GTS 8XX/GPA 65 Installation Manual (Includes the GA 58 Antenna) 190-00587-00 April, 2009 Revision 4TP
© Copyright 2009 Garmin Ltd. or its subsidiaries All Rights Reserved Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express prior written consent of Garmin.
This manual reflects the operation of software version X.XX. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions.
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TABLE OF CONTENTS PARAGRAPH PAGE 1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 GENERAL DESCRIPTION..............................................................................................................1-1 Introduction........................................................................................................................................1-1 Equipment Description ......................................................................................................................
LIST OF ILLUSTRATIONS FIGURE PAGE 2-1 GTS 800 Installation with Top and Bottom Directional Antennas....................................................2-7 2-2 GTS 800 Installation with Top and Bottom Monopole Antennas .....................................................2-8 2-3 GTS 800 Installation with Top Directional Antennas and no Bottom Antenna ................................2-8 2-4 GTS 820/GTS 850 Installation Top and Bottom Directional Antennas ............................................
LIST OF TABLES TABLE PAGE 2-1 2-2 2-3 2-4 3-1 3-2 3-3 3-4 GPA 65 Minimum Wiring Requirements ..........................................................................................2-6 Cable Types and QMA Connectors .................................................................................................2-11 Recommended Coaxial Length........................................................................................................2-12 Coaxial Cable Set Length Tolerance ...................
GTS 8XX HARDWARE MOD LEVEL HISTORY The following table identifies hardware modification (Mod) Levels for the GTS 8XX. Mod Levels are listed with the associated service bulletin number, service bulletin date, and the purpose of the modification. The table is current at the time of publication of this manual (see date on front cover) and is subject to change without notice.
1 1.1 GENERAL DESCRIPTION Introduction This manual presents mechanical and electrical installation requirements for installing the GTS 8XX/GPA 65 Traffic Advisory System (TAS) and Traffic Collision Avoidance System (TCAS I). 1.2 Equipment Description The GTS 8XX is a microprocessor-based Line Replaceable Unit (LRU) that uses active interrogations of Mode S (GTS 820 and GTS 850 only) and Mode C transponders to provide Traffic Advisories to the pilot.
1.4 Technical Specifications 1.4.1 Environmental Qualification Form It is the responsibility of the installing agency to obtain the latest revision of the GTS 8XX/GPA Environmental Qualification Form.
1.4.3 General Specifications The table below contains general specifications. For detailed environmental specifications, see the Environmental Qualification Form. Characteristics Specifications Operating Temperature Range -55°C to +70°C. Humidity 95% non-condensing Altitude Range -1,500 ft to 55,000 ft Software Compliance RTCA/DO-178B levels B, C, and D Hardware Compliance RTCA/DO-254 Level C Environmental Compliance RTCA/DO-160E 1.4.
1.5 Certification The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those installing this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for installation in an aircraft. The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements.
1.5.2 TSO/ETSO Deviations 1.5.2.1 GTS 800 TSO/ETSO TSO-C147 RTCA DO-197A RTCA DO-185A RTCA DO-260A Deviation 1. Garmin was granted a deviation from TSO-C147 section 1.c to use RTCA DO-160E, instead of RTCA DO-160D as the standard for Environmental Conditions and Test Procedures for Airborne Equipment. 1. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.2.1 to use the Interrogations Spectrum requirement of RTCA DO-185A section 2.2.3.3 instead of the requirement of RTCA DO197A section 2.2.3.
1.5.2.2 GTS 820 TSO/ETSO TSO-C147 RTCA DO-197A RTCA DO-185A RTCA DO-260A Page 1-6 Revision 4TP Deviation 1. Garmin was granted a deviation from TSO-C147 section 1.c to use RTCA DO-160E, instead of RTCA DO-160D as the standard for Environmental Conditions and Test Procedures for Airborne Equipment. 2. Garmin was granted a deviation from TSO-C147 Appendix 1 section 1.6 to use selective Mode S interrogations as specified by RTCA DO-185A section 2.2.3.8.1 and 2.2.3.
1.5.2.3 GTS 850 TSO/ETSO TSO-C118 RTCA DO-197A RTCA DO-185A RTCA DO-260A Deviation 1. Garmin was granted a deviation from TSO-C118 section a.(2) to use RTCA DO-160E, instead of RTCA DO-160B as the standard for Environmental Conditions and Test Procedures for Airborne Equipment. 1. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.2.1 to use the Interrogations Spectrum requirement of RTCA DO-185A section 2.2.3.3 instead of the requirement of RTCA DO197A section 2.2.3.2.1. 2.
1.6 Reference Documents The following publications are sources of additional information for installing the GTS 8XX. Before installing the GTS 8XX, the technician should read all referenced materials along with the manual.
1.7 Limited Warranty This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will at its sole option, repair or replace any components that fail 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.
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2 2.1 INSTALLATION OVERVIEW Introduction This section provides hardware equipment information for installing the GTS 8XX/GPA 65 and related hardware. Installation of the GTS 8XX/GPA 65 should follow the aircraft TC or STC requirements. Cabling is fabricated by the installing agency to fit each particular aircraft. The guidance of FAA advisory circulars AC 43.13-1B and AC 43.13-2A, where applicable, may be found useful for making retro-fit installations that comply with FAA regulations. 2.1.
For a GTS 800 installation with a single GA 58 directional antenna, two QMA Connector Kits (4 pieces, either straight or right angle) are required. For a GTS 800 installation with dual GA 58 directional antennas, four QMA Connector Kits (4 pieces, either straight or right angle) kits are required.
2.2 Installation Considerations Fabrication of a wiring harness is required. Sound mechanical and electrical methods and practices are required for installation of the GTS 8XX/GPS 65. 2.2.1 Antenna Considerations Antenna installations on pressurized cabin aircraft require FAA approved installation design and engineering substantiation data whenever such antenna installations incorporate alteration (penetration) of the cabin pressure vessel by connector holes and/or mounting arrangements.
2.2.1.1 TAS/TCAS Antenna Location To achieve proper interrogation and surveillance volumes the following GTS 8XX antenna installation guidelines should be followed. The GTS 8XX requires a top-mounted directional antenna. An optional bottom mounted directional or L-band monopole antenna can be installed in conjunction with the top-mounted directional antenna. Antenna locations are critical to maintain the surveillance coverage across all azimuth and elevation angles.
2.3 Electrical Bonding Electrical equipment, supporting brackets, and racks should be electrically bonded to the aircraft’s main structure. Refer to SAE ARP 1870 section 5 when surface preparation is required to achieve electrical bond. The electrical bond should achieve direct current (DC) resistance less than or equal to 2.5 milliohms to local structure to where the equipment is mounted. Compliance should be verified by inspection using a calibrated milliohm meter.
The maximum wiring length from the GTS 8XX to the GPA 65 is 45 feet. Table 2-1.
2.4.1 Coaxial Cable The GTS 800 requires two sets of coaxial cable assemblies and the GTS 820/850 requires three sets of coaxial cable assemblies when a directional GA 58 antenna (or other Garmin approved antenna) is used for both top and bottom. Each set consists of four coaxial cable assemblies. Each set of four cables must be assembled using the same type of coaxial cable in order to meet phase and attenuation matching requirements.
Figure 2-2. GTS 800 Installation with Top and Bottom Monopole Antennas If no bottom mount antenna is installed, each of the GTS 800 bottom jacks (J1 BTM, J2 BTM, J3 BTM and J4 BTM) must be terminated with a QMA 2 watt termination as specified in Table 2-2 and shown in Figure 2-3. Figure 2-3.
2.4.1.2 GTS 820 and GTS 850 Installations GTS 820 and GTS 850 installation with both top and bottom mount directional antennas use one set of coaxial cables for the four GTS 820 or GTS 850 TOP jacks (J1 TOP, J2 TOP, J3 TOP, J4 TOP) that are connected to the corresponding GPA 65 processor unit jacks (J1U, J2U, J3U, J4U). Each top cable assembly shall not exceed the maximum attenuation of 3.0dB at 1090MHz as shown in Figure 2-4 and stated in Table 2-3.
Figure 2-5. GTS 820 and GTS 850 Installation with Top Directional and Bottom Monopole Antenna If no bottom mount antenna is installed, each of the GTS 820 or GTS 850 bottom jacks (J1 BTM, J2 BTM, J3 BTM and J4 BTM) shall be terminated with a QMA 2 watt termination as specified in Table 2-2 and shown in Figure 2-6. Figure 2-6.
NOTE Any QMA terminations used other than those specified in Table 2-2 will constitute the installation as being non-compliant with the manufacturer’s installation standards. 2.4.1.3 Fabrication of Coaxial Cable Assemblies The installing agency may fabricate cable assemblies by terminating either M17/128-RG400 or M17/60-RG142 coaxial cable with available QMA connector kits. Table 2-2 lists recommend cable types to be used with specified QMA connectors for the GTS 8XX. Table 2-2.
Table 2-3. Recommended Coaxial Length Loss of 2.5 dB Loss of 3.0 dB RG Type 1' 10" [0.55m] 2' 7" [0.79m] 9' 0" [2.74m] 12' 0" [3.66m] 15' 5" [4.70m] 18' 8" [5.68m] 15.5 M17/128 -RG400 RG-400 2' 0" [0.60m] 2' 9" [0.84m] 10' 5" [2.94m] 13' 0" [3.96m] 16' 6" [5.03m] 20' 1" [6.12m] 14.45 M17/60RG142 RG-142 2' 5" [0.74m] 3' 4" [1.02m] 11' 6" [3.50m] 15' 5" [4.70m] 19' 6" [5.94m] 23' 10" [7.26m] 12.16 311901 3' 3" [0.99m] 4' 6" [1.37m] 15' 8" [4.77m] 21' 0" [6.40m] 26' 8" [8.
The coaxial cable lengths in each coaxial cable assembly set used to connect the GTS 800 TOP and BOTTOM jacks to the top and bottom antenna jacks, the TOP GTS 820 or GTS 850 jacks to the GPA 65 jacks, and the BOTTOM GTS 820 or GTS 850 jacks to the directional antenna jacks, shall be within 2 inches of each other. The coaxial cable assembly lengths in each coaxial cable assembly set between the GPA 65 jacks and directional antenna jacks for the GTS 820 or GTS 850 shall be within 0.25 inches of each.
2.4.1.4 Coaxial Cable Assembly Instructions The following assembly instructions apply to coaxial cables assemblies using QMA connectors specified in Table 2-2 for use with RG-400 or RG-142 cable types: 1. Slide the heat shrink sleeve and crimp ferrule onto the cable. 2. Strip the cable to the dimensions shown in Figure 2-7. Figure 2-7. RG-400/RG-142 Coaxial Cable Stripping Dimensions 3. Slide the center contact onto the center conductor of the cable.
Figure 2-9. Heat Shrink Positioning NOTE Use of QMA connectors other than those specified in Table 2-2 for coaxial cable assemblies fabricated by the installing agency using either M17/128-RG400 or M17/60-RG142 coaxial cable will constitute the cable assemblies as being non-compliant with the manufacturer’s installation standards. 2.4.1.
2.6 Mounting Requirements The GTS 8XX can be mounted vertically or horizontally using the installation racks shown below. Refer to Appendix A for outline and installation drawings. Figure 2-10. GTS 8XX Vertical Installation Rack (Garmin P/N115-00781-00) Figure 2-11.
3 INSTALLATION PROCEDURE 3.1 Unpacking Unit Carefully unpack the equipment and make a visual inspection of the unit for evidence of damage incurred during shipment. If the unit is damaged, notify the carrier and file a claim. To justify a claim, save the original shipping container and all packing materials. Do not return the unit to Garmin until the carrier has authorized the claim. Retain the original shipping containers for storage.
Table 3-3.
NOTES 1. Non-Garmin part numbers shown are not maintained by Garmin and consequently are subject to change without notice. 2. Extracting a contact used for #18 AWG requires that the wire barrel be cut off from the contact. It may also be necessary to push the pin out from the face of the connector when using and extractor due to the absence of the wire. A new contact must be used when reassembling the connector. 3.
CAUTION Do not pull on the cable when removing the QMA plug from the jack. To disengage the QMA connectors, pull back firmly on the outer sleeve of the QMA plug away from the jack connector (refer to Figure 3-2). This will disengage the locking mechanism that secures the plug connector to the jack connector. Pulling on or disengaging the QMA connectors in any other way is not recommended and may cause damage to both the connectors and coaxial cable. Disengage Outer Sleeve Figure 3-2.
3.4 Backshell, Pigtail Circular Connector, and Configuration Module Assemblies The GTS 8XX connector kits includes three Garmin backshell assemblies. The backshell assembly houses the configuration module, if applicable. Garmin’s backshell also gives the installer the ability to easily terminate shield grounds at the backshell housing. Refer to the Jackscrew Backshell Installation Instructions (Garmin part number 190-00313-11) for backshell assembly instructions.
3.5.1 Post Installation Configuration & Checkout Before beginning the installation calibration, the installer must perform a visual inspection to verify the coaxial cables are installed correctly based upon the system and antenna configuration. NOTE Tests performed with a ramp tester should be performed away from buildings that may reflect the signal. Local air traffic control should be advised if the ramp tester has an altitude programmed into it that may cause interaction with other TCAS-equipped traffic.
3.5.2.1 Normal System Mode Tab The Normal tab displays various faults, flags, and operational information. When the Normal tab is selected, the unit is commanded to Normal System Mode. Figure 3-3. GTS 8XX Install Tool – Normal Tab Normal Mode – System Faults: Red Bold text indicates that a fault is active. Gray text indicates that there is no active fault. (System Faults are described in the Self-Test section.) Status Flags: Black Bold text indicates that a flag is set.
3.5.2.2 Configuration System Mode Tab The Configuration tab displays configuration data and allows the installer to change the installation configuration. When the Configuration tab is selected, the unit is commanded to Configuration System Mode. Figure 3-4.
Figure 3-5. GTS 8XX Install Tool – Configuration Tab (GTS 820 and GTS 850) The Configuration tab displays installation configuration options. Changes made in the Configuration tab are not immediately committed to the GTS. Changed options will be colored yellow until ‘Set Active’ is selected. Configuration Mode – Barometric Altitude Source: Note: At least one source must be selected (same altitude source used for the transponder).
GPS Position/Velocity/Time Source: Note: At least one source required for ADS-B IN functionality. Primary A429 RX Channels 1 - 6 or Disabled Secondary A429 RX Channels 1 - 6 or Disabled Traffic Display Destination: Note: At least one source is required. Primary A429 TX Channels 1 - 6 or Disabled COM RS-232 Ports 1 - 5 or Disabled Transponder 1 & 2 Communication: Note: At least Transponder 1 RX and TX required for GTS 820 and GTS 850. Primary should be configured for channels wired to Transponder 1.
Volume Level: Allows audio volume level selection from 0 to -63 dB in 0.5 dB increments. Maximum audio output is at least 80 mW into a 600 Ohm load. (6.93 Vrms) Voice Gender: Enter voice preference selection. Gear/Wheel: Enter type of aircraft gear design. ADSB TX Capable: Indicate whether aircraft is equipped with ADS-B transmitter. Squat ‘on-ground’ Sense: Indicate type of sense switch. Mode S ID (HEX): Applicable to GTS 820 and GTS 850 only.
3.5.2.3 Upload System Mode Tab The Upload tab displays version information for Boot Block, Region List, System, FPGA, Audio, Magnetic Variation. Boot Block updating is not allowed. For other files, select the appropriate image files and select upload. Figure 3-6. GTS 8XX Install Tool – Upload Tab 3.5.2.4 Debug Tab The Debug tab is reserved and not available for field installation use.
3.5.3 CDTI Display Setup and Configuration For configuration of the displays, refer to their respective installation manuals. • • • • • 3.5.
k) Receiver Calibration fault. Check antenna installation and all cable connections and retry self test. Ensure that self test occurs in area free of buildings and large objects that can reflect signals. If fault persists, return unit to Garmin for service. NOTE Receiver self-calibration is performed prior to the transmitter self-calibration. In the event that a receiver calibration fault occurs, a transmitter self-calibration will not be performed. l) Transmitter Calibration fault.
When the display receives an indication that a pilot initiated Self Test is in progress, this state is clearly annunciated on the traffic display and the following test patterns will be executed. Figure 3-7. Self Test Table 3-5. Self Test Intruder #1 (transmitted in intruder number field) 2.0 NM Vertical Rate = Climbing, relative altitude = –200 feet TA, Bearing = –90 degrees Intruder #2 (transmitted in intruder number field) 3.
3.5.5 Ramp Test and Return To Service Test Using a ramp tester, such as a TIC TR220 or equivalent, make the following setup and measurements to verify GTS 8XX operational and surveillance functional. To select a scenario that will properly converge and intercept the GTS 8XX, the GTS 8XX must be in Ground Test mode. To enable Ground Test mode, the aircraft must be on the ground and the GTS 8XX must be in Normal System mode and in Standby.
3.5.6 Antenna Verification The first step in antenna verification is to verify auto-calibration operates without indicating a fault. 1. With the GTS 8XX powered up and “Standby” indicated on the CDTI cycle the GTS 8XX to “Operate”. Each time the GTS 8XX transitions between these modes a self test of the antenna circuit is initialized. If the antenna connection is not correct the CDTI will display “Failure” indicating it will be necessary to recheck the antenna coaxial connections.
14. Reengage the same intruder scenario as above. 15. Verify a target is annunciated on the GTS 8XX TAS/TCAS display at the correct bearing of approximately 90 degree azimuth at 2 NM and co-altitude. 16. Toggle intruder traffic to standby or off. 17. Reposition ramp test set and directional antenna to an aft position of 180 degrees. 18. Reengage the same intruder scenario as above. 19.
3.6 GA 58 Antenna Installation Refer to the GA 58 installation drawing shown in Appendix A of this manual. CAUTION Do not use construction grade RTV sealant or sealants containing acetic acid. These sealants may damage the electrical connections to the antenna. Use of these type sealants may void the antenna warranty. 1. Refer to the GA 58 installation drawing shown in Appendix A for the mounting cutout. 2.
3.7 GPA 65 PA/LNA Installation Refer to the GPA 65 installation drawing shown in Appendix A of this manual. 1. Assemble the wiring harness and circular connector per Section 3.4. 2. Assemble the coaxial cables per Section 2.4.1. 3. Mount the unit to a suitable mounting location using #8-32 pan head screws (4 ea) (not provided). 4. Connect the circular connector and eight coaxial cables ensuring each coaxial cable is connected to the correct jack connector.
4 SYSTEM INTERCONNECTS 4.1 GTS 8XX Pin Function List 4.1.
Connector P8001, continued Pin 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 Pin Name SIGNAL GROUND CONFIG MODULE DATA SIGNAL GROUND ARINC 429 OUT 5 A ARINC 429 OUT 5 B ARINC 429 IN 5 A ARINC 429 IN 5 B SIGNAL GROUND ARINC 429 OUT 6 A ARINC 429 OUT 6 B ARINC 429 IN 6 A ARINC 429 IN 6 B SIGNAL GROUND ETHERNET OUT A ETHERNET OUT B ETHERNET IN A ETHERNET IN B SIGNAL GROUND RS-422 OUT A RS-422 OUT B SIGNAL GROUND CONFIG MODULE CLOCK TOP
4.1.
Connector P8002, continued Pin 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 Pin Name HEADING X LO (GROUND) SIGNAL GROUND HEADING Y HI HEADING Y LO (GROUND) SIGNAL GROUND SPARE EXTERNAL SUPPRESSION I/O SIGNAL GROUND TA DISPLAY ENABLE* AURAL TA ALERT* SPARE VISUAL TA ALERT* TRAFFIC SYSTEM STATUS VALID* RESERVED RESERVED SIGNAL GROUND ALERT AUDIO OUT HI ALERT AUDIO OUT LO HEADING Z HI (GROUND) HEADING Z LO (GROUND) SIGNAL GROUND 26 VAC HEADING
4.1.
4.2 GPA 65 Pin Function List 4.2.
4.3 Power 4.3.1 Aircraft Power Functions This section covers the power input requirements. 4.3.1.1 Aircraft Power Pin Name AIRCRAFT POWER 1 AIRCRAFT POWER 1 AIRCRAFT POWER 2 AIRCRAFT POWER 2 AIRCRAFT GROUND AIRCRAFT GROUND AIRCRAFT GROUND AIRCRAFT GROUND Connector P8003 P8003 P8003 P8003 P8003 P8003 P8003 P8003 Pin 2 3 4 5 21 22 23 24 I/O In In In In ----- Pins 2 and 3 are internally connected to form AIRCRAFT POWER 1. Pins 4 and 5 are internally connected to form AIRCRAFT POWER 2.
4.3.1.3 PA/LNA Pin Name +6 VDC PA/LNA POWER OUT +6 VDC PA/LNA POWER OUT +35 VDC PA/LNA POWER OUT +35 VDC PA/LNA POWER OUT -5 VDC PA/LNA POWER OUT -5 VDC PA/LNA POWER OUT +6 VDC POWER IN +6 VDC POWER IN +35 VDC POWER IN +35 VDC POWER IN -5 VDC POWER IN -5 VDC POWER IN Connector P8003 P8003 P8003 P8003 P8003 P8003 P651 P651 P651 P651 P651 P651 Pin 7 8 12 13 15 16 L P B M E S I/O Out Out Out Out Out Out In In In In In In Used to provide power to the GPA 65.
4.4 Serial Data 4.4.1 RS-232 Pin Name RS-232 OUT 1 RS-232 IN 1 RS-232 OUT 2 RS-232 IN 2 RS-232 OUT 3 RS-232 IN 3 RS-232 OUT 4 RS-232 IN 4 Connector P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 Pin 2 3 5 6 8 9 11 12 I/O Out In Out In Out In Out In The RS-232 outputs conform to EIA Standard RS-232C with an output voltage swing of at least ±5V when driving a standard RS-232 load. 4.4.
4.4.
4.4.5 USB Pin Name Connector Pin I/O USB VBUS POWER** P8001 75 In USB DATA HI** P8001 76 I/O USB DATA LO** P8001 77 I/O USB GROUND P8001 78 -**Signals have ESD (Electrostatic Discharge) protection, but not lightning protection. USB TYPE B RECEPTACLE pigtail cable must be wired directly to P8001 to minimize lightning exposure. This interface is used for unit configuration and software uploads. Conforms to the Universal Serial Bus Version 1.1 standard for a “full-speed” device.
4.5 Configuration 4.5.1 Configuration Module Pin Name Connector CONFIG MODULE GND P8001 CONFIG MODULE PWR OUT** P8001 CONFIG MODULE DATA** P8001 CONFIG MODULE CLK** P8001 **Signals have ESD (Electrostatic Discharge) protection, but not lightning protection. 4.6 Pin 1 21 40 60 I/O --I/O I/O Pin 63 64 I/O In In Pin 71 72 I/O In In Analog/Discrete 4.6.1 Heading Input 4.6.1.1 26 Volt AC References Pin Name 26 VAC HEADING REF HI 26 VAC HEADING REF LO Connector P8002 P8002 Used to sample AC inputs.
4.6.2 Inputs From Gyros Pin Name HEADING X HEADING LO (GROUND) HEADING Y HEADING LO (GROUND) HEADING Z (GROUND) HEADING LO (GROUND) Connector P8002 P8002 P8002 P8002 P8002 P8002 Pin 41 42 44 45 60 61 I/O In -In -In -- Inputs heading information from a directional gyro. 3-wire synchro magnetic heading input, with HEADING Z grounded. Index reference is 0° as specified by ARINC 407. Frequency: Voltage: Input Impedance: Resolution: Accuracy: 400Hz ± 10% 11.8 Vrms nominal, 13.0 Vrms maximum >10 kΩ ± 0.
4.6.5 Active High Discrete Inputs Pin Name Connector Pin I/O HEADING VALID P8002 68 In ANALOG RADAR ALTIMETER VALID P8002 76 In ACTIVE: 8 V ≤ Vin ≤ 36 V INACTIVE: 0 V ≤ Vin ≤ 3.5 V, or Rin ≥ 100k ohms Sink current is internally limited to approximately 1 mA typical for an input connected to +28VDC. 4.6.
APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-1.
APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-2.
APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-3.
APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-4.
APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-5.
APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-6.
APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-7.
APPENDIX B INTERCONNECT EXAMPLE Figure B-1.
APPENDIX B INTERCONNECT EXAMPLE Figure B-2.
APPENDIX B INTERCONNECT EXAMPLE Figure B-3.
APPENDIX B INTERCONNECT EXAMPLE Figure B-4.
APPENDIX B INTERCONNECT EXAMPLE Figure B-5.
APPENDIX B INTERCONNECT EXAMPLE Figure B-6.
APPENDIX B INTERCONNECT EXAMPLE Figure B-7.
APPENDIX B INTERCONNECT EXAMPLE Figure B-8.
APPENDIX B INTERCONNECT EXAMPLE The Configuration Module is only applicable for retrofit installtions Figure B-9.
