level for day or night select appropriate menu item (Day, Night) and press the rotary knob. Turn the rotary knob to change the value between 0 (off) to 5 (bright). Press the rotary knob to save the new value. To change the threshold level for the day/night switching select Threshold and press the rotary knob. Turn the rotary knob to change the value between 1 (high light sensitivity) to 5 (low light sensitivity). Press the rotary knob to save the new value. KTX2-F.A-MAN.0001.docx Page 35 of 74 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 EASA.AP445 KTX2-F.0100 MAN Figure 22: Button Illumination Mode "Auto"
KTX2-F.A-MAN.0001.docx Page 36 of 74 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-F.0100 EASA.AP445 3.4.2 Flight-Identifier (Flight ID) MAN The transponder can store up to eight flight IDs for multiple aircraft configurations (e.g. in a portable station as used in hot-air/gas filled balloons). For multiple flight IDs, an appropriate Aircraft Address must be assigned to each of the flight IDs. See 3.4.2.4 for details. Note:
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 any blanks. To configure a Flight ID configuration select Flight ID and press the rotary knob. A menu for adding, modifying and deleting a Flight ID configuration is displayed. Figure 23: Flight ID configuration Select Add to add a Flight ID, Modify to modify a Flight ID or Delete to delete a Flight ID and press the rotary knob. 3.4.2.1 Add/Edit Flight ID To add a Flight ID select Add and press the rotary knob. If all eight possible IDs are already configured the following notification is displayed. Figure 24: FID Limitation Notification If this message appears you can either modify an existing entry (see 3.4.2.2) or delete an existing entry
(see 3.4.2.3) and add a new one as shown below. KTX2-F.A-MAN.0001.docx Page 37 of 74 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 EASA.AP445 KTX2-F.0100 MAN If a new Flight ID can be added a submenu Edit FID Param. is displayed. Figure 25: Flight ID Edit Menu Note:
All configuration settings of a new Flight ID are set to their default values. 3.4.2.1.1 Flight ID Value To configure the Flight ID perform the following procedure:
1. Select FID and press the rotary knob to start editing a Flight ID. The first character turns yellow. 2. Turn the rotary knob to change the value. 3. Press the rotary knob again to save the selected character. The next character turns yellow. 4. Repeat steps 2 and 3 until all characters (max. 8) are set to desired value. 5. Saving the 8th character will end the editing. If the Flight ID contains less than 8 characters then enter a space as last character to end the editing. Note:
After editing the changed value is not saved automatically! You have to select Save once all data have been configured (see 3.4.2.1.4). Enter the FID left-aligned, without any blanks or dashes
(!), e.g. DENWS for the marking D-ENWS. A missing FID disables mode-S operation and A/C-
mode only will be engaged. See chapter 4 Self-Test, Errors and Warnings KTX2-F.A-MAN.0001.docx Page 38 of 74 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-F.0100 EASA.AP445 3.4.2.1.2 Aircraft Address (AA) Value MAN To configure the Aircraft Address (AA) perform the following procedure:
1. Select AA and press the rotary knob to start editing the AA. The first digit turns yellow. 2. Turn the rotary knob to change the value. 3. Press the rotary knob again to save the selected digit. The next character turns yellow. 4. Repeat steps 2 and 3 until all digits are set to desired value. Note:
After editing the changed value is not saved automatically! You have to select Save once all data have been configured (see 3.4.2.1.4). Note:
Before you can enter the Aircraft Address, the Flight ID needs to be defined. Note:
All values except 000000 and FFFFFFF are valid. The transponder accepts all values but if an invalid value is used as Aircraft Address the transponder will show a failure and the transponder switches to AC-only mode. 3.4.2.1.3 Device Parameter To configure the parameters associated to a Flight ID select Device Parameter" and press the rotary knob. A submenu Device Param. is displayed. Note:
The submenu Device Parameter consists of two (2) pages. Figure 26: Device Parameter Configuration Menu Note:
After changing any parameter the new value is not saved automatically! You have to select Save once all data have been configured (see 3.4.2.1.4). 3.4.2.1.3.1 Aircraft Category To configure the aircraft category select Aircraft Category" and press the rotary knob. A submenu AC Category is displayed. Note:
The submenu Device Parameter consists of two (2) pages. KTX2-F.A-MAN.0001.docx Page 39 of 74 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 EASA.AP445 KTX2-F.0100 MAN Figure 27: Aircraft Category Selection Menu Turn the rotary switch to select the desired aircraft category and press the rotary knob to confirm. Note:
The transponder is not yet certified for A/C FixW>5.7t, speed >250kts and helicopters (RotorCr). Therefore, these items are not yet selectable. 3.4.2.1.3.2 Ground Switch To activate or deactivate the Airborne/Ground switch function select GND Switch Support and press the rotary knob. A submenu GND Switch Sup. is displayed. Figure 28: Ground Switch Setup Menu Turn the rotary knob to select Yes or No and press the rotary know to confirm. GND Switch Support Explanation Yes No The Airborne/Ground switch function is enabled. The transponder switches the Airborne/Ground mode automatically depending on the status of the Ground Switch input (see 5.1.3). The Airborne/Ground switch function is disabled. Airborne/Ground mode has to be switched manually using the mode button (see 2.2.2). Table 2: GND Switch Support 3.4.2.1.3.3 Speed Category To configure the maximum speed category select Max. Cruise Speed" and press the rotary knob. A submenu Maximum Speed is displayed. KTX2-F.A-MAN.0001.docx Page 40 of 74 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 EASA.AP445 KTX2-F.0100 MAN Figure 29: Maximum Speed Category Selection Menu Turn the rotary switch to select the desired speed category and press the rotary knob to confirm. KTX2-F.A-MAN.0001.docx Page 41 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 3.4.2.1.3.4 Select GNSS Device If the ADS-B function is used, an appropriate WAAS GNSS source needs to be connected (see 5.1.5). This transponder is certified to TSO-C166b and meets the requirements of AC 20-165B when directly connected to one of the certified or approved GNSS units listed below. This will form the basis of a 14 CFR 91.227 compliant ADS-B installation. Certified GNSS Unit Remarks NexNav Mini WAAS GPS Receiver Part Number 21000 Table 3: Certitified GNSS Units Other aircraft voluntarily equipped with ADS-B like experimental aircrafts, gliders, ultralights etc. may be equipped with an appropriate low-cost WAAS GNSS source. It is encouraged to use only GNSS receivers recommended by TQ. Approved GNSS Unit Remarks Holux GPS Receiver Model: M-215+
Table 4: Approved GNSS Units If other than a recommended GNSS receiver is used the following shall be observed:
Standard NMEA0183 protocol ($GPRMC message required) Update Rate from 5 to 0.5 Hz (0.2 to 2 seconds) To configure the GNSS Device select Select GNSS Device" and press the rotary knob. A submenu GNSS Device is displayed. Figure 30: GNSS Device Selection Menu KTX2-F.A-MAN.0001.docx Page 42 of 74 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 EASA.AP445 KTX2-F.0100 MAN Turn the rotary switch to select the desired GNSS device and press the rotary knob to confirm. GNSS Device Explanation No GNSS Device No WAAS GNSS device is used. The ADS-B function is disabled. NexNav mini A NexNav mini device is used. The ADS-B function is enabled. Approved Device A recommended NMEA WAAS GNSS device is used. The device must support at least the $GxRMC-sentence (as defined in the NMEA 0183 protocol). The ADS-B function is enabled. Table 5: List of supported GNSS Devices If an Approved Device is selected a submenu is displayed for configuring the baud rate. Turn the rotary switch to select the appropriate baud rate and press the rotary knob to confirm. Figure 31: Baud Rate Selection Menu KTX2-F.A-MAN.0001.docx Page 43 of 74 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-F.0100 EASA.AP445 3.4.2.1.3.5 Select Length/Width MAN On the ground, ADS-B transmits encoded aircraft size information which is used by ATC to identify taxiing routes and potential conflicts. To configure the length and width of the aircraft select Length/Width" and press the rotary knob. A submenu Length/Width is displayed. Figure 32: Aircraft Length/Width Configuration Menu To configure the length of the aircraft perform the following procedure:
1. Select Length" and press the rotary knob. The first digit of the length value turns yellow. 2. Turn the rotary knob to change the value. 3. Press the rotary knob again to save the selected digit. The next digit turns yellow. 4. Turn the rotary knob to change the value. 5. Press the rotary knob again to save the selected digit. The length value turns green. Note:
The aircraft length has to be entered in meters rounded to next full meter. E.g.: If the length is 7.2 m, the value must be 08. To configure the width of the aircraft (wingspan) perform the following procedure:
1. Select Width" and press the rotary knob. The first digit of the width value turns yellow. 2. Turn the rotary knob to change the value. 3. Press the rotary knob again to save the selected digit. The next digit turns yellow. 4. Turn the rotary knob to change the value. 5. Press the rotary knob again to save the selected digit. The next digit turns yellow. 6. Turn the rotary knob to change the value. 7. Press the rotary knob again to save the selected digit. The width value turns green. Note:
The aircraft width has to be entered in meters rounded to the next 1/10 meter. E.g.: If the width is 9.31 m, the value must be 09.4 KTX2-F.A-MAN.0001.docx Page 44 of 74 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-F.0100 EASA.AP445 3.4.2.1.3.6 GNSS Antenna Offset MAN The GNSS antenna offset is used together with the aircraft length and width to manage taxiway conflicts. Within the GNSS antenna offset menu, the longitudinal and lateral position offset of the GNSS antenna can be entered. While mainly important for large aircraft, the values can be entered for small aircraft as well. To configure the GNSS antenna offset select GNSS Ant. Offset and press the rotary knob. A submenu GNSS Ant. Offset is displayed. Figure 33: GNSS Antenna Offset Configuration Menu To configure the longitudinal offset of the GNSS antenna perform the following procedure:
1. Select Long." and press the rotary knob. The first digit of the offset value turns yellow. 2. Turn the rotary knob to change the value. 3. Press the rotary knob again to save the selected digit. The next digit turns yellow. 4. Turn the rotary knob to change the value. 5. Press the rotary knob again to save the selected digit. The offset value turns green. Note:
The longitudinal offset has to be entered in meters measured from the nose of the aircraft. E.g.: If the offset is 3.2 m, the value must be 04. To configure the lateral offset of the GNSS antenna perform the following procedure:
1. Select Lat." and press the rotary knob. The +/- sign of the offset value turns yellow. 2. Turn the rotary knob to change the sign. 3. Press the rotary knob again to save sign value. The first digit of the offset value turns yellow. 4. Turn the rotary knob to change the value. 5. Press the rotary knob again to save the selected digit. The next digit turns yellow. 6. Turn the rotary knob to change the value. 7. Press the rotary knob again to save the selected digit. The offset value turns green. Note:
For most small aircraft a value of 00 is adequate. 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. The lateral offset has to be entered in meters measured from longitudinal (Roll) axis of the aircraft. E.g.: If the offset is 1.3 m to left side, the value must be -02. KTX2-F.A-MAN.0001.docx Page 45 of 74 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-F.0100 EASA.AP445 3.4.2.1.4 Save Flight ID MAN To save a Flight ID configuration select Save and press the rotary knob. The Flight ID menu for adding, modifying and deleting a Flight ID configuration will be displayed after the configuration is saved. 3.4.2.2 Modify Flight IDs To modify a Flight ID select Modify and press the rotary knob. A submenu Select FID is displayed. See 3.4.2.4 for details. After the desired Flight ID is selected the submenu Edit FID Param. is displayed and the parameters of the Flight ID can be modified (see 3.4.2.1). 3.4.2.3 Delete Flight IDs To delete a Flight ID select Delete and press the rotary knob. A submenu Select FID is displayed. See 3.4.2.4 for details. After the desired Flight ID is selected the submenu Delete FID is displayed. Figure 34: Delete Flight ID Menu To delete the Flight ID turn the rotary knob to select Yes and press the rotary knob. The Flight ID is deleted and the Flight ID menu is displayed. If you select No and press the rotary knob the Flight ID is not deleted and the Flight ID menu is displayed. The FID and AA-Code are only displayed for information purposes. 3.4.2.4 Multiple Flight IDs In case multiple Flight IDs are configured a selection menu is displayed where necessary. The selection menu for multiple Flight IDs allows the selection of an already configured Flight ID (see 3.4.2.1) for the operation or configuration of the transponder. The selection menu may consist of two pages (see note below). KTX2-F.A-MAN.0001.docx Page 46 of 74 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 EASA.AP445 KTX2-F.0100 MAN Figure 35: Multiple Flight ID Selection Menu Turn the rotary knob to select the desired Flight ID. Press the rotary knob to confirm the selection. The transponder will then use the selected configuration. Note:
If more than four Flight IDs are configured turn the rotary knob clockwise until the next page is shown. To go back to the previous page turn the rotary knob counterclockwise. 3.4.3 Modify VFR To configure the VFR squawk code Modify VFR" and press the rotary knob. A submenu Modify VFR is displayed. Figure 36: Modify VFR Code Menu To change the VFR squawk code perform the following procedure:
1. Press the rotary knob. The first digit of the standby squawk turns yellow. 2. Turn the rotary knob to change the value. 3. Press the rotary knob again to save the selected digit. The next digit turns yellow. 4. Repeat steps 2 and 3 until all four (4) digits are set to desired VFR squawk code. KTX2-F.A-MAN.0001.docx Page 47 of 74 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-F.0100 MAN EASA.AP445 Note:
Make sure, that you enter the correct VFR squawk code for the particular country where your aircraft is operated. Examples:
Germany:
USA:
VFR Squawk = 7000 VFR Squawk = 1200 KTX2-F.A-MAN.0001.docx Page 48 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 3.4.4 Factory Reset In certain cases it may be necessary to perform a factory reset. Performing a factory reset will reset all settings to their factory defaults. To perform a factory reset select Factory Reset and press the rotary knob. A submenu Factory Reset is displayed. Figure 37: Factory Reset Menu To perform a factory reset turn the rotary knob to select Yes and press the rotary knob. A notification is displayed which requests a restart of the transponder. 3.4.5 Test Menu The second page of the setup menu contains only the test menu. To enter the test menu select Test Menu and press the rotary knob. A submenu Test Menu is displayed. Figure 38: Test Menu To calibrate the altitude offset select Altitude Offset and press the rotary knob. A submenu Altitude Offset is displayed (see 3.4.5.1). To enter the test mode select Test Mode and press the rotary knob. A submenu Test Mode is displayed (see 3.4.5.2). To show some device information select Device Information and press the rotary knob. A submenu Device Info is displayed (see 3.4.5.3). KTX2-F.A-MAN.0001.docx Page 49 of 74 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-F.0100 EASA.AP445 3.4.5.1 Altitude Offset Calibration MAN The Altitude Offset Calibration allows you to adjust the built-in altitude encoder to ensure that the flight level transmitted by the transponder complies with all relevant standards. This process is normally carried out every 24 months, as part of the altimeter checks on the aircraft. The maximum allowed difference between the primary altimeter and the altitude encoder is 125 feet according to ETSO C88a. The altitude encoder in the transponder is extremely accurate, has an excellent long-term stability and is accurately calibrated during manufacture. But it is possible that a combination of allowed accuracy deviations in the altitude encoder and the primary altimeter may show an altitude difference exceeding 125 feet. In that case it is recommend to perform an altitude offset calibration. 3.4.5.1.1 Calibration Equipment To perform the altitude offset calibration the transponder needs to be powered up. Additionally a pitot static test set is needed together with the appropriate adapters to connect to the static port on the aircraft. The pitot static test set should be able to drive the altitude from sea level to above the service ceiling of the aircraft. Note:
For the calibration procedure no transponder test set is required. During the calibration procedure all necessary information is displayed. Nevertheless a transponder test set can be used to verify the transmissions of the transponder. 3.4.5.1.2 Calibration Procedure Figure 39: Altitude Offset Calibration Menu To perform the altitude offset calibration perform the following procedure:
1. Select Altitude and press the rotary knob. The first digit of the altitude set point turns yellow. 2. Turn the rotary knob to change the value. 3. Press the rotary knob again to save the selected digit. The next digit turns yellow. 4. Repeat steps 2 and 3 until all digits are set to desired altitude set point. Note: It is recommended to use 18000 ft as altitude set point. 5. On the pitot static test set drive the altitude to the set point value as entered before and wait until the pressure has stabilized. 6. Select Start and press the rotary knob. The calibration procedures is started. During the Delta value shows three dashes (---). KTX2-F.A-MAN.0001.docx Page 50 of 74 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-F.0100 EASA.AP445 MAN 7. After a few seconds either the Delta value is showing the altitude offset value or a notification is displayed. In a normal case the calibration procedure was successfully performed and the new altitude offset value is stored. In a rare case the offset value determined by the calibration procedure is beyond the limits. Possible reasons can be:
Altitude set point values of transponder and static test set do not match.
=> Check the settings. Failure in the static port connection from the static test set to the transponder.
=> Check the installation. Failure of the altitude encoder.
=> Send the unit for servicing. To verify the altitude measurement the following procedure must be performed:
1. Switch off the transponder. 2. Switch on the transponder in Setup Mode and enter the Test Mode (see 3.4.5.2). 3. On the pitot static test set drive the altitude to -1000 feet. 4. Verify that the altitude displayed on the transponder correspond within the 125 foot tolerance. Additionally verify the altitude value transmitter by the transponder. 5. Repeat this procedure for all altitudes to the service ceiling of the aircraft in steps of 1000 feet. 3.4.5.2 Test Mode The submenu Test Mode displays the following internal measurements:
Operating voltage (Battery) DC Converter voltage (power supply for the transmitter) Altitude (in feet) Figure 40: Test Mode Menu 3.4.5.3 Device Info The submenu Device Info displays the checksum of the software and the serial number of the device. KTX2-F.A-MAN.0001.docx Page 51 of 74 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 EASA.AP445 KTX2-F.0100 MAN Figure 41: Device Info Menu KTX2-F.A-MAN.0001.docx Page 52 of 74 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-F.0100 EASA.AP445 4. Errors, Warnings and Notifications MAN The transponder distinguishes 3 types of faults:
Degrading failures Limiting failures Severe failures Additionally notifications are displayed where appropriate. 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 4.1 Degrading failures If a degrading failure is detected the transponder continues to operate. But its performance may be reduced. Once detected a warning message is displayed. This message can be confirmed by pressing the rotary knob. The normal operation display will be shown again with the failure indication. To handle a nonrecurring cause the transponder can be switched off and on again. If the error reoccurs the transponder can be operated as usual but with reduced performance. Note:
Only the last failure is shown except for the battery voltage warning. KTX2-F.A-MAN.0001.docx Page 53 of 74 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-F.0100 EASA.AP445 The following table shows a list of all degrading failures of the transponder. MAN Failure Explanation Degradation Action / Remark DC converter Bad antenna TX supply voltage is low TX output power is reduced. Send unit for servicing. Antenna VSWR is bad (very high) TX output power is reduced. Transmitter weak TX output power is too low TX output power is reduced. Check antenna installation (cable, connectors etc.) to resolve the problem before next flight. If no root cause can be discovered, send unit for servicing. Check antenna installation (cable, connectors etc.) to resolve the problem before next flight. If no root cause can be discovered, send unit for servicing. Flight Level The altimeter reports a failure No barometric altitude information is sent. Check connection and function of static air port to resolve the problem before next flight. If no root cause can be discovered, send unit for servicing. Low battery voltage Battery voltage is below 11 Volts See below. See below. Very low battery voltage Battery voltage is See below. See below. below 7.5 Volts Table 6: Degrading Failures 4.1.1 Low Battery Voltage If the supply voltage of the transponder falls below 11 V DC, a yellow indication BAT LOW is shown in the center of the display. The indication is shown as long as the voltage is too low. Figure 42: Low Battery Voltage Note:
The transponder is designed to operate above 9 V DC. Do not operate the unit below 9 volts. KTX2-F.A-MAN.0001.docx Page 54 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 Degradation:
TX output power may be reduced. Possible Reasons:
1. Battery exhausted. 2. Voltage of electric generator is low. Actions:
1. Exchange or charge the battery. 2. Check electric generator. 4.1.2 Very Low Battery Voltage If the supply voltage of the transponder falls below 7.5 V DC, a red indication BAT LOW is shown in the center of the display. The indication is shown as long as the voltage is too low. Figure 43: Very Low Battery Voltage Degradation:
Transponder is switched into STBY mode. No further operation possible. Possible Reasons:
1. Battery exhausted. 2. Voltage of electric generator is very low. Actions:
1. Exchange or charge the battery. 2. Check electric generator. KTX2-F.A-MAN.0001.docx Page 55 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 4.2 Limiting failures If no FID-Code (Flight ID) is entered or if the corresponding Aircraft Address (AA-Code) is missing or incomplete, the following failure is displayed after switching on the transponder:
Figure 44: Missing AA-Code To fix this error an appropriate FID and AA-Code has to be configured as described in chapter 3.4.2. Note:
This message can be cleared by pressing the rotary knob. The transponder will then operate in A/C mode only. 4.3 Severe failures In case a severe failure is detected, a message (example) as shown below is displayed. No further operation of the transponder is possible. No replies will be made to interrogations and ADS-B out is switched off. Figure 45: Critical Error (Example) To handle a nonrecurring cause the transponder can be switched off and on again. But if the error reoccurs the transponder must be switched off. KTX2-F.A-MAN.0001.docx Page 56 of 74 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-F.0100 EASA.AP445 The following table shows a list of all degrading failures of the transponder. MAN Displayed Error Explanation Remarks EEPROM access Severe operation error. No access Send unit for servicing. to EEPROM. FPGA communication FPGA internal Severe operation error. No access to FPGA. Send unit for servicing. Severe operation error. FPGA internal failure. Send unit for servicing. ADC Severe operation error. No access to ADC. Send unit for servicing. Trans. out. power Severe operation error. No or very low TX output power. Check installation (power cable, antenna cable, etc.). If no root cause can be discovered, send unit for servicing. Antenna failure Severe operation error. Antenna not connected or Antenna VSWR is very high. Check installation (power cable, antenna cable, etc.). If no root cause can be discovered, send unit for servicing. MCU Severe operation error. MCU internal failure. Send unit for servicing. Unknown Error Severe operation error. Check installation (power cable, antenna cable, etc.). If no root cause can be discovered, send unit for servicing. Table 7: Severe Failures KTX2-F.A-MAN.0001.docx Page 57 of 74 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-F.0100 EASA.AP445 4.4 Notifications MAN 4.4.1 GNSS Data CRC Failure Figure 46: GNSS CRC Failure Possible Reasons:
Invalid data from GNSS source. Actions:
Check installation, cable, connections and configuration of the installed GNSS source. 4.4.2 Do System Restart The following message is displayed if a restart of transponder is necessary. Figure 47: System Restart Actions:
Switch the transponder off and on again KTX2-F.A-MAN.0001.docx Page 58 of 74 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. KTX2-F.0100 MAN TQ Aviation 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 connections, except for the antenna, see chapter 5.2.2 for details. The positive supply line needs to be protected by a 3A slow blow fuse!
The transponder should be connected to an uninterruptible power supply as short power interrupts may cause the transponder to restart in STBY Mode or in Multiple Flight ID selection. 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) must 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 transmission of a competing transmitter for the duration of the pulse train transmission. The transponder 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, see chapter 5.2.2. All equipment connected to the suppression line must be re-inspected and reapproved from a qualified avionic technician before operation. Use only shielded lines. 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 no-weight-on-wheel (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, see chapter 5.2.2. KTX2-F.A-MAN.0001.docx Page 59 of 74 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-F.0100 MAN EASA.AP445 This option must additionally be activated in the Setup. For details on configuration please refer to chapter 3.4.2.1.3.2. 5.1.4 Static Air Port The transponder has a built-in altitude encoder which must be connected to the same source of static pressure as the primary altimeter on the aircraft. For this purpose the transponder has a hose connection at its rear side for nominal 5mm or 3/16 inch tubing (inside diameter). Connect the static air connection to the static pressure port and ensure a tight connection with a suitable hose clamp. 5.1.5 GNSS Interface A GNSS source can be connected to the serial interface (RS232) providing GNSS position data for use of ADS-B out. Requirements:
Required GNSS hardware:
o NexNav Mini (Part-No. 21.000) which turns the transponder into a 14 CFR 91.227 compliant device as required for TCd aircraft (FAA 2020 mandate). or o Standard NMEA0183 RMC data stream including the RMC-sub-format
(4800/9600/19200/38400 Baud) for aircrafts which do not require the ADS-B requirements defined in 14 CFR 91.227. GNSS hardware needs to be connected to pin 13 (RX-RS232) and optionally pin 2 (TX-RS232) of the D-SUB connector (see chapter 5.2.2). Power supply needs to be provided separately considering the required operating voltage for the GNSS hardware. The WAAS GNSS device needs to be selected in the setup menu (see chapter 3.1.4.4). Note:
For connection to the NexNav Mini device, a proprietary cable is available from TQ. Please contact you dealer for more information. If a standard NMEA0183 WAAS GNSS source is sufficient for your aircraft (LSA, Experimental, Ultralight etc.) you should consider brands recommended by TQ to avoid incompatibilities or malfunctions. Note:
For correct function of the movement detection an update rate of 5 Hz is recommended for NMEA devices. 5.1.6 Antenna Connector The antenna is connected to a single coaxial connector (SMA) at the rear side of the transponder. 5.1.6.1 L-Band ADS-B Antennas The L-Band antenna used with the KTX2 must fulfil to the following specifications:
KTX2-F.A-MAN.0001.docx Page 60 of 74 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 EASA.AP445 KTX2-F.0100 MAN Standard 50 , vertically polarized antenna with a VSWR < 1.7:1 at 1090 MHz. TSO-C66( ), TSO-C74( ), TSO-C112( ) , or TSO-154c antennas that also meet the VSWR specification. Only the L-Band antennas listed in the table below have been tested for compatibility with transponder installations. Manufacturer Part Number Connector Type Remarks RAMI Comant AV-74 CI-105 Comant CI-105-11 Table 8: L-Band Antennas 5.1.6.2 Antenna Installation BNC BNC TNC The antenna should be installed according to the manufacturers instructions. The following considerations should be taken into account for the antenna installation:
The antenna should be placed not directly near any projections, the engine(s) and propeller(s). It should also be placed not directly near landing gear doors, access doors or others openings which will break the ground plane for the antenna. The antenna should be mounted on the bottom surface of the aircraft and in a vertical position when the aircraft is in level flight. The antenna should not be mounted within 3 feet of the ADF sense antenna or any COMM antenna and 6 feet from the transponder to the DME antenna. Where practical, the antenna location should be chosen to keep the cable lengths as short as possible and to avoid sharp bends in the cable to minimize the VSWR. To prevent RF interference, the antenna must be physically mounted at a minimum distance of 3 feet from the transponder. Electrical connection to the antenna should be dust and water proof to avoid loss of efficiency as a result of the presence of liquids or moisture. All antenna feeders must be installed in such a way that a minimum of RF energy is radiated inside the aircraft. 5.1.6.3 Antenna Cable The transponder is designed to fulfil the ADS-B Class 1 requirements allowing a maximum loss of 2 dB in the connectors and cable used to connect it to the antenna. Exceeding this loss will degrade the transmitter output power and receiver sensitivity. A typical installation needs two (2) connectors at each end of the antenna cable. Calculating a loss of 0.25dB for each connector allows a loss of 1.5dB for the cable itself. An acceptable cable must have the following characteristics:
Less than 1.5dB loss for the cable length needed. Characteristic impedance of 50 Ohms. KTX2-F.A-MAN.0001.docx Page 61 of 74 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 EASA.AP445 KTX2-F.0100 MAN Double braid screens or a foil and braid screen. Once the cable length from the transponder to the antenna is known, a cable type can be chosen which has a loss per meter low enough to meet the above requirements (see table below). Note:
Low loss cable typically uses foamed or cellular dielectrics and foil screens. These make such cables especially prone to damage from too-tight bends or from momentary kinking during installation. Once kinked, these cables do not return to full performance when straightened. The following table is shows a list of some common cable types and the maximum usable lengths. Cable Type Max Length in meters (feet) Insertion Loss dB/meter
(db/100ft)1 Remarks RG-400 M17/128-RG400 RG-304 M17/112-RG304 RG-393 M17/127-RG393 Carlisle IT Type 3C142B Carlisle IT Type 311601 Carlisle IT Type 311501 Carlisle IT Type 311201 Carlisle IT Type 310801 2.5 (8 2) 0.6 (18.5) 4.2 (13 9) 0.36 (11.1) 5 (16 5) 0.3 (9.2) 3.1 (10 2) 0.48 (14.5) 5.2 (17 1) 0.29 (8.7) 6.5 (21 4) 0.23 (7.1) 8.3 (27 4) 0.18 (5.6) 12.5 (41) 0.12 (3.6) Table 9: Common Antenna Cables When routing the cable, ensure that you:
Keep the cable length as short as possible. Avoid routing the cable round tight bends. Avoid kinking the cable, even temporarily during installation. Secure the cable so that it cannot interfere with other systems. Route the cable away from any heat sources. 1 RG type coaxial cable insertion loss can vary significantly between manufacturers. The insertion loss for RG type cables shown in this column is considered 'worst case'. Refer to the cable manufacturer's specification sheet for actual attenuation (insertion loss) for the cable being used. KTX2-F.A-MAN.0001.docx Page 62 of 74 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 EASA.AP445 KTX2-F.0100 MAN Route the cable away from potential interference sources such as ignition wiring, 400Hz generators, fluorescent lighting and electric motors. Allow a minimum separation of 300mm (12 inches) from an ADF antenna cable. Note:
In case an already installed antenna can be further used (old transponder is replaced) and the existing connector does not fit, it is recommended to replace the connector. Alternatively, an adapter from the existing connector to a SMA male type connector can be used. But this will add an additional loss of typical 0.1 0.2 dB to the installation which must be considered. If the total loss of 2 dB is exceeded the cable must be replaced. Note:
An SMA<->TNC adapter is available from TQ. KTX2-F.A-MAN.0001.docx Page 63 of 74 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-F.0100 EASA.AP445 5.2 Wiring MAN 5.2.1 Conductor Cross Section Power Supply (Batt. Plus, GND):
Signals:
AWG22 (0.38 mm) AWG20 (0.62 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 harness comply with common aviation wiring standards. Consult your approved aviation shop for installation details. 5.2.2 Wiring Scheme Figure 48: Wiring KTX2-F.A-MAN.0001.docx Page 64 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 6. Drawings Figure 49: Dimensions of KTX2-F Standard round format KTX2-F.A-MAN.0001.docx Page 65 of 74 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 EASA.AP445 KTX2-F.0100 MAN Figure 50: Panel Cut-Out KTX2-F.A-MAN.0001.docx Page 66 of 74 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-F.0100 EASA.AP445 7. Technical Data MAN 7.1 General Designation Authorization EASA.21O.10070633 Certification ETSO-C112e / TSO-C112e ETSO-C88b / TSO-C88b ETSO-C166b_A3 / 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-KTX2F Dimensions KTX2-F 158.75 x 41.4 x 190.35 +/- 1 mm
(6.25 x 1.63 x 7.5) pure housing Weight KTX2-F 0.600 kg Mounting KTX2-F: cut-out dimensions 155 x 38 +/- 0.2 mm
(6.1 x 1.5) installation depth short frame: 140 +/- 0.2 mm (5.5) long frame: 236.4 +/- 0.2 mm (9.3) Temperature ranges:
Operation Storage
-20 C to +55 C
-55 C to +85 C Maximum 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. Category
[C4Z]CAB[SM]XXXXXXZ[BBB][AC]TB[B2F2]XXAX Software Category ED-12C (RTCA DO-178C) Level C Hardware Category DO-254 Level C Power supply 9 V DC to 33V DC KTX2-F.A-MAN.0001.docx Page 67 of 74 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 EASA.AP445 KTX2-F.0100 MAN Designation Power consumption depending on the number of requests = 0.2 to 1.0A (@ 12V DC) Illumination 0.02A (@ 12V DC) Fuse External fuse required: 3A, slow-blow Compass security distance 300 mm (12) Table 10: Technical Data KTX2-F.A-MAN.0001.docx Page 68 of 74 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-F.0100 EASA.AP445 7.2 Transmitter Receiver MAN TRANSMITTER Reply transmission frequency 1090 1MHz RF Peak Power Output 54dBm (250 W) nominal at antenna connector, 51dBm (125 W) minimum at antenna base
(allowing 0.5dB connector loss and 1.5dB cable loss) Squitter Transmitted periodically at random intervals, full self-
verification of data and occurrence Table 11: Transmitter Data RECEIVER Receiving frequency 1030 1MHz 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. Table 12: Receiver Data General ICAO 24-bit Aircraft Address
(Hex-Code) Aircraft Address as assigned by National Aviation Authority 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. Table 13: General Data KTX2-F.A-MAN.0001.docx Page 69 of 74 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. KTX2-F.0100 MAN TQ Aviation 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. 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 reasonable protection against harmful interference in a residential installation. This transponder 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. However, 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 determined by turning the equipment off and on, the user is encouraged to try to correct the interference by one or more of the following measures:
Reorient or relocate the receiving antenna. Connect the equipment into an outlet on a circuit different from that to which the receiver Increase the separation between the equipment and receiver. is connected. Consult the dealer or an experienced radio/TV technician for help. 8.2 Compliance Notice: This device complies with Part 15 of the FCC Rules and with Industry Canada license-
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. 8.3 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-F.A-MAN.0001.docx Page 70 of 74 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. KTX2-F.0100 MAN TQ Aviation EASA.AP445 9. Maintenance 9.1 Periodic Maintenance This 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 must be accomplished following any repair action. Repairs must 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 malfunction, 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-F.A-MAN.0001.docx Page 71 of 74 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 EASA.AP445 KTX2-F.0100 MAN 10. EXCLUSIVE LIMITED WARRANTY and LIMITATIONS ON LIABILITY 1. Our warranty and liability is based on legal provisions, provided nothing else has been agreed. 2. Delivery items may differ from product illustrations, especially in regard with color and weight. Such differences do not constitute a defect of quality which is relevant for warranty claims. 3. The Customer's warranty rights are subject to the fact that the Customer has properly fulfilled its obligations of examination and notification of defects under 377 HGB (Commercial Code). Inasmuch as the Customer is a consumer, the delivery will be considered as approved if written notice of defects is not received within a period of ten (10) working days after arrival of the goods. If the defect was not noticeable in an ordinary inspection the period is extended to four (4) weeks. If the claim for defects is not files in good times, warranty shall be excluded. 4. Our warranty obligation to the Customer ends 36 months after delivery to the Customer or 24 months after delivery to the end customer, whichever period expires first. The warranty obligation for claims for subsequent performance, replacement deliveries or replacement performance after a substitute performance, replacement delivery or replacement performance exist within the scope of the remaining period of the warranty term as stated above. 5. The warranty period expiries prematurely, however, if repair attempts or other modifications are made to the contractual objects by the Customer or agents it has commissioned without the prior agreement. 6. Our liability for damages attributable to it or its agents is, in cases of gross negligence or damage with negligence, an obligation that is significant for achieving the purpose of the contract and is financially and materially limited to the business and product liability insurance cover concluded. Any further liability is excluded. KTX2-F.A-MAN.0001.docx Page 72 of 74 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-F.0100 EASA.AP445 11. Software License Conformity MAN OpenSource-Software has been developed with the collaboration of many different developers under differing conditions. Thus, any liability for consequential damages arising out of the use of OpenSource-
Software shall, if not compulsory regulated by law, be excluded or limited to modifications or alterations of OpenSource-Software which can clearly and definably be assigned to TQ or its auxiliary persons. Used licenses:
TQSSLAv1.0.2 BSD-3-Clause GPL-3.0-with-GCC-exception Zlib ATT-style Copyright holders, warranty disclaimer and license text can be downloaded from:
https://www.tq-group.com/en/support/downloads/tq-software-license-conditions/
or contact the product management per e-mail: mailto:support@tq-general-aviation.com KTX2-F.A-MAN.0001.docx Page 73 of 74 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 EASA.AP445 KTX2-F.0100 MAN TQ-Systems GmbH Support E-mail:
support@tq-general-aviation.com Internet:
www.tq-avionics.com KTX2-F.A-MAN.0001.docx Page 74 of 74 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.
| 1 | Photos Internal | Internal Photos | 783.20 KiB | February 09 2019 |
Annex B 1-8673/19-01-01_AnnexB Internal photos of the Equipment Under Test This addendum is electronically signed and valid without handwritten signature. For verification of the electronic signatures, the public keys can be requested at the testing laboratory. Document authorized:
Christoph Schneider Lab Manager Radio Communications & EMC CTC advanced GmbH Untertuerkheimer Str. 6-10 66117 Saarbruecken / Germany Phone: +49 681 5 98 - 0 Fax: +49 681 5 98 - 9075 web: ctcadvanced.com e-mail: mail@ctcadvanced.com Photos Photo 1 Photo 2 2019-06-25 Document No. 1-8673/19-01-01_AnnexB 2/5 Photo 3 Photo 4 2019-06-25 Document No. 1-8673/19-01-01_AnnexB 3/5 Photo 5 2019-06-25 Document No. 1-8673/19-01-01_AnnexB 4/5 Document history Version Applied changes initial release
- END OF DOCUMENT -
Date of release 2019-06-25 2019-06-25 Document No. 1-8673/19-01-01_AnnexB 5/5
| 1 | Photos External | External Photos | 1002.38 KiB | February 09 2019 |
Annex A 1-8673/19-01-01_AnnexA External photos of the Equipment Under Test This addendum is electronically signed and valid without handwritten signature. For verification of the electronic signatures, the public keys can be requested at the testing laboratory. Document authorized:
Christoph Schneider Lab Manager Radio Communications & EMC CTC advanced GmbH Untertuerkheimer Str. 6-10 66117 Saarbruecken / Germany Phone: +49 681 5 98 - 0 Fax: +49 681 5 98 - 9075 web: ctcadvanced.com e-mail: mail@ctcadvanced.com Photos Photo 1 Photo 2 2019-06-25 Document No. 1-8673/19-01-01_AnnexA 2/7 Photo 3 Photo 4 2019-06-25 Document No. 1-8673/19-01-01_AnnexA 3/7 Photo 5 Photo 6 2019-06-25 Document No. 1-8673/19-01-01_AnnexA 4/7 Photo 7 Photo 8 2019-06-25 Document No. 1-8673/19-01-01_AnnexA 5/7 Photo 9 2019-06-25 Document No. 1-8673/19-01-01_AnnexA 6/7 Document history Version Applied changes initial release
- END OF DOCUMENT -
Date of release 2019-06-25 2019-06-25 Document No. 1-8673/19-01-01_AnnexA 7/7
| 1 | Confidentiality Request Letter - Permanent | Cover Letter(s) | 48.17 KiB | February 09 2019 |
CONFIDENTIALTY REQU EST for Certification Service in USA Federal Communication Commission Equipment Authorization Division, Application Processing Branch 7435 Oakland Mills Road Columbia, MD 21048 2019-06-28 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.KTX2F Model name KTX2-F Mode S Transponder For the product stated above, we request permanent confidentiality for exhibits which contain Operational Description, Block Diagram, Schematics, Parts 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. sincellv. t- ^/w.. Head of Design Organisation EASA.AP445 TQ-Systems GmbH Mhlstrae 2, Gut Delling, 82229 Seefeld, Germany Tel.: +498'l 53 9308-469 Fax: +498153 9308-7469 thomas.eilers@tq-qrouo.com Amtsgericht Mnchen, HRB 105 018, UST-ldNr. DE 811 607 913 Geschftsfhrer: Dipl.-lng. (FH) Detlef Schneider, Dipl.-lng. (FH) Rdiger Stahl, Dipl.-lng. (FH) Stefan Schneider
| 1 | Notification Letter to the FAA | Cover Letter(s) | 113.20 KiB | February 09 2019 |
TQ-Systems GmbH Elektronische Baugruppen und Systeme TQ-Systems GmbH, Gut Delling / Mhlstrae 2, 82229 Seefeld, Germany FAA - Federal Aviation Administration Office of Spectrum Policy and Management ASR-1, 800 lndependence Ave., SW., Washington, DC 20591 United States of America Date:
Page POC:
Dept.:
Phone:
Telefax:
E-Mail:
2019.08.22 1of 2 Eilers, Thomas TQ EWA DE
+49(0)8153 9308469
+49(0)8153 9308-7469 thomas.eilers@tq-grou p. com Notification of FCC Equipment Certification Application for TQ-Systems KTX2-F Mode S Transponder FCG lD: 2ANFF-KTX2F Dear Ladies and Gentlemen, ln accordance with FCC Rules and Regulations, CFR Title 47, Part 87, Chapter l; Part 87 - Aviation Services, notification is hereby given from TQ-Systems to file for FCC Equipment Certification for the TQ-Systems KTX2-F Mode S Transponder. Part numbers:
. FCC lD:
. ETSO authorisation number:
o EASA ETSO Authorization:
. Frequency range:
o Output Power:
o Emission designator:
295153 (flat variant in 160mm format) 2ANFF-KTX2F E4S4.210.10070633 ETSO-C88b (TSO-C88b), ETSO-C1 12e (TSO-C112e), ETSO-C 1 66b_43 (TSO-C1 66b) 1090 r 1 MHz (Tx); 1030 t 1 MHz (Tx);
250W (> 24dBW) @ 9 to 33VDc 9MBOMlD 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-F Mode S Transponder FCC Documentation", and its contents are as listed in ATTACHMENT A.
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not hesitate to contact me TQ-Systems GmbH i.V. Thomas Eilers Head of Design Organisation EASA.AP445 TQ-SystemrGmbHlGutDellinglMhlstrae2l82229SeefeldlTel.+4981539308-0lFax+498'l534223lwww.tq-group.comlinfo@tq-group.com Geschfthrer: Detlef Schneder, Rdger Sthl, Stefn Schneider I Amtsgericht Mnchen I HRB-Nr. I 05 0 l I I USt-ldNr. DE 252 251 764 I WEEE-Re9.-Nr. DE 1631 I 528 Donner&Reusche|1812200303001Kto.10392101DE282003030001039210001USD:Kto.31039210lDE87200303003l0392l000lBlCCHDBDEHH Hypoverensbrnk Mllnchen I BLZ 700 202 70 I Kto. 85 603 205 I DE98 7OO2 O27O 0085 032 05 I USD:Kto. 885 627 056 I DE68 7002 0270 0885 6270 56 I BIC HYVEDEMM VRBlnkStlrnberglBLZ70093200lKto.5l23003lDE65700932000005l23003l8lCGFNODEFISTHlEsgeltenunsereAllgemeinenGeschftsbedingungen ATTACHMENT A lncluded support Information 1. Test report no.: 1-8673_19-01-02 2. Test report no.: 1-8673_19-01-O1_AnnexA 3. Test report no.: 1-8673_19-01-O1_AnnexB 4. Test report no.: 1-8673_19-01-O1_AnnexC 5. Test report no.: 1-8178_19-01-O2_AnnexD (Test system) 6. Operational Description: KTX2-F.A-HDD.0001 7. Schematics part 1: KTX2.D|G.SP.0600 8. Schematics part2: KTX2-F.HD.SP.0200 9. Schematics part 3: KTX2.RF.SP.0600 10. Schematics part 4: KTX2-F.Bridge.SP.0200 11. Schematics part 5: KTX2-F.LCD.SP.0200 12. Schematics part 6: KTX2-F.LED.SP.0200 13. Mechanical Drawing KTX2-F Housing - 315138.0101 14. Mechanical Drawing KTX2-F Hose Connector - 304593.0102 15. Mechanical Drawing KTX2-F Cover - 315133.0100 16. KTX2-DIG.SLE.0600 = Bill of Material 17. KTX2-F.V2-KPL.SLE.0100 = Bill of Material 18. KTX2.RF.SLE.0600 = Bill of Material 19. KTX2-F HA.SLE.O100 = Bill of Material 20. KTX2-F Mode S Transponder Architecture - Master Block Diagram 21. KTX2-F.A-MAN.0100.en.= Operation and lnstallation Manual KTX2-F Mode S Transponder 22. KTX2-F.A-DDP.0100 = Declaration of Design and performance (Operational Description) 23. Label= KTX2-F Label ldentification 24. KRT2-F.A-HDD.O100 = Detailled Design Document 25. 21O.10070633_CERT_REV_0 20190821 = ETSO authorization certificate E4S4.21O.10070633 26. Confidentiality Request for Certification Service in USA TQ-SystemsGmbHlGutDellnglMhlstrae2l82229SeefeldlTel.+498'1539308-0lFax+49815342231www.tq-group.comlnfootq-group.com Geschftlijhrer: DetlefSchneider, RidigerStahl,Stefan Schneider I Amtsgericht Mnchen I HRB-Nr.105 018 I Ust-ldNr. DE 252 251 764 I WEEE-Reg.-Nr, DE4631 1528 Donner &Reusche| 1 8L2200 303 00 1 Kto. 1 039 210 1 D828 2003 0300 0103 9210 00 1 USD:Kto.31 039 210 1 DE87 2003 0300 3103 9210 00 1 81C CHDBDHH Hypovefen3blnk mllnchen I BLzTOO 2O270 I Kto. 85 603 205 I DE98 7OO2 0270 00A5 6032 05 I USDrKto. 8A5 627 056 I DE68 7002 0270 0885 6270 56 I BIC HYVEDEMM VR Bnk Strrnberg I BLZ 700 932 00 I Kto. 5 123 003 I DE65 7009 3200 0005 1230 03 I BIC GENODEFISTH I Es gelten unsere Allgemeinen Geschftsbedingungen
| frequency | equipment class | purpose | ||
|---|---|---|---|---|
| 1 | 2019-09-02 | 1090 ~ 1090 | TNB - Licensed Non-Broadcast Station Transmitter | Original Equipment |
| app s | Applicant Information | |||||
|---|---|---|---|---|---|---|
| 1 | Effective |
2019-09-02
|
||||
| 1 | Applicant's complete, legal business name |
TQ Systems GmbH
|
||||
| 1 | FCC Registration Number (FRN) |
0026768952
|
||||
| 1 | Physical Address |
Muehlstrasse 2 Gut Delling
|
||||
| 1 |
Muehlstrasse 2
|
|||||
| 1 |
Seefeld, N/A
|
|||||
| 1 |
Germany
|
|||||
| app s | TCB Information | |||||
| 1 | TCB Application Email Address |
T******@ctcadvanced.com
|
||||
| 1 | TCB Scope |
B3: Maritime & Aviation Radio Services equipment in 47 CFR parts 80 & 87
|
||||
| app s | FCC ID | |||||
| 1 | Grantee Code |
2ANFF
|
||||
| 1 | Equipment Product Code |
KTX2F
|
||||
| app s | Person at the applicant's address to receive grant or for contact | |||||
| 1 | Name |
S****** G********
|
||||
| 1 | Telephone Number |
+4917********
|
||||
| 1 | Fax Number |
+4981********
|
||||
| 1 |
s******@tq-group.com
|
|||||
| app s | Technical Contact | |||||
| n/a | ||||||
| app s | Non Technical Contact | |||||
| n/a | ||||||
| app s | Confidentiality (long or short term) | |||||
| 1 | Does this application include a request for confidentiality for any portion(s) of the data contained in this application pursuant to 47 CFR § 0.459 of the Commission Rules?: | Yes | ||||
| 1 | Long-Term Confidentiality Does this application include a request for confidentiality for any portion(s) of the data contained in this application pursuant to 47 CFR § 0.459 of the Commission Rules?: | No | ||||
| if no date is supplied, the release date will be set to 45 calendar days past the date of grant. | ||||||
| app s | Cognitive Radio & Software Defined Radio, Class, etc | |||||
| 1 | Is this application for software defined/cognitive radio authorization? | No | ||||
| 1 | Equipment Class | TNB - Licensed Non-Broadcast Station Transmitter | ||||
| 1 | Description of product as it is marketed: (NOTE: This text will appear below the equipment class on the grant) | Mode-S Transponder | ||||
| 1 | Related OET KnowledgeDataBase Inquiry: Is there a KDB inquiry associated with this application? | No | ||||
| 1 | Modular Equipment Type | Does not apply | ||||
| 1 | Purpose / Application is for | Original Equipment | ||||
| 1 | Composite Equipment: Is the equipment in this application a composite device subject to an additional equipment authorization? | No | ||||
| 1 | Related Equipment: Is the equipment in this application part of a system that operates with, or is marketed with, another device that requires an equipment authorization? | No | ||||
| 1 | Grant Comments | Power listed is peak conducted at the antenna connector. The antenna(s) of this Transponder equipment are mounted along the fuselage of air transport aircraft. These locations are accessible to airport maintenance personnel only and are in general not accessible to the general population. Users and installers must be provided with antenna installation instructions and transmitter operating conditions for satisfying RF exposure compliance. | ||||
| 1 | Is there an equipment authorization waiver associated with this application? | No | ||||
| 1 | If there is an equipment authorization waiver associated with this application, has the associated waiver been approved and all information uploaded? | No | ||||
| app s | Test Firm Name and Contact Information | |||||
| 1 | Firm Name |
CTC advanced GmbH (former CETECOM ICT Services )
|
||||
| 1 | Name |
G******** S******
|
||||
| 1 | Telephone Number |
49-68********
|
||||
| 1 | Fax Number |
49-68********
|
||||
| 1 |
t******@ctcadvanced.com
|
|||||
| Equipment Specifications | |||||||||||||||||||||||||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Line | Rule Parts | Grant Notes | Lower Frequency | Upper Frequency | Power Output | Tolerance | Emission Designator | Microprocessor Number | |||||||||||||||||||||||||||||||||
| 1 | 1 | 87 | 1090.00000000 | 1090.00000000 | 755.0000000 | 195.0000000000 ppm | 9M39M1D | ||||||||||||||||||||||||||||||||||
some individual PII (Personally Identifiable Information) available on the public forms may be redacted, original source may include additional details
This product uses the FCC Data API but is not endorsed or certified by the FCC