User Guide for uAvionix models including: uAvionix, ping200XTM TSO, UAV-1002373-001
Index of /downloads/ping200X
UAV-1002373-001 5 DRAFT – TSO PENDING 3 Limited Warranty uAvionix certified products are warranted to be free from defects in material and workmanship for two years from the installation of ping200X in or on
ping200XTM TSO User and Installation Guide UAV-1002373-001 DRAFT TSO PENDING © 2020 uAvionix Corporation. All rights reserved. Except as expressly provided herein, no part of this guide may be reproduced, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of uAvionix. uAvionix grants permissions to download a single copy of this guide onto an electronic storage medium to be viewed for personal use, provided that the complete text of this copyright notice is retained. Unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. uAvionix® and Ping® are registered trademarks of uAvionix Corporation and may not be used without express permission of uAvionix. ping200X, tailBeaconX, skyBeaconX, tailBeacon, skyBeacon, and skyBeacon Installer are trademarks of uAvionix Corporation and may not be used without express permission of uAvionix. ForeFlight is a registered trademark of ForeFlight LLC and is used with permission. Patent uavionix.com/patents UAV-1002373-001 2 DRAFT TSO PENDING 1 Revision History Revision Date Comments A 10/22/2020 Initial release UAV-1002373-001 3 DRAFT TSO PENDING 2 Warnings / Disclaimers All device operational procedures must be learned on the ground. uAvionix is not liable for damages arising from the use or misuse of this product. This equipment is classified by the United States Department of Commerce's Bureau of Industry and Security (BIS) as Export Control Classification Number (ECCN) 7A994. These items are controlled by the U.S. Government and authorized for export only to the country of ultimate destination for use by the ultimate consignee or end-user(s) herein identified. They may not be resold, transferred, or otherwise disposed of, to any other country or to any person other than the authorized ultimate consignee or end-user(s), either in their original form or after being incorporated into other items, without first obtaining approval from the U.S. government or as otherwise authorized by U.S. law and regulations. UAV-1002373-001 4 DRAFT TSO PENDING 3 Limited Warranty uAvionix certified products are warranted to be free from defects in material and workmanship for two years from the installation of ping200X in or on the aircraft. For the duration of the warranty period, uAvionix, at its sole discretion, will repair or replace any product which fails in normal use. Such repairs or replacement will be made at no charge to the customer for parts or labor, provided that the customer shall be responsible for any transportation cost. Restrictions: This warranty does not apply to cosmetic damage, consumable parts, damage caused by accident, abuse, misuse, fire or flood, theft, damage caused by unauthorized servicing, or product that has been modified or altered. Disclaimer of Warranty: IN NO EVENT, SHALL UAVIONIX BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE OR INABILITY TO USE THE PRODUCT OR FROM DEFECTS IN THE PRODUCT. SOME STATES DO NOT ALLOW THE EXCLUSION OF INCIDENTAL OR CONSEQUENTIAL DAMAGES, SO THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU. Warranty Service: Warranty repair service shall be provided directly by uAvionix. Proof of purchase for the product from uAvionix or authorized reseller is required to obtain and better expedite warranty service. Please email or call uAvionix support with a description of the problem you are experiencing. Also, please provide the model, serial number, shipping address and a daytime contact number. You will be promptly contacted with further troubleshooting steps or return instructions. It is recommended to use a shipping method with tracking and insurance. UAV-1002373-001 5 DRAFT TSO PENDING 4 Table of Contents 1 Revision History...................................................................................3 2 Warnings / Disclaimers ........................................................................ 4 3 Limited Warranty..................................................................................5 4 Table of Contents ................................................................................ 6 5 System Information .............................................................................. 9 5.1 Certification...................................................................................9 5.2 TSO Authorization.......................................................................10 5.3 Applicable P/Ns .......................................................................... 10 5.4 System Functions ....................................................................... 10 5.5 TSO Deviations and Incomplete..................................................11 5.6 FCC ID........................................................................................12 5.7 Device Marking ........................................................................... 13 5.7.1 ping200X Hardware...............................................................13 5.7.2 ping200X Software ................................................................ 13 5.8 Environmental Qualification Form ............................................... 14 5.9 Continued Airworthiness ............................................................. 15 5.10 System Limitations ...................................................................... 15 6 System Specifications........................................................................16 6.1 System Functionality ................................................................... 16 6.2 ping200X TSO Specifications ..................................................... 16 6.2.1 General Specifications........................................................... 16 6.2.2 Mode S Transponder Specifications ...................................... 17 6.2.3 Altitude Encoder Specifications ............................................. 17 6.2.4 Control Interface Specifications ............................................. 18 6.2.5 Position Interface Specifications ............................................ 18 6.2.6 System Interfaces..................................................................18 UAV-1002373-001 6 DRAFT TSO PENDING 7 Installation ......................................................................................... 19 7.1 Unpacking and Inspecting...........................................................19 7.2 Authorized Part Numbers............................................................19 7.3 Installation Materials and Tools...................................................19 7.4 Additional Required Equipment...................................................20 7.5 Mounting ..................................................................................... 20 7.6 Wiring ......................................................................................... 21 7.7 Transponder Antenna ................................................................. 22 7.8 Static Pressure Port .................................................................... 23 7.9 Cooling Requirements ................................................................ 23 8 Control and Configuration Interface ................................................... 24 9 Position Interface ............................................................................... 24 10 Configuration and Calibration ............................................................ 24 10.1 Configuration .............................................................................. 26 10.1.1 ICAO Address ....................................................................... 26 10.1.2 Aircraft Maximum Speed ....................................................... 27 10.1.3 Aircraft Stall Speed................................................................27 10.1.4 Aircraft Length / Width ........................................................... 27 10.1.5 Aircraft Registration ............................................................... 27 10.1.6 GPS Antenna Lateral / Longitudinal Offset ............................ 28 10.1.7 Aircraft Emitter Type..............................................................28 10.1.8 ADS-B In Capability...............................................................28 10.1.9 Baro Altitude Source ............................................................. 29 10.1.10 Serial Port Baud Rate............................................................29 10.1.11 SIL / SDA .............................................................................. 29 10.1.12 Default Control Mode ............................................................ 29 10.1.13 Default Squawk ..................................................................... 30 10.1.14 Baro Altitude Resolution ........................................................ 30 10.1.15 In / Out Protocols...................................................................30 UAV-1002373-001 7 DRAFT TSO PENDING 10.2 Control ........................................................................................ 30 10.3 Post-Installation Checks.............................................................. 31 10.4 Software Part Number ................................................................ 33 10.5 Altitude Encoder Calibration........................................................34 11 Normal Operation .............................................................................. 35 12 Maintenance ...................................................................................... 35 13 Support .............................................................................................. 35 Appendix A Control Interface ................................................................. 36 Appendix B Position Interface ................................................................ 40 Appendix C Example Installations..........................................................41 UAV-1002373-001 8 DRAFT TSO PENDING 5 System Information 5.1 Certification This installation manual provides mechanical and electrical information necessary to install ping200X. It is not equivalent to an approved airframespecific maintenance manual, installation design drawing, or installation data package. The content of this manual assumes use by competent and qualified personnel using standard maintenance procedures in accordance with Title 14 of the Code of Federal Regulation and other related accepted procedures. The conditions and tests required for approval of this article are minimum performance standards. Those installing this article either on or within a specific type or class of aircraft must determine that the aircraft installation conditions are within the standards which include any accepted integrated functions not specified by the standards. TSO articles, articles approved with 14 CFR Part 21.8(d), and any accepted integrated function(s) not specified in the standard must have separate approval for installation in an aircraft. The article may be installed only according to 14 CFR Part 43 or the applicable airworthiness requirements. This is an incomplete system intended to provide the functions identified in, and when installed according to, this installation manual. UAV-1002373-001 9 DRAFT TSO PENDING 5.2 TSO Authorization ping200X complies with the following TSOs when properly installed and interfaced with equipment as detailed in this guide. Function TSO / MPS Class / Type Air Traffic Control Radar Beacon System/Mode Select (ATCRBS / Mode S) Airborne Equipment TSO-C112e RTCA/DO-181E Level 2els, Class 1 [1] Extended Squitter Automatic Dependent Surveillance Broadcast (ADS-B) and Traffic Information Service Broadcast (TIS-B) Equipment Operating on TSO-C166b RTCA/DO-260B Class B1S the Radio Frequency of 1090 MHz Automatic Pressure Altitude Reporting Code-Generating Equipment TSO-C88b SAE/AS8003 N/A [1] Anticipating RTCA/DO-181F Level 2 Transponder requirements, ping200X does not support the UM protocol, does not support the Comm-A protocol, and does not have the capability to process and transmit air-initiated Comm-B messages. 5.3 Applicable P/Ns Description PF007 Boot Program Software ping200X (PF007 Operating Program) Software ping200X FPGA P/Ns UAV-1001758-( ) UAV-1002393-( ) UAV-1002392-( ) 5.4 System Functions System Function Mode S Transponder 1090ES Transmitter Altitude Encoder DO-178C DAL DO-254 DAL C C C C C C UAV-1002373-001 10 DRAFT TSO PENDING 5.5 TSO Deviations and Incomplete TSO C112e C112e Deviation uAvionix was granted a deviation from TSO-C112e Paragraphs 3.e and 6.f to use RTCA/DO-178C in place of RTCA/DO-178B. uAvionix was granted a deviation to not implement Utility Message (UM Field) support, consistent with anticipated RTCA/DO-181F and FAA/TSO-C112f Level 2 transponder requirements. C112e This impacts the Mode S Level 2 transponder SARPs requirements as contained in ICAO Annex 10 Volume IV §§3.1.2.6.5.3.1, 3.1.2.6.11.3.2.1.3, 3.1.2.6.11.3.4.2.2, and 3.1.2.7.9.2.3. uAvionix was granted a deviation to not implement Comm-A support, consistent with anticipated RTCA/DO-181F and FAA/TSO-C112f Level 2 transponder requirements. C112e This impacts the Mode S Level 2 transponder SARPs requirements as contained in ICAO Annex 10 Volume IV §§2.1.5.1.2, 3.1.2.6.11.1.2, and 3.1.2.10.5.2.1.1. uAvionix was granted a deviation to not implement broadcast interrogation support, consistent with anticipated RTCA/DO181F and FAA/TSO-C112f Level 2 transponder requirements. C112e This impacts the Mode S Level 2 transponder SARPs requirements as contained in ICAO Annex 10 Volume IV §§2.1.5.1.2, 3.1.2.6.11.1.2, and 3.1.2.10.5.2.1.1. uAvionix was granted a deviation to not implement multi-site message support, as it applies to the Comm-B operation of Level 2 transponders, consistent with anticipated RTCA/DO181F and FAA/TSO-C112f Level 2 transponder requirements. This impacts the Mode S Level 2 transponder SARPs requirements as contained in ICAO Annex 10 Volume IV §§2.1.5.1.2 and 3.1.2.6.11.3. UAV-1002373-001 11 DRAFT TSO PENDING C112e uAvionix was granted a deviation to not implement Air-Initiated Comm-B support, consistent with anticipated RTCA/DO-181F Level 2 and FAA/TSO-C112f transponder requirements. Airinitiated Comm-B messages are neither processed nor transmitted. C112e C166b C166b C88b C88b This impacts the Mode S Level 2 transponder SARPs requirements as contained in ICAO Annex 10 Volume IV §§2.1.5.1.2 and 3.1.2.6.11.3. uAvionix was granted a deviation to not reply to ATCBRS/Mode S All-Calls, as required by ICAO Annex 10 Volume IV §3.1.2.1.5.1.1.1 on or after January 1, 2020, and consistent with anticipated RTCA/DO-181F and FAA/TSOC112f requirements. uAvionix was granted a deviation from TSO-C166b Paragraphs 3.e and 6.h to use RTCA/DO-178C in place of RTCA/DO-178B. uAvionix was granted a deviation to not implement Airborne Velocity Subtypes 3 and 4, consistent with anticipated RTCA/DO-260C and FAA/TSO-C166c requirements. uAvionix was granted a deviation from TSO-C88b Paragraphs 3.e and 6.h to use RTCA/DO-178C in place of RTCA/DO178B. uAvionix was granted a deviation from TSO-C88b Paragraph 3.d to use RTCA/DO-160G in place of RTCA/DO-160E. 5.6 FCC ID Model ping200X TSO FCC ID 2AFFTP200S UAV-1002373-001 12 DRAFT TSO PENDING 5.7 Device Marking 5.7.1 ping200X Hardware 5.7.2 ping200X Software The software contained in ping200X is identified by electronic marking. Reference Section 10.4 for information on determining the software part number. UAV-1002373-001 13 DRAFT TSO PENDING 5.8 Environmental Qualification Form Conditions DO-160G Section Description of Conducted Tests Temperature and Altitude 4.0 Equipment tested to Categories B2,C4 Low temperature ground survival 4.5.1 -55°C Low Temperature Short-Time 4.5.1 -35°C Operating Low Temperature Operating 4.5.2 -35°C (see Note 1) High Temperature Operating 4.5.4 +70°C High Temperature Short-Time 4.5.3 +70°C Operating High Temperature Ground Survival 4.5.3 +85°C Loss of Cooling 4.5.5 Cooling air not required (+70°C operating without cooling) Altitude 4.6.1 35,000 ft (see Note 2) Decompression 4.6.2 Equipment identified as Categories B2,C4 no test Overpressure 4.6.3 Equipment identified as Categories B2,C4 no test Temperature Variation 5.0 Equipment tested to Category B Humidity 6.0 Equipment tested to Category A Operation Shocks 7.0 Equipment tested to Category B Crash Safety 7.0 Equipment tested to Category B Type 5 Vibration 8.0 Aircraft zone 2: type 5 Category S level M Explosion 9.0 Equipment identified as Category X no test Waterproofness 10.0 Equipment identified as Category X no test Fluids Susceptibility 11.0 Equipment identified as Category X no test Sand and Dust 12.0 Equipment identified as Category X no test Fungus 13.0 Equipment identified as Category X no test Salt Spray 14.0 Equipment identified as Category X no test Magnetic Field 15.0 Equipment tested to Category Y Power Input 16.0 Equipment tested to Category BX Voltage Spike 17.0 Equipment tested to Category B AF Conducted Susceptibility 18.0 Equipment tested to Category B Induced Signal Susceptibility 19.0 Equipment tested to Category AC RF Susceptibility 20.0 Equipment tested to Category TT RF Emissions 21.0 Equipment tested to Category B Lightning Induced Transient 22.0 Equipment tested to Category A2XXXX Susceptibility Lightning Direct Effects 23.0 Equipment identified as Category X no test Icing 24.0 Equipment identified as Category X no test Electrostatic Discharge 25.0 Equipment tested to Category A Fire, Flammability 26.0 Equipment identified as Category X no test Notes: 1. Tested to operating low of -45°C when used with an external barometer 2. Tested to 50,000 ft UAV-1002373-001 14 DRAFT TSO PENDING 5.9 Continued Airworthiness Maintenance of the ping200X is "on condition" only. Periodic regulatory function checks of the transponder and altitude encoder must be performed. The aircraft must be returned to service in a means acceptable to the appropriate aviation authority. If the altitude encoder reports correspondence errors in excess of ±125 feet, when compared to the primary flight altimeter, then calibration as described in Section 10.5 must be performed. If the error cannot be corrected using the calibration procedure, the unit must be repaired or replaced. Note: Transponders certified after January 1, 2020 must not respond to ATCRBS/Mode S All-Calls (Long P4 interrogation). This may produce unexpected results in transponder test sets. Note: Mode S transponders must only respond to Mode S Only All- Calls when airborne. ping200X can be placed in an airborne state for test purposes by entering "Ground Test Mode" using the "ping200X Control & Config" Windows application, or by using certain compatible control heads. For more details see Section 10.3. 5.10 System Limitations Installation This article meets the minimum performance and quality control standards required by a technical standard order (TSO). If you are installing this article on or in a specific type or class of aircraft, you must obtain separate approval for installation. UAV-1002373-001 15 DRAFT TSO PENDING 6 System Specifications 6.1 System Functionality ping200X is a Mode S, Level 2els, Class 1 transponder with ADS-B extended squitter, elementary surveillance and SI code support. The ping200X has a nominal power output of 250W and meets the power output requirements for Class 1. The ADS-B function meets DO-260B Class B1S. This transponder replies to both legacy Mode A/C interrogations and to Mode S interrogations from both ground radar and airborne collision avoidance systems. In all cases, the interrogations are received by the transponder on 1030MHz and replies are transmitted on 1090MHz. 6.2 ping200X TSO Specifications 6.2.1 General Specifications Characteristics Specifications Width 46.99 mm Height 9.50 mm Depth 63.85 mm Weight 45 g Operating temperature range -35°C to +70°C (internal barometer) -45°C to +70°C (external barometer) Maximum pressure altitude 35,000 ft (internal barometer) 50,000 ft (external barometer) Input voltage range 9 to 30.3 VDC 14V current 0.16A idle 0.25A maximum 28V current 0.13A idle 0.20A maximum Inrush Current Limit [1] 1A Export Compliance ECCN 7A994 [1] Inrush and internal short-circuit protection is internally current limited to 1A UAV-1002373-001 16 DRAFT TSO PENDING 6.2.2 Mode S Transponder Specifications Characteristics Specifications Transmit frequency 1090 MHz Transmit power 54 dBm (250 W) Receive frequency 1030 MHz ATCRBS sensitivity -74 dBm Mode S sensitivity -74 dBm RF Impedance 50 RF Connector SMA 6.2.3 Altitude Encoder Specifications Characteristics Specifications Operating Range -1,000 ft to 35,000 ft (TSO compliant) 35,001 ft to 50,000 ft (extended range, ±1% typical) Maximum Differential 36,000 ft Pressure Maximum Rate of Altitude 20,000 fpm Change Static Pressure Port M3 barb fitting UAV-1002373-001 17 DRAFT TSO PENDING 6.2.4 Control Interface Specifications Characteristics Specifications Physical RS-232 Rate and properties 57,600 bps 8N1 Protocols UCP, UCP-HD and Apollo For more control interface details, see Appendix A . 6.2.5 Position Interface Specifications Characteristics Specifications Physical RS-232 Rate and properties 115,200 bps 8N1 Protocols MAVLink For more position interface details, see Appendix B . 6.2.6 System Interfaces Control Head or Autopilot Position Source TXD RXD GND GND PWR TXD Aircraft Power Avionics Breaker Aircraft Ground Position WH RXD RD PWR BK GND Control BK GND GY TXD OR RXD RD PWR ping200X Static Pressure Transponder Antenna UAV-1002373-001 18 DRAFT TSO PENDING 7 Installation 7.1 Unpacking and Inspecting Carefully unpack the device and make a visual inspection of the unit for evidence of any damage incurred during shipment. If the unit is damaged, notify the shipping company to file a claim for the damage. To justify your claim, save the original shipping container and all packing materials. 7.2 Authorized Part Numbers Item ping200X Hardware ping200X Software P/N UAV-1002723-( ) UAV-1002393-( ) 7.3 Installation Materials and Tools ping200X requires configuration, either using the available uAvionix Windows-based application, or dynamically using the described configuration protocol. Typical installations will be configured using: · "ping200X Control & Config" Windows application, UAV-1004567-( ) · ping200X USB configuration adapter, UAV-1004050-001 ping200X may require standard aviation parts for installation, such as: · Screws or appropriate hardware · Wire · Shielded wire (2 or 3 conductor) · Circuit breakers · Environmental splices · Ring terminals for grounding · Static pressure lines and fittings · Thread locking compound. We recommend Loctite® 242 or 243 which works well with stainless steel hardware. Minimally, ping200X installation requires access to the following tools: · Screwdriver or other appropriate driver · Appropriate crimping tool(s) or soldering equipment UAV-1002373-001 19 DRAFT TSO PENDING 7.4 Additional Required Equipment ping200X is a "remote" transponder. To fully function it requires connection to a controlling device, often referred to as a control head. It is possible to statically configure ping200X, but certain capabilities, such as changing the squawk code and responding to annunciations, will not be available when no controlling device is connected. For transmission of complete ADS-B data elements, ping200X also requires connection to a position source. The following table details the functions provided directly by ping200X. Transponder X ADS-B Transmitter X Altitude Encoder X GPS Receiver Transponder Control Head w/ Antenna Annunciation In typical configurations, the control head provides control, display, and annunciation. 7.5 Mounting The ping200X is designed to be mounted in any convenient location in the cockpit, the cabin, or an avionics bay. The following installation procedure should be followed, taking care to allow adequate space for installation of cables and connectors. · Select a position in the aircraft that is not too close to any high external heat source. The ping200X is not a significant heat source itself and does not need to be kept away from other devices for this reason. · Avoid sharp bends and placing the cables too near to the aircraft control cables. Secure the transponder to the aircraft via the two integrated mounting brackets. The brackets are designed to accept screws up to size M3 or 440. Thread locking compound should be used as appropriate, and the ping200X should be mounted on a flat surface. Note: Installation of the ping200X must be in accordance with AC 43.13-2B, Chapter 1. UAV-1002373-001 20 DRAFT TSO PENDING 7.6 Wiring ping200X requires connections to power, ground, an RS-232 control interface and an RS-232 position interface. Color Red Black Grey Orange Type Power Input Power Input Data Output Data Input 4-wire Control Interface Function Aircraft Power Aircraft Ground Control RS-232 Transmit Control RS-232 Receive Color Red Black White Type Power Output Power Output Data Input 3-wire Position Interface Function Position Power (directly tied to 4-wire power input without additional protection, can be used to power position source) Position Ground (directly tied to 4-wire power input without additional protection, can be used to power position source) Position RS-232 Receive If new power wiring is required, refer to AC 43.13-1B Chapter 11 for guidance. The wiring should present an impedance of less than 0.5 . The following table provides guidance for typical aircraft hook-up wire. Gauge ohm/km 20 AWG 35 22 AWG 64 Maximum Length for 0.5 14.2 m 7.8 m Refer to Appendix C for example wiring diagrams and installations. UAV-1002373-001 21 DRAFT TSO PENDING 7.7 Transponder Antenna An appropriate L-band antenna, designed to receive and transmit vertically polarized signals at 1030 and 1090 MHz, must be installed. The following antennas may be used: · Standard 50 vertically polarized antenna with VSWR 1.5:1 over the 1030 to 1090 MHz frequency band · TSO-C74( ) or TSO-C112( ) antennas that meet the above specification · uAvionix SMA dipole, P/N UAV-1000653-008 Take into consideration the antenna manufacturer's installation instructions. General guidance is provided below. · The antenna should be mounted in a vertical orientation when the aircraft is in level flight. For uAvionix UAV-1000653-008, see below for proper orientation. UAV-1002373-001 22 DRAFT TSO PENDING · Keep the cable lengths as short as possible and avoid sharp bends in the cable to minimize the Voltage Standing Wave Ratio (VSWR) (i.e. Return Loss). · Ensure that cable and connector losses do not reduce power output below allowed levels for your aircraft operation. · Conventional monopole antennas require an appropriate ground plane. For metallic aircraft, ensure good ground connection to the antenna. For composite aircraft, a ground plane must be installed. · The antenna connections should be protected from the elements, and antenna cabling should be installed to minimize RF energy radiated inside the aircraft. 7.8 Static Pressure Port ping200X contains a TSO-C88b altitude encoder. The barb fitting (size M3) located on the unit's enclosure should be securely attached to the aircraft's static pressure system, when available. Minimize static pressure line lengths as possible. Press-plastic tubing (PVC, soft nylon or polyurethane) with a nominal ID of 1/8" (3.18mm) can be used, and secured with a small tie wrap. Adapters may be used to convert the barb to match the aircraft's current static plumbing. Ensure any fittings are free from leaks. Upon completion of installation, a case leak test should be performed per 14 CFR 43 Appendix E. If an external altitude source is configured, the static pressure system does not need to be connected to the ping200X static pressure port. The Maximum Operating Altitude listed on the ping200X nameplate is not applicable when used with an external altitude encoding source. 7.9 Cooling Requirements ping200X is designed to meet all applicable TSO requirements without forced-air cooling. Attention should, however, be given to the incorporation of cooling provisions to limit the maximum operating temperature if ping200X is installed in close proximity to other avionics. The reliability of equipment operating in close proximity in an avionics bay can be degraded if adequate cooling is not provided. UAV-1002373-001 23 DRAFT TSO PENDING 8 Control and Configuration Interface ping200X has a control and configuration serial interface. It can be used to configure the equipment at installation time, and optionally to control the device while operating. Typically, a control head or unmanned aircraft autopilot is connected to the device during operation. Transponder control provides the ping200X with data such as operating mode, squawk code, and optionally external pressure altitude information. Status and annunciation information is provided by ping200X over the control interface. For details on the ping200X control interface, refer to Appendix A . 9 Position Interface For complete ADS-B transmissions, a serial connection to a position source is required. ping200X receives compliant position information from a GPS or similar position source. Only one position source can be configured to the ping200X at a time. If multiple position sources are detected, ping200X will indicate a "Maintenance Required" failure. If no position data is provided, certain ADS-B messages will be incomplete. Care must be taken to ensure the position source is qualified to meet ADSB regulations for your operation, and that the ping200X is appropriately configured (SIL/SDA value). Amongst other considerations, position source and system latency must be considered. The following position source has been qualified for use: · uAvionix truFYX, P/N UAV-1002809-001 (SIL=3 / SDA=2) For details on the ping200X position interface, refer to Appendix B . 10 Configuration and Calibration The transponder system should be configured during initial system installation. Connect the ping200X to a PC running the Configuration and Control application via the USB COM port adapter. UAV-1002373-001 24 DRAFT TSO PENDING PC USB Adapter Control RXD TXD POWER (9-30.3 V) GY TXD OR RXD RD PWR BK GND GND ping200X Set `Conn Type' to `Serial', `Port' to the USB or serial port connected to the ping200X, `App Baud' to `57600' and `Protocol' to `UCP'. Verify the COM Settings Click `Start'. UAV-1002373-001 25 DRAFT TSO PENDING 10.1 Configuration The configuration items list below should be used to document the system installation for future reference. These items can be found on the `Configuration' tab and are permanently stored in the ping200X. Configuration Item ICAO Address Aircraft Maximum Speed (kts) Aircraft Stall Speed Aircraft Length (m) Aircraft Width (m) Aircraft Registration GPS Antenna Lateral Offset (m) GPS Antenna Longitudinal Offset (m) Aircraft Emitter Type ADS-B In Capability UAT RX 1090ES RX Baro Altitude Source Serial Port Baud Rate (bps) SIL SDA Default Control Mode Default Squawk Baro Altitude Resolution (ft) In Protocols Out Protocols Default 0x000000 < 75 0 L 15 W 23 " " 0 Applied by sensor Unmanned aerial vehicle NO NO Internal 57600 <= 1E-7 (3) <= 1E-5 (2) None (Off) 1200 25 UCP UCP Configured 10.1.1 ICAO Address The ICAO address is a 24-bit number issued to the aircraft by the registration authority of the aircraft. These addresses are usually written as a 6-digit hexadecimal number, although you may also encounter one written as an 8-digit octal number. The ping200X understands the hexadecimal format. An octal number must be converted to hexadecimal format before entering. UAV-1002373-001 26 DRAFT TSO PENDING Tip: By using the N-Number Look Up function on https://www.faa.gov, locate and use the "Mode S Code (base 16 / hex)" value. Applies to U.S. registered aircraft only. 10.1.2 Aircraft Maximum Speed Mode S transponders can transmit their maximum airspeed characteristics to aircraft equipped with TCAS. This information is used to identify threats and to plan avoidance action by the TCAS equipped aircraft. The airspeeds are grouped in ranges. 10.1.3 Aircraft Stall Speed The default aircraft stall speed is 0. Set as appropriate for your aircraft to allow automatic air/ground state determination. Set to 0 to lock in airborne state, or to allow switching by the control head. See Appendix A for more details. 10.1.4 Aircraft Length / Width When on the ground, ADS-B transmits encoded aircraft size information which is used by ATC to identify taxiing routes and potential conflicts. Enter the length and width (wingspan) fields and the appropriate size codes will be calculated for transmission. Aircraft Length in Meters L 15 15 < L 25 25 < L 35 35 < L 45 45 < L 55 55 < L 65 65 < L 75 75 < L 85 L > 85 Aircraft Width in Meters W 23 28.5 < W 34 33 < W 38 39.5 < W 45 45 < W 52 59.5 < W 67 72.5 < W 80 W > 80 Any 10.1.5 Aircraft Registration The Aircraft Registration can be up to an 8 alpha-numeric code that corresponds to the tail number of the aircraft. (0-9, A-F). This value is used by default in the ADS-B "Callsign" field, unless a valid "Flight ID" is provided via the control interface. UAV-1002373-001 27 DRAFT TSO PENDING Note: This is typically your aircraft N-number, unless otherwise advised by the FAA or ATC. 10.1.6 GPS Antenna Lateral / Longitudinal Offset The GPS antenna offset is used in conjunction with the length and width to manage taxiway conflicts. A typical GPS does not report the geographic position of the center of the aircraft, or even the tip of the nose of the aircraft; instead, it usually reports the location of the actual GPS antenna (not the GPS receiver). In normal flight operation, this distinction is of no importance at all, but if ADS-B is used to manage taxiway conflicts, a significant offset in antenna position could mean the aircraft footprint is not in the same place as the ADS-B reported position. Although the GPS Antenna Offset is primarily intended for position correction on large transport aircraft, General Aviation aircraft can also have a significant offset. For example, if the aircraft has a long tail boom and the GPS antenna is on top of the tail, the GPS position could be 4 meters or more from the nose of the aircraft. GPS Antenna Lateral Offset from roll axis (meters) 0 Left 2 Left 4 Left 6 Right 2 Right 4 Right 6 GPS Antenna Longitudinal Offset from aircraft nose (meters) 0 to 60 meters in 2-meter increments 10.1.7 Aircraft Emitter Type The aircraft emitter type default is `Unmanned aerial vehicle'. 10.1.8 ADS-B In Capability The ADS-B transmissions include an indication to the ground stations of whether the aircraft includes a 1090MHz ADS-B receiver, a UAT ADS-B receiver, or both. This data is used to transmit ADS-R or TIS-B broadcasts to your aircraft if conditions indicate. ping200X does not include an ADS-B receiver. Only select these items if you have a separate ADS-B receiver on-board. UAV-1002373-001 28 DRAFT TSO PENDING 10.1.9 Baro Altitude Source By default, ping200X utilizes pressure altitude measurements from an internal TSO-C88b altitude encoder for Mode C, S and ADS-B messages. If desired, an existing or external altitude encoder can be used in lieu of the internal altitude encoder. To do so, change the ping200X's "Baro Altitude Source" from "Internal" to "External". If set to "External", the ping200X will use the barometric pressure altitude reported in the Control Message in all Mode C, S and ADS-B messages. 10.1.10 Serial Port Baud Rate This setting configures the speed of the control interface serial baud rate in bps. 10.1.11 SIL / SDA Set SIL according to the advertised integrity level of the GPS source. Per AC 20-165B, ping200X's System Design Assurance (SDA) must report the lowest SDA value of the ADS-B system. The ADS-B system includes both the SDA of the ping200X and the paired GPS position source. If the paired GPS SDA is less than 2, configure the ping200X SDA value to the SDA of the GPS. For GPS's SDAs greater than or equal to 2, configure the ping200X SDA to 2. 10.1.12 Default Control Mode Select the default operating mode, to be used prior to arrival of control messages. This setting configures the ping200X for Mode A, Mode C, Mode S and ADS-B Extended Squitter transmissions. · None selected disables all modes · Mode A - Squawk · Mode C Altitude · Mode S Addressed Identification and Altitude · Mode ES ADS-B Identification and Position reporting ! When not used with a control head or equivalent device, modes A / C / S / ES must be enabled by default to meet all authorized TSOs. UAV-1002373-001 29 DRAFT TSO PENDING 10.1.13 Default Squawk The default squawk is 1200. To assist ATC tracking of aircraft, an aircraft squawk is transmitted. The configured value is the squawk code that will be transmitted in lieu of available control data. 10.1.14 Baro Altitude Resolution The barometric pressure altitude source resolution default is 25 (ft). 10.1.15 In / Out Protocols The default In / Out protocols are UCP. 10.2 Control The `Control' tab allows the installer to exercise and verify the transponder's operation. This simulates a control head or similar equipment. Ownship Display Serial Port Setup Control Packet Statistics Fault Status GPS Simulator Serial Activity Viewer Transponder Status UAV-1002373-001 30 DRAFT TSO PENDING 10.3 Post-Installation Checks Post-installation checks must be performed by the installer, after configuration, as appropriate for the aircraft and type of installation. To ensure compliance with regulations in the United States, verify functionality identified in 14 CFR Part 43 Appendix F (ATC Transponder Tests and Inspections) and 14 CFR Part 43 Appendix E (Altimeter System Test and Inspection). Aircraft with ping200X installed may be subject to requirements in 14 CFR §§ 91.215, 91.225 and 91.227. Additional compliance with AC 20-165B may be required. A complete post-installation check may be performed by using a ramp tester such as a VIAVI IFR6000. A simplified post-installation check procedure follows. STEP Launch the `ping200X Control & Config' Windows application Set Port to the USB or serial port connected to the ping200X Set the `App Baud' to `57600' Set `Protocol' to `UCP' - If the ping200X has been reconfigured for a protocol other than UCP, this procedure may not apply Connect the antenna Apply power from a minimum of a 11V, 1A power source Press `Start' in `ping200X Control & Config' Windows application Confirm activity in `Serial Activity Viewer' and incrementing `Pkts' in `Packet Statistics' of `Control' tab Verify `ICAO Address' in `Ownship Display' is correct for your aircraft, and not `000000' Confirm `Baro Altitude' in `Ownship Display' shows the current pressure altitude; i.e. the current altitude as displayed on an altimeter set to 29.92 If a GPS is connected and the GPS antenna has a clear view of the sky, allow the GPS time to obtain a position fix; confirm that `Latitude' and `Longitude' are correct in `Ownship Display' UAV-1002373-001 DRAFT TSO PENDING CHECK 31 STEP Select `ALT' from the `Mode' selection box in `Control' Verify `TX System' fault annunciation LED turns green in `Fault Status' If you are in range of Radar or connected to an interrogating test set, `Transponder Status' will indicate interrogations If not already in airborne state, access the `Service' tab and select `Enable Ground Test Mode' - This will enable airborne state until the ping200X is power cycled Return to `Control' tab and verify `Air/Ground State' displays `Airborne' in `Ownship Display' Perform ramp test procedures as necessary for required aircraft operations An EFB application such as ForeFlight Mobile, when connected to an ADS-B receiver such as Sentry, can be used to verify ADS-B transmissions; - Using ForeFlight Mobile, in the ADS-B Device screen, select `Ownship' when detected, and verify transmitted parameters CHECK UAV-1002373-001 32 DRAFT TSO PENDING 10.4 Software Part Number Launch the `ping200X Control & Config' Windows application. Confirm the displayed `P/N' and `Version' on the `Firmware Version' section of the `Service' tab is current per Service Bulletins listed at: https://uavionix.com/support/ping200X/ If not current, apply Service Bulletins as appropriate to update the software. UAV-1002373-001 33 DRAFT TSO PENDING 10.5 Altitude Encoder Calibration STEP Launch the `ping200X Control & Config' Windows application CHECK Set Port to the USB or serial port connected to the ping200X Set the `App Baud' to value noted in Section 10.1 Set `Protocol' to value noted in Section 10.1 Apply power from a minimum of a 11V, 1A power source UAV-1002373-001 34 DRAFT TSO PENDING Press `Start' in `ping200X Control & Config' Windows application With a Pitot Static Test Set connected, select the `Service' tab Press `Get' to retrieve the calibration information Adjust Pitot Static Test Set to the Low calibration altitude Wait for Pitot Static Test Set to reach the Low calibration altitude, then click 'Start' Wait for calibration to complete Adjust Pitot Static Test Set to Mid calibration altitude Wait for Pitot Static Test Set to reach the Mid calibration altitude, then click 'Start' Wait for calibration to complete Adjust Pitot Static Test Set to the High calibration altitude Wait for Pitot Static Test Set to reach the High calibration altitude, then click 'Start' Wait for calibration to complete Click `Send' to send updated calibration to the device 11 Normal Operation ping200X must be enabled, typically in ALT mode, during all phases of flight including surface movement operations. 12 Maintenance The ping200X is not a user serviceable product. All service must be performed either by uAvionix or an authorized uAvionix repair center. 13 Support For additional questions or support please visit: https://www.uavionix.com/support/ UAV-1002373-001 35 DRAFT TSO PENDING Appendix A Control Interface ping200X is optionally controlled and configured using the data interface specified below. Characteristics Physical Data rate Parity Data bits Stop bits Protocol Specifications RS-232 57,600 bps (default) None 8 1 UCP (RX/TX enabled by default) UCP-HD (disabled by default) Apollo (disabled by default) UCP is enabled by default for use as the input protocol. Apollo input can optionally be enabled simultaneous with UCP, and messages are processed based on the received data format. UCP is enabled for use as the output protocol. Additionally, Apollo output is automatically enabled upon receipt of an Apollo input message. The data rate and protocols can be configured by the UCP/UCP-HD Transponder Configuration message. UCP or UCP-HD input is required to be enabled to allow device configuration. A.1 UCP uAvionix Control Protocol (UCP) is documented in uAvionix UCP Transponder Interface Control Document UAV-1002375-001. This document is made available to authorized parties, and may be obtained by contacting uAvionix. UCP can be used to configure, control, and monitor status of the ping200X. A.1.1 Control Message The Control message must be supplied to ping200X as documented in the UCP ICD. Minimally, Mode A (squawk) code, IDENT, emergency state, and transponder mode are provided in this message. UAV-1002373-001 36 DRAFT TSO PENDING Mode To set the transponder operating mode, appropriate enable bits must be set in the Control message. The mapping of traditional transponder modes to required Control message enablement bits follows. Operating Mode STBY ON (suppress altitude) ALT Mode A X X Mode C X Mode S X X 1090ES X X Flight Identification If Flight Identification is provided in the Control message, that value is transmitted as Flight ID. If none (all spaces) is provided, the Call Sign/Aircraft Registration value configured in the device is transmitted. Air-Ground State Optionally, air-ground state may be provided in the Control message. To use air-ground state from the control message, the device must be configured with a VS0 of zero. Air-ground logic is described by the following chart. VS0 == 0 yes Use control input no Auto A-G state algorithm ground determined ground set Ground airborne determined Airborne airborne set Airborne subsonic and supersonic state is automatically determined by ping200X. UAV-1002373-001 37 DRAFT TSO PENDING A.1.2 Heartbeat Message With UCP enabled, the Heartbeat message is sent once per second. The following specific fault indications are available in the Heartbeat message, and should be mapped to annunciations compliant with applicable regulations. TSO-C166b requires annunciations of ADS-B transmission device and function failures (see RTCA/DO-260B §2.2.11.5) Fault Maintenance Required Failure TX System Failure GNSS No 3D Fix Failure GNSS Unavailable Description ICAO address not set (RTCA/DO-181E §2.2.10.3) ICAO address not set (RTCA/DO-260B §2.2.11.3.1) Multiple position sources available check configuration (RTCA/DO-260B §2.2.5.3) Transponder replies not enabled or acquisition squitter rate failure (RTCA/DO-181E §2.2.10.4) Transmit not enabled or extended squitter rate failure (RTCA/DO-260B §2.2.11.2.1 and §2.2.11.5.1) No valid 3D position from GNSS (RTCA/DO-229E §2.1.2.6) Unable to communicate with GNSS subsystem (RTCA/DO260B §2.2.11.6) A.2 UCP-HD uAvionix Control Protocol Half Duplex (UCP-HD) is documented in uAvionix UCP Transponder Interface Control Document UAV-1002375001. This document is made available to authorized parties, and may be obtained by contacting uAvionix. UCP-HD can be used to configure, control, and monitor status of the ping200X. A.2.1 Control Message See A.1.1 for a description of the Control message. A.2.2 Transponder Status With UCP-HD enabled, the Transponder Status is sent in response to each Control message, as documented in the ICD. The presence of a fault to annunciate is delivered by the "Fault or Failure Indicated" bit being set. To determine the specific fault, query the Heartbeat message using a Message Request. See A.1.2 for a description of the fault indications available in the Heartbeat message. UAV-1002373-001 38 DRAFT TSO PENDING A.3 Apollo Apollo can be used to control and monitor status of the ping200X. To use, ensure Apollo is enabled as an input protocol. Once an Apollo message is received, Apollo message output is enabled until device reset. A.3.1 Supported Input Messages The following input messages are supported: Mode (#MD) The Mode message configures the operating mode, Mode A (squawk) code, and IDENT. Setting `O' `A' `C' Description STBY ON (Altitude Suppress) ALT Mode A X X Mode C X Mode S X X 1090ES X X Altitude (#AL) The altitude message provides pressure altitude information. UAV-1002373-001 39 DRAFT TSO PENDING Appendix B Position Interface Position data may be provided through the control interface using UCP or UCP-HD GNSS Data Messages, however typical configurations will use the dedicated position interface to supply position data. The position interface communicates using the MAVLink protocol format, and accepts custom uAvionix "Navigation Data Messages". This message is documented in the uAvionix OEM Protocol Specification UAV-1001912001. This document is made available to authorized parties, and may be obtained by contacting uAvionix. UAV-1002373-001 40 DRAFT TSO PENDING Appendix C Example Installations ping200X can be statically configured, or dynamically controlled by a control head or autopilot. To meet local regulations, dynamic control may be required (for configuration of squawk code, etc.). For complete ADS-B messages, a position source is necessary. The installation information below serves as a supplement to any manuals describing controlling devices, and concern basic wiring of the transponder control and position functionalities only. For further installation and operating instructions, please reference the appropriate installation manual and pilot's guide. The installer should become fully familiar with the installation process for the controlling device. Use of these devices may be limited to non-certified aircraft. These descriptions are informational, and in no way grant an installation approval. C.1 Standalone (control optional) with truFYX GPS This installation uses the truFYX GPS for position data. An optional control head or autopilot, configured for UCP (default) or UCP-HD protocol, may be connected to provide other dynamic or configuration data. truFYX GPS Optional Control Head or Autopilot truFYX BK GND RD PWR GY TXD OR RXD TXD RXD GND Aircraft Power Avionics Breaker Aircraft Ground Position WH RXD RD PWR BK GND Control BK GND GY TXD OR RXD RD PWR Configure the ping200X as appropriate. UAV-1002373-001 DRAFT TSO PENDING ping200X Static Pressure Transponder Antenna 41 C.2 AV-30-C or AV-30-E Control Head with truFYX GPS This installation uses the uAvionix truFYX GPS for position data. The uAvionix AV-30-C or AV-30-E provides control, status, and altitude encoder data. AV-30-C or AV-30-E MFD AV-30-( ) GND 9 RXD 4 TXD 5 PWR 1 truFYX BK GND RD PWR GY TXD OR RXD truFYX GPS MFD Breaker Aircraft Power Avionics Breaker Aircraft Ground Position WH RXD RD PWR BK GND Control BK GND GY TXD OR RXD RD PWR Static Pressure not required Transponder Antenna ping200X Configure the ping200X as appropriate, ensuring the following values have been updated from defaults: Parameter In Protocols Out Protocols Serial Port Baud Rate Baro Altitude Source Value UCP-HD UCP-HD 2400 External UAV-1002373-001 42 DRAFT TSO PENDING C.3 Third-party EFIS C.3.1 ping200X Configuration Configure the ping200X as appropriate, ensuring the following values have been updated from defaults: Parameter In Protocols Out Protocols Serial Port Baud Rate Baro Altitude Source Value UCP and Apollo Apollo 57600 or as appropriate External C.3.2 EFIS Configuration The following third-party EFIS displays have the capability to send barometric pressure altitude data and control the mode and squawk functions of the ping200X through any available RS-232 serial output. ping200X configuration must still take place through the "ping200X Control & Config" Windows application. GRT MGL Known Compatible EFIS MINI-B MINI-AP MINI-X Sport EX Horizon EX iEFIS Only the serial OUTPUT is required. It should be set to the following parameters. Characteristics Physical Rate and properties Protocol Specifications RS-232 57,600 bps 8N1 (or as configured on ping200X) SL70, STX 165R, or UCP UAV-1002373-001 43 DRAFT TSO PENDING C.3.3 Wiring Example pinout options for certain compatible EFIS displays are shown below. Please consult the EFIS installation manuals for more information. GRT Mini-X Serial Serial / Mini-AP 1 2 Orange (RXD) 5 1 GRT Mini-B Serial Serial Serial 1 2 3 Orange (RXD) 5 1 9 GRT Sport EX Serial Serial Serial Serial Serial Serial / Horizon EX 1 2 3 4 5 6 Orange (RXD) A2 A4 A25 A5 A3 A1 UAV-1002373-001 44 DRAFT TSO PENDINGMicrosoft Word 2016