Avidyne IFD540 Installation Manual
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Avidyne IFD540 Installation Manual

Fms/ gps/ nav /com
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  • Page 2: Revision

    11, 29, 33, 49, 56-61, 66-67, 70, 74, 79-81, 84, 86, 94, 121 All materials copyrighted, including images that represent the software. Copyright 2014 Avidyne Corporation. All rights reserved. The latest installation manuals are available to authorized dealers on the web at www.avidyne.com.

  • Page 3: Table Of Contents

    Environmental Qualification Forms ................ 22 Databases ......................22 Fault Detection and Exclusion (FDE) ..............22 1.10 STC Approved Model List ..................23 1.11 Avidyne Supplied Material ..................24 1.11.1 Product Ship Kits ................... 24 1.11.2 Optional Ship Kits ..................24 1.12 Materials Required but not Supplied ..............
  • Page 4 IFD5XX Installation Manual 2. Installation Considerations..........26 Plug & Play Considerations ................... 26 Optional Installation Features ................27 IFD5XX Interfaces ....................27 Minimum System Configuration ................33 2.4.1 VFR Installation ....................34 2.4.2 IFR Installation ....................34 Pre-Installation Checklist ..................37 3.
  • Page 5 IFD5XX Installation Manual 3.4.6 Antenna Ground Plane ..................44 Navigation Antennas ....................44 3.5.1 VOR/LOC Antenna .................... 44 3.5.2 Navigation Coaxial Cable .................. 44 3.5.3 Navigation Coaxial Cable Connector ..............44 3.5.4 Diplexer ......................44 Glideslope Antenna ....................44 3.6.1 Glideslope ......................
  • Page 6 IFD5XX Installation Manual 5.1.1 Determining the Field of View ................50 5.1.2 Navigation Annunciation ..................51 5.1.3 Course Deviation Indicator ................53 5.1.4 Instrument Panel Cutout ..................53 5.1.5 Requirements for Tray Installation ..............53 Equipment Location - Replacement Unit ............... 54 Angle of Regard .....................
  • Page 7 IFD5XX Installation Manual Traffic System ......................69 Lightning Detection System ................... 69 Satellite Weather ....................70 Audio Panels ......................70 GAD 42 ........................70 Air Data System Sources..................72 Heading System Sources ..................73 6.10 Multifunction Displays .................... 74 6.11 Terrain Alerting ......................
  • Page 8 IFD5XX Installation Manual 7.5.8 VOR/LOC/GS CDI (Page 7 of 10) ..............96 7.5.9 VOR/LOC/GS ARINC 429 Configuration (Page 8 of 10) ........98 7.5.10 GPS Vertical Offset (Page 9 of 10) .............. 100 7.5.11 GDL Configuration Pages (Page 10 of 10) ..........101 7.5.12 GAD 42 Configuration ..................
  • Page 9 IFD5XX Installation Manual ILS Flight Test ...................... 109 Autopilot ....................... 109 Sensors ........................ 110 9. Glove Validation Procedures ........... 111 Software and Database Update Procedures ..... 112 10.1 Data Updates ....................... 112 10.2 Datalogs Download ....................115 10.3 Software Update ....................117 Periodic Maintenance ..........
  • Page 10 IFD5XX Installation Manual Notes to Installers: The following important issues regarding the Avidyne 700-00182-XXX GPS/NAV/COM System installation should be noted during the planning stages. These installation instructions assume that the GPS/NAV/COM transceiver and GPS antenna can be installed in a structurally sound manner in accordance with the installation manual and AC 43.13-( ).

  • Page 11: General Information

    IFD5XX Installation Manual 1. General Information 1.1 Introduction This manual contains information about the physical, mechanical, and electrical characteristics of the Avidyne IFD5XX GPS/Navigation/Communication, and provides installation instructions for its components. 1.2 Applicability This manual applies to the following part numbers:...

  • Page 12: Technical Specifications

    IFD5XX Installation Manual 1.3 Technical Specifications The following section gives mechanical and electrical characteristics for the IFD5XX: 1.3.1 IFD5XX Specifications Physical Specifications Bezel Height 4.58 inches (116 mm) Bezel Width 6.25 inches (159 mm) Depth (w/Connectors) 11.00 inches (279 mm) Weight 6.75 ±...

  • Page 13: Gps Specifications

    IFD5XX Installation Manual 1.3.3 GPS Specifications Channels 16 channels (13 GPS, 3 GPS/WAAS/SBAS) Velocity 1000 knots maximum (below 60,000 ft) TTFF (Time to First Fix) 150 seconds Reacquisition 20 seconds Position Update Interval 0.2 seconds (5 Hz) Lat/Long Position Accuracy 3.4 meters Fault Detection/RAIM RAIM/FDE WAAS Beta 3 Compliant @ 5 Hz...

  • Page 14: Vhf Communication Transceiver Specifications

    IFD5XX Installation Manual 1.3.4 VHF Communication Transceiver Specifications Audio Output 65 mW into 150 load Audio Response <6dB Variation from 350 to 2500 Hz, 4kHz -18dB AGC Characteristics <6dB Variation from 10uV to 10mV Sensitivity 4uV (6dB (S+N)/N 30% mod @ 1KHz) 10mV spurious signal produces no more output than a Spurious Response desired signal at 6dB (S+N)/N...

  • Page 15: Vhf Navigation Specification

    IFD5XX Installation Manual 1.3.5 VHF Navigation Specification Glideslope Receiver 0 +/-.0091 ddm w/ test signal varied +/-17kHz. 60dB for Selectivity +/- 132kHz offset Sensitivity (flag) 10uV max Spurious Response >-60 dB Centering Accuracy 0 ± 0.02 DDM or better Deflection Response 67% of final value in 600msec Localizer Receiver Selectivity...
  • Page 16 IFD5XX Installation Manual article may be installed only if performed under 14 CFR Part 43 or the applicable airworthiness requirements. Title Type/Categories Ranges Number ILS Glide Slope Receiving Equipment Operating within TSO-C34e the Radio Frequency Range of 328.6-335.4 Megahertz (MHz) Airborne ILS Localizer Receiving Equipment TSO-C36e...

  • Page 17: Tso Deviations

    IFD5XX Installation Manual Title Type/Categories Ranges Number Traffic Advisory System Class A (Display TSO-C147 (TAS) Airborne Equipment Functions Only) Aircraft Flight Information Services – Broadcast (FIS-B) TSO-C157a Datalink Systems and Equipment Electronic Map Display TSO-C165 Equipment for Graphical Depiction of Aircraft Position VHF Radio Communications Transceiver Equipment TSO-C169a...
  • Page 18 IFD5XX Installation Manual Deviation(s) are used where appropriate for rapid pilot recognition of exceedances; The fuel flow indicators are a digital readout instead of pointer and dial. Environmental qualification TSO-C110a – Airborne Passive performed in accordance with DO- Thunderstorm Detection Equipment 160G rather than DO-160B.

  • Page 19: Non-Tso Functions

    IFD5XX Installation Manual Deviation(s) of 10 NM or less is selected; Smoothing and scaling algorithms at TSO-C157a – Aircraft Flight Information high map ranges remove small Services – Broadcast (FIS-B) Data Link patches of high-intensity NEXRAD Systems and Equipment returns in favor of surrounding lower-intensity returns.

  • Page 20: Partial Tso Functions

    IFD5XX Installation Manual 1.5.4 Partial TSO Functions The following IFD5XX TSOs are partial function: Description Comment Fuel Flowmeters Display Only TSO-C44c Airborne Passive Thunderstorm Detection Display Only TSO-C110a Equipment Traffic Alert and Collision Avoidance Display Only TSO-C118 System (TCAS) Airborne Equipment, TCAS I Traffic Advisory System (TAS) Airborne Display Only...

  • Page 21: Software And Hardware Design Assurance Levels

    IFD5XX Installation Manual 1.6 Software and Hardware Design Assurance Levels The IFD5XX contains software developed in accordance with DO-178B Level B, C, and D design assurance levels. The following table lists functions of the IFD5XX system and their corresponding software design assurance level. All complex electronic hardware devices were developed in compliance with DO-254 Level DO-178B Design Component...

  • Page 22: Environmental Qualification Forms

    IFD5XX Installation Manual DO-178B Design Component Function Assurance Level Maintenance Mode Table 11: DO-178B Software Design Assurance Levels 1.7 Environmental Qualification Forms The environmental Qualification for the IFD5XX is listed in Appendix A: Environmental Qualification Form. Note: If the IFD5XX has been exposed to extreme cold temperature prior start, it may take a warm up period to achieve standard performance.

  • Page 23: Stc Approved Model List

    IFD5XX, however, it will require additional installation approval (e.g. Field approval, STC, or TC amendment), reference FAA Advisory Circular 23-22 as needed. If installing a IFD5XX on a Part 27/29 aircraft via field approval, the Avidyne Helicopter tray must be used, reference Table 13.

  • Page 24: Avidyne Supplied Material

    IFD5XX Installation Manual 1.11 Avidyne Supplied Material The following Ship Kits are available for ordering from Avidyne Corporation. Note: Ship Kit content and/or Part numbers may change without notice, verify before ordering. 1.11.1 Product Ship Kits Ship Kit Ship Kit...

  • Page 25: Materials Required But Not Supplied

    IFD5XX Installation Manual Ship Kit Component 820-00101-001 ByteFlight Cable 033-00102-000 Table 15: ByteFlight Ship Kit 1.12 Materials Required but not Supplied The IFD5XX will require common installation supplies. The following items may be required for installation, but not supplied: Wire (Shielded and Un-shielded) Hardware (Screws, washers, nuts, ring terminals, etc) Circuit Breakers Tie wrap or Lacing Cord...

  • Page 26: Installation Considerations

    TAWS compliance, the IFD5XX cannot be installed without a separately installed EGWPS/TAWS unit. For those installations that use a combined IFD5XX – Avidyne AXP340 Mode S ADS-B transponder, the on-ground/in-air discrete signal wire may need to be added from the IFD5XX tray to the AXP340 tray as identified in Section 6.12.

  • Page 27: Optional Installation Features

    The IFD5XX can interface with a host of other avionics equipment. The following list represents the proven interfaces. There may be other devices that can be configured the same as one on the below list but Avidyne has not tested it and can therefore not make any compatibility claims.
  • Page 28 KEA-346 Terra AT-3000 Sandia SAE5-35 Trans-Cal Industries IA-RS232-X Trans-Cal Industries SSD120 ACK Technologies A-30 EFIS Bendix King EFS 40/50 Avidyne EXP5000 Aspen Pilot PFD (EFD1000) Collins Proline 21 Collins EFIS 84 Honeywell Primus 1000 Sextant SMD 45 Displays Garmin GDU 620 (G500/600)
  • Page 29 GPSMAP 695 Garmin GPSMAP 696 Garmin Aera 796/795 Argus 3000 Argus 5000 Argus 7000 Horizon DDMP Avidyne EX500 Avidyne EX600 Avidyne EX5000 Avidyne FlightMax Series Heading Bendix King KAH 460 Inertial System (KAU 461 also) Collins AHC 85 Inertial System...
  • Page 30 Bendix King KTA-870 Bendix King KTA-970 Bendix King KMH980 Bendix King KMH880 Garmin GTS800/820/850 Ryan TCAD 9900B Ryan TCAD 9900BX Avidyne TAS-6XX series Transponder Garmin GTX330 Garmin GTX330 ES Garmin GTX 330D ES Garmin GTX 327 Trig TT31 Avidyne AXP340...
  • Page 31 IFD5XX Installation Manual Category Vendor Model Bendix King KAP150 Bendix King KAP140 Bendix King KAP100 Century Century Century Century Century Century 31/41 Century 2000 Century Triden Century AK 1081 GPSS Converter Collins APC-65 Series Collins FGC-65 Collins FYD-65 STec STec STec STec STec...
  • Page 32 IFD5XX Installation Manual Category Vendor Model Bendix King KN65 Bendix King KDI 572 Bendix King KDI 574 Bendix King KDM706 Collins DME 40 Collins DME 42 Collins TCR 451 Narco DME 890 Narco IDME 891 ARC (Cessna) RTA-476A Nav Indicator Garmin GI 102/A Garmin...

  • Page 33: Minimum System Configuration

    MD41-14XX Staco Switch 992561 Vivisun 95-40-( ) Vivisun 95-45-( ) Remote TAWS Annunciator Garmin 013-0079-XX Mid Continent MD41-10XX Audio Panel Avidyne AMX240 Apollo (Garmin) SL10 Apollo (Garmin) SL15 Garmin GMA 340 Garmin GMA 347 PS Engineering 6000 PS Engineering 7000...

  • Page 34: Vfr Installation

    IFD5XX Installation Manual 2.4.1 VFR Installation This section is intended for stand-alone IFD5XX installations intended for VFR navigation on un-pressurized aircraft less than 6000 pounds. The following items must be installed in IFD5XX VFR Configuration: IFD5XX unit GPS Antenna (TSO-C144a or TSO-C190, reference Section 3.3.5 for approved antennas) VHF Communication Antenna is needed for communication functions...
  • Page 35 Note: All equipment required by 14 CFR 91.205 must be previously installed on the aircraft for IFR operations. If the IFD540 is installed per this section, it can provide guidance for the following operations conducted under instrument flight rules (IFR):...
  • Page 36 IFD5XX Installation Manual Air Data/ Audio Panel Heading Data Autopilot CDI/HSI Datalink (WSI, XM, etc.) Lightning EFIS/MFD Detection Switches/ Traffic System Annunciators Avidyne IFD5XX Antenna GPS/Nav/Comm Transponder Fuel Antenna Management System Antenna Antenna EGPWS CrossSync to 2 Encoding Altimeter Figure 1: Full IFR Installation...

  • Page 37: Pre-Installation Checklist

    This checklist will help in determining installation requirements. If the Installation Items below are not complete, additional installation approval may be required. Installation Item Reference IFD5XX Complete Is the aircraft on the Avidyne STC Approved Avidyne Document □  Model List? AVIFD-306...

  • Page 38: Antenna Installation

    Antenna installations are beyond the scope of this manual and a separate installation approval is required. The Avidyne GPS antenna, Avidyne Part Number 200-00260-000, can be installed as shown in the following Figures in Appendix C: Figure C - 35, Figure C - 36, and Figure C - 37. The GPS Antenna must be installed using the following guidelines to be in compliance with the STC.

  • Page 39: Gps Location

    IFD5XX Installation Manual saddle is to act as a tapered shim and is not intended to transfer load into the skin Doubler Fabrication: Doubler material is to be 2024-T3 clad aluminum per AMS QQ-A-250/5 Form the doubler to match the fuselage curvature Etch, alodine, and prime the doubler per the guidance provided in AC43.13-1B Drill holes and install rivets per AC43.13-1B...
  • Page 40 Antennas should be installed 3” or more from the windshield. 3.3.1.1 Aircraft Lightning Zone If installing an Avidyne GPS Antenna (Avidyne Part Number 200-00260-000), the GPS antenna is qualified to be installed in aircraft lightning zone 2A as defined by SAE ARP5414A and RTCA DO-160G.

  • Page 41: Gps Antenna Bonding

    IFD5XX Installation Manual Determine the Distance (in feet) to Aircraft Lightning Zone 2A for the aircraft on the Vertical Axis. Example: For example, if an aircraft shown in Figure 3 has a V 175 KIAS, the No Installation Area will be 7.2 feet. This is shown on Figure 2 with a dotted line and Figure 3 with a shaded area.

  • Page 42: Gps Coaxial Cable Connector

    IFD5XX Installation Manual If dual GPS Systems are installed on the aircraft, the GPS coaxial cables should be routed in such a manner to provide maximum separation between the two GPS coaxial cables. 3.3.4 GPS Coaxial Cable Connector The connectors on the GPS coaxial cable should be assembled per the connector manufacturer’s assembly instructions.

  • Page 43: Gps Interference

    IFD5XX Installation Manual 3.3.6 GPS Interference After installing the IFD5XX System, the GPS antenna must be tested to insure no interference is present. The GPS Antenna System is subject to interference from VHF COM transceiver, Emergency Locator Transmitter (ELT) antenna, or Direction Finder (DF) receiver which can radiate harmonics that can potentially interfere with the GPS antenna.

  • Page 44: Vhf Antenna

    IFD5XX Installation Manual 3.4.5 VHF Antenna The VHF Communication Antenna should meet one of the following Technical Standard Orders (TSO): TSO-C37( ), TSO-C38( ), TSO-C169( ). 3.4.6 Antenna Ground Plane The VHF Communication Antenna should be mounted on a minimum of 18 x 18 inch metal surface or ground plane.

  • Page 45: Electrical Installation

    All shield grounds should be grounded using the ground block on the IFD5XX tray backplate. Shield grounds should be as short as possible (shorter than 3.0”, if possible) Shield grounds on non-Avidyne equipment should be grounded per the manufacturer’s installation instructions. In the absence of any installation data, the shield wires can be connected to the connecter backshell or aircraft ground.

  • Page 46: Copper Overbraid Installation

    8 feet in length on IFD5XX RS-232 Channel 3 on P1001. Installations with longer installation lengths between IFD5XX units must use Byteflight cable. The ByteFlight wire is available from Avidyne, reference Table 15. 600-00299-000 Page 46 of 198...

  • Page 47: Databus Wiring - New Installations

    Aircraft installing one IFD5XX should connect the power and grounds as shown in Figure 4. Single Avionics Bus Avionics Bus IFD540 Aircraft Ground Figure 4: IFD5XX Power Distribution Aircraft with a maximum certified gross takeoff weight less than 6000 pounds must connect the dual IFD5XX as shown in Figure 5.
  • Page 48 IFD5XX Installation Manual Preferred Alternate Avionics Bus 1 Avionics Bus 2 Avionics Bus IFD540 IFD540 IFD540 IFD540 Aircraft Ground Aircraft Ground Aircraft Ground Aircraft Ground Figure 5: Dual IFD5XX Power Distribution (Aircraft <6000 lbs) Aircraft with a maximum certified gross takeoff weight greater than 6000 pounds must install the dual IFD5XX as shown in Figure 6.

  • Page 49: Electrical Load Analysis

    IFD5XX Installation Manual The installer is responsible for preservation of multiple power busses on the aircraft in accordance with manufacturer's original design and the requirements of 14 CFR Part 23. This includes maintaining electrical power to essential equipment. 4.10 Electrical Load Analysis Prior to installing the IFD5XX, an electrical load analysis (ELA) must be performed.

  • Page 50: Mechanical Installation

    IFD5XX Installation Manual 5. Mechanical Installation This section will describe the physical mounting of the IFD5XX in the aircraft. Aircraft installing the IFD5XX for VFR use only, as defined in Section 2.4.1, can install the IFD5XX unit in any location easily accessible to the pilot. However, the IFD5XX installation must not introduce any new hazards.

  • Page 51: Navigation Annunciation

    IFD5XX Installation Manual Figure 8: Field of View 5.1.2 Navigation Annunciation The navigation annunciations listed in Table 23 must be installed in the Pilot's Field of view. This may be accomplished in several ways. The following are acceptable: Use Navigation Annunciation on an existing Primary Flight Display or Horizontal Situation Indicator located in the Pilot's primary field of view If the IFD5XX is located within the acceptable field of view,...
  • Page 52 IFD5XX Installation Manual The IFD5XX should have the following annunciation within the Pilot's Field of View when installing an external annunciator: Navigation Annunciation Type VLOC Annunciate GPS Annunciate OBS Annunciate (optional) Waypoint Annunciate Terminal Annunciate Approach Annunciate Message Annunciate LOI, INTEG, or INTG Annunciate Table 23: Navigation Annunciation The navigation annunciators should be readable under all lighting conditions.

  • Page 53: Course Deviation Indicator

    AC 43.13-2B, Chapter 11, Paragraph 1104(a). 5.1.5 Requirements for Tray Installation The Avidyne Tray must be installed in the aircraft as described below in order to satisfy the structural requirements for the STC. Deviations to these requirements will require separate approval.

  • Page 54: Equipment Location - Replacement Unit

    “Status” tab along to bottom edge of the display and then press the “Info” Line Select Key as needed until “Temps” is displayed. Note the hottest source(s) on that page and supply that information to Avidyne Technical Support to include both the source and the associated temperature for follow-on guidance.

  • Page 55: Weight And Balance

    IFD5XX Installation Manual 5.8 Weight and Balance After installing the IFD5XX, the aircraft’s weight and balance must be updated after installation is complete. For those installations where an IFD5XX is replacing a GNS530 (any variant), since the IFD5XX is within 5% of the weight of the removed GNS530 (less than 1 pound difference), no new weight and balance must actually be performed according to AC 43.13-1B Change 1 Acceptable Methods, Techniques, and Practices Aircraft Inspection and Repair (Chapter 10) and AC 120-27E Aircraft Weight and Balance Control.

  • Page 56: System Installation

    IFD5XX Installation Manual 6. System Installation The following section will describe interfacing the IFD5XX to various other avionics and aircraft equipment. 6.1 Pin Function List The following Section Lists the Pin function for each connector. 6.1.1 P1001 Main Connector Description Signal Type VLOC Annunciate Output...
  • Page 57 IFD5XX Installation Manual Description Signal Type Main +To (1.65V Common) Output Main +From Output Main +Up (1.65V Common) Output Main +Down Output Main Ver +Flag Output Main Ver -Flag (GND) Main OBS Rotor C Output Main OBS Rotor H(GND) Main OBS Stator D Input Main OBS Stator E (2.5V Common OBS) Output...

  • Page 58: P1002 Communication Connector

    IFD5XX Installation Manual Description Signal Type GPS RS232 In 1 Input GPS RS232 Out 2 Output GPS RS232 In 2 Input Altitude Common (GND) Altitude C4 Input Altitude C2 Input Altitude C1 Input Altitude B4 Input Altitude B2 Input Altitude B1 Input Altitude A4 Input...

  • Page 59: P1006 Navigation Connector

    IFD5XX Installation Manual Pins Description Signal Type Reserved (Synchro X in – as of Release 10.1.0.0) Aircraft Power Input Aircraft Power Input Reserved (Synchro Reference Signal + - as of Release 10.1.0.0) Transmit Interlock (Unused) Input COM Remote Transfer Input Reserved Intercom Microphone Audio LO Input...

  • Page 60: P1050 Additional I/O Connector

    IFD5XX Installation Manual Pins Description Signal Ser DME-Chan Req/PAR DME - 4MHz Input/Output Ser DME-Rnav Mode/PAR DME - 2MHz Input/Output DME Common Input VOR/ILS Arinc-429 Out B Output VOR/ILS Arinc-429 Out A Output VOR OBI Clock Output VLOC OBI Sync Output VOR OBI Data Output...

  • Page 61: Altitude Gray Code

    IFD5XX Installation Manual Pins Description Signal Spare Annunc 2 Output Spare Annunc 1 Output TAWS Audio Active Out Output Reserved 17-21 Ground 22-59 NO CONNECT RS232 Out 5 Output RS232 IN 5 Input RS232 Out 6 Output RS232 IN 6 Input Ground 65-78...

  • Page 62: Main Course Deviation Indicator Output

    IFD5XX Installation Manual 6.1.6 Main Course Deviation Indicator Output The main indicator displays both lateral and vertical deviations, TO/From, and Flag indications from the NAV and GPS receivers. 6.1.6.1 Lateral/Vertical Deviations The lateral and vertical deviations are on the following connector and pins: Description Connector Signal Type...
  • Page 63 IFD5XX Installation Manual 6.1.6.4 Navigation Superflags The Navigation Superflags is on the following connector and pins: Description Connector Signal Type Main Lateral +Flag P1001 Output Main Lateral -Flag P1001 Output Table 32: Main Navigation Superflag Output Superflag outputs system voltage when valid and <.25 VDC when not valid. This output is capable of driving 500mA at 28 VDC or 250mA at 14 VDC.
  • Page 64 IFD5XX Installation Manual 6.1.6.6 Annunciators Electrical Output Description Connector Signal Type VLOC Annunciate P1001 Output GPS Annunciate P1001 Output Waypoint Annunciate P1001 Output Terminal Annunciate P1001 Output Approach Annunciate P1001 Output Message Annunciate P1001 Output OBS Annunciate P1001 Output Auto Annunciate P1001 Output Integrity Annunciate...

  • Page 65: Serial Data

    IFD5XX Installation Manual 6.1.7 Serial Data 6.1.7.1 RS-232 Description Connector Signal Type RS-232 Output 1 P1001 Output RS-232 Input 1 P1001 Input RS-232 Output 2 P1001 Output RS-232 Input 2 P1001 Input RS-232 Output 3 P1001 Output RS-232 Input 3 P1001 Input RS-232 Output 4...

  • Page 66: Com/Vor/Ils Audio Electrical Characteristics

    IFD5XX Installation Manual 6.1.9 Com/VOR/ILS Audio Electrical Characteristics 6.1.9.1 Com Microphone Key Description Connector Signal Type COM MIC Key P1002 Input Table 39: VHF Communication Microphone Key This input is active if either the voltage to ground <1.9V or the resistance to ground is <375 . This input is considered inactive if the voltage to ground is 11-33 VDC.

  • Page 67: Vor/Ils Indicator Electrical Characteristics

    IFD5XX Installation Manual Table 42: VHF Communication and Navigation Switch Inputs This input is active if either the voltage to ground <1.9V or the resistance to ground is <375 . This input is considered inactive if the voltage to ground is 11-33 VDC. COM Remote Transfer and VLOC Remote Transfer are momentary inputs.
  • Page 68 IFD5XX Installation Manual 6.1.11.1 Serial/Parallel Tuning Signal Description Connector Type NAV PAR DME – 8MHz P1006 Output SER DME – CHAN REQ/PAR DME – P1006 Output* 4MHz SER DME – RNAV MODE/PAR DME – P1006 Output* 2MHz NAV PAR DME – 1MHz P1006 Output NAV PAR DME –...

  • Page 69: Bezel Lighting

    The IFD5XX can be connected to Traffic Systems either by RS232 or ARINC 429. The IFD5XX supports the following Traffic Systems: Manufacturer Model Data Format Notes TAS6XX, 9900BX RS232 or RS-232 Avidyne Corporation ARINC 429 preferred SKY497, SKY899 ARINC 429 L3 Communications KTA-870, ARINC 429 Bendix/King...

  • Page 70: Satellite Weather

    IFD5XX Installation Manual 6.5 Satellite Weather The IFD5XX can be connected to Satellite Weather Systems via RS232. The IFD5XX supports the following Satellite Weather Systems: Manufacturer Model Data Format Notes Avidyne Corporation MLB700 RS232 GDL69/69A RS232 Version 4.01 or Garmin...
  • Page 71 IFD5XX Installation Manual strapping method as described in Garmin P/N 190-00159-00 GAD42 Installation Manual, Section 5.1. 600-00299-000 Page 71 of 198 Revision: 02...

  • Page 72: Air Data System Sources

    The IFD5XX can be connected to either Uncorrected or Baro-corrected Altitude Sources. The IFD5XX can be connected to the following Air Data Systems: Manufacturer Model Data Format Notes Aspen EFD1000 ARINC 429 Low Speed Avidyne Entegra PFD ARINC 429 Low Speed Garmin G500/600 ARINC 429 Low Speed B & D 90004-003...

  • Page 73: Heading System Sources

    Collins AHS-85E ARINC 429 High Speed Table 53: IRU/AHRS Systems The Avidyne IFD5XX can accept heading information via ARINC 429 from other IRU/AHRS sources if the following labels are provided: 314 - True Heading 320 - Magnetic Heading 600-00299-000 Page 73 of 198...

  • Page 74: Multifunction Displays

    Aviation format for MX20 version 5.6 and later. Aviation format for all Garmin GMX200 RS232 GMX200 versions Use GAMA format 2, low speed Avidyne ARINC EX500/EX600/EX5000 MFD software P/N Corporation 530-00193-( ) or later is required Avidyne GAMA output may Corporation also be used.

  • Page 75: Audio

    6.12 ADS-B/Transponder Output The IFD5XX will transmit ADS-B compliant GPS position data to the following compatible ADS-B capable transponders Manufacturer Model Notes Avidyne AXP340 ADS-B output requires a separate installation approval. Connect the appropriate input pin on the AXP340 with the...

  • Page 76: Autopilot

    IFD5XX Installation Manual 6.13 Autopilot The IFD5XX can be connected to various Autopilot Systems via analog or ARINC 429 connections. The IFD5XX supports the following Autopilot Systems: Manufacturer Model Data Format Notes KAP100/140/150, Analog KFC150/200/250/275 Deviation, /300/325 Discrete KCP 320 Honeywell KFC225 Analog...

  • Page 77: Configuration And Checkout

    IFD5XX Installation Manual 7. Configuration and Checkout After completing installation, a complete installation checkout should be performed. Complete the following sections to verify the installation is installed correctly. Prior to configuring the IFD5XX unit, the following checks should be performed. 7.1 Wiring Check Verify wiring is properly installed and secured.

  • Page 78: Unit Installation

    IFD5XX Installation Manual 7.4 Unit Installation Install unit in the tray using the captive 3/32” Hex screw. Verify the connectors are fully engaged prior to powering on the unit. 7.5 Configuration The IFD5XX can be configured in the aircraft. This section will describe the procedures for configuring the IFD5XX.

  • Page 79: Arinc 429 Port Configuration

    IFD5XX Installation Manual 7.5.2 ARINC 429 Port Configuration (Page 1 of 10) The ARINC 429 can be selected individually for each ARINC 429 Transmit and Receive Port. Each Transmit and Receive Port will have a “Speed” selection and “Data” selection. Figure 11: ARINC 429 Configuration Page The “Speed”...
  • Page 80 IFD5XX Installation Manual The “Data” will have the following INPUT options: Selection Description No device connected to this ARINC 429 input Airdata Altitude, temperature, and speed information from the following Air Data Systems: B&D 2600, 2601, 2800, 90004-003, Bendix/King KAD 280/480, Shadin ADC 2000 Airdata/AHRS Heading, altitude, temperature, and speed information from an Air...
  • Page 81 Traffic Advisory Traffic information from the following traffic advisory systems: Bendix/King KTA-870, KMH880 Garmin GTS 800/820/850 Avidyne TAS6XX (but RS-232 is preferred) (Ryan 9900BX) (but RS-232 is preferred) L3 Communications SKY497 Skywatch L3 Communications SKY899 Skywatch HP Table 62: ARINC 429 Input Selection Note: ARINC 429 devices should be wired to both IFDs in dual IFD installations since ARINC 429 data is not shared between IFDs on the CrossSync line.
  • Page 82 Sandel SN3308 Sandel SN3500 Aspen EFD1000 (see note below) Avidyne EX500 Avidyne EX600 Avidyne EX5000 Note: When integrating an Aspen EFD1000 with a dual IFD5XX installation, ensure the “CRS SDI” field in the Aspen setup pages (page 18) is set to Nav 1/2 and not Common.
  • Page 83 IFD5XX Installation Manual Selection Description Sextant 2nd Edition GAMA 429 Non- ARINC 429 data that is not necessarily conforming to the GAMA standard General Aviation Subset, 2 Edition. Table 63: ARINC 429 Output Selection Note: It is important in dual IFD installations that the corresponding SDI selection be made properly.

  • Page 84: Port Configuration

    IFD5XX Installation Manual 7.5.3 RS-232 Port Configuration (Page 2 of 10) The RS-232 Configuration Page allows the configuration Inputs and Outputs to match that of the equipment installed in the aircraft. Figure 12: RS-232 Configuration Page The following selections can be made on the RS-232 Input. Channel Inputs Selection Description...
  • Page 85 Other JPI systems (e.g. JPI FS-450) can use this setting but see the specific format guidance from JPI for the Garmin GNS series. MLB700 Serial weather data information from the Avidyne MLB700 Serial lightning data information from the Avidyne TWX670 WX-500...
  • Page 86 Serial position, altitude, velocity, and navigation data to the following units: Argus 3000, 5000, or 7000 Moving Map Avidyne FSD Series Garmin MX20 (V5.6 or later), GMX200 Garmin GPSMAP 195, GPSMAP 295 or GPS III Pilot Garmin GPSMAP 196, GPSMAP 296, and GPSMAP 396...

  • Page 87: Page 3 Of

    Garmin MX20 (V5.7 or later), GMX 200 WX-500 Serial communication to L3 Communications WX500 Stormscope MLB700 Serial weather data information to the Avidyne MLB700 and WSI AV-300 / 350 Serial communication to the Avidyne TWX670 Table 67: RS-232 Output Selection 7.5.4 Main System Configuration (Page 3 of 10)
  • Page 88 IFD so that the caution and warning indications generated by the TAWS system can be displayed to the pilot and so that the IFD's TA and FLTA functions will be inhibited. Avidyne TA/FLTA is not an approved TSO-C151 EGPWS unit. The IFD system supports a Honeywell KGP560/860 system only. All other external TAWS/EGPWS systems must be disabled if the internal TA and FLTA is operational on the IFD system.

  • Page 89: Page 4 Of

    IFD5XX Installation Manual 7.5.5 Main Input Configuration (Page 4 of 10) The Main Input Page displays information received from ARINC 429, RS-232, and other electrical inputs. This page is helpful during troubleshooting of the IFD5XX system. 7.5.6 Main Lighting Configuration (Page 5 of 10) The source of the lighting for the IFD5XX can be the bezel photocell sensor or the dimming bus.
  • Page 90 IFD5XX Installation Manual Photo Maximum The Photo Maximum sets the maximum brightness when the dimming source is the photocell. Both the Bezel and Display fields have a range of 50 to 100, and the factory default is 100. dimBus Transition % The dimBus Transition % sets the threshold where the aircraft dimming bus takes over from the photocell.
  • Page 91 IFD5XX Installation Manual The AviCurve tracks the aircraft dimming bus as follows: Figure 15: Lighting Curve - AviCurve Figure 16: Lighting Curve - Proportional Curve 600-00299-000 Page 91 of 198 Revision: 02...
  • Page 92 IFD5XX Installation Manual Field Selection Bezel Value displayed represents the current % brightness of the bezel backlighting Display Value displayed represents the current % brightness of the display backlighting Mx Input Photocell – Maintenance Mode will use this method if selected.

  • Page 93: Page 6 Of

    IFD5XX Installation Manual 7.5.7 Main CDI/OBS Config Page (Page 6 of 10) This page will test the Main CDI/OBS output on the IFD5XX. Figure 17: Main CDI/OBS Configuration Page The following parameters can be tested: CDI (LAT/VERT) Selection Description Max Left The remote CDI will be off-scale full deflection to the left/up Full Left The remote CDI will be deflected to the left/up...
  • Page 94 IFD5XX Installation Manual TO-FROM Selection Description From The From flag on the external indicator is in view Hidden The TO/FROM flag on the external indicator is hidden The TO flag on the external indicator is in view Table 75: Main CDI Flag Test Page Selected Course This section will calibrate the external CDI/HSI to the IFD5XX.
  • Page 95 IFD5XX Installation Manual OBI Source Selection Description Always GPS The MAIN Serial OBI output will always be selected to GPS. Track CDI The MAIN Serial OBI will track the Nav Source knob selection. Table 78: OBI Source Selection V-Flag State Selection Description Declutter...

  • Page 96: Page 7 Of

    IFD5XX Installation Manual 7.5.8 VOR/LOC/GS CDI (Page 7 of 10) This will test the operation of the VOR/LOC/GS output from the IFD5XX on the P1006 connector to an external CDI/HSI display. Figure 18: CDI Test Page CDI (LAT/VERT) Selection Description Max Left The external CDI will be off-scale full deflection to the left/up Full Left...
  • Page 97 IFD5XX Installation Manual SPR Flag (LAT/VRT Super Flag) Selection Description Hidden The lateral and vertical flag on the external indicator is hidden In view The lateral and vertical flag on the external indicator is in view Table 82: NAV Superflag Test Page TO-FROM Selection Description...

  • Page 98: Vor/Loc/Gs Arinc 429 Configuration

    IFD5XX Installation Manual 7.5.9 VOR/LOC/GS ARINC 429 Configuration (Page 8 of 10) This page will configure the ARINC 429 for the VOR/LOC/GS output. Figure 19: VOR/LOC ARINC 429 Configuration Page The following parameters can be configured. Speed: Selection Description Standard Low-speed ARINC 429 High High-speed ARINC 429 Table 85: VOR/LOC/GS ARINC 429 Speed Configuration...
  • Page 99 IFD5XX Installation Manual SDI: Selection Description Common RX: Accepts all 429 inputs TX: Generates all 429 outputs with SDI =0 VOR/ILS 1 Number 1 (Pilot) VOR/ILS Receiver RX: Accepts 429 inputs with SDI = 0 or 1 TX: Generates all 429 outputs with SDI = 1 VOR/ILS 2 Number 2 (Copilot) VOR/ILS Receiver RX: Accepts 429 inputs with SDI = 0 or 2...

  • Page 100: Gps Vertical Offset

    IFD5XX Installation Manual 7.5.10 GPS Vertical Offset (Page 9 of 10) This page will configure the GPS Receiver for the antenna offset on the aircraft and designate if the IFD5XX will use the WAAS functionality of the system. Figure 20: GPS Antenna Setup Measure the distance from the ground to the top of the GPS antenna to nearest tenth of a foot, as shown in the image below, and enter the value into the IFD5XX (to the nearest 1/10 foot).

  • Page 101: Gdl Configuration

    IFD5XX Installation Manual 7.5.11 GDL Configuration Pages (Page 10 of 10) This page allows the configuration of the Garmin GDL 69/69A. This page is always displayed in Maintenance Mode. The GDL 69/69A must be activated prior to configuring the IFD5XX, reference the GDL installation manual for setup and configuration information. Figure 22: GDL Configuration Page GDL Selection Page This page selects the attenuation and the type of GDL receiver connected to the IFD5XX.

  • Page 102: Gad 42 Configuration

    IFD5XX Installation Manual 7.5.12 GAD 42 Configuration The IFD5XX can be connected to the Garmin GAD42 Interface Adapter but there is no dedicated GAD42 configuration page in the IFD5XX. If the IFD5XX is replacing a GNS530/W that had previously been connected to a GAD42, then no action is required since the configuration is already saved in the GAD42.
  • Page 103 IFD5XX Installation Manual Figure 24: Software Version Page Figure 25: Fan Status Page 600-00299-000 Page 103 of 198 Revision: 02...

  • Page 104: Checkout

    IFD5XX Installation Manual Figure 26: IFD Temperature Status Page The pages on the “Diag” tab are for Avidyne Service Center diagnostics purposes and are not described in this manual. 7.6 Checkout After configuring the IFD5XX, the following post-installation tasks should be performed.

  • Page 105: Electrical Load Analysis

    IFD5XX Installation Manual Acceptable Methods, Techniques, and Practices Aircraft Inspection and Repair (Chapter 10) and AC 120-27E Aircraft Weight and Balance Control. 7.6.5 Electrical Load Analysis Verify the aircraft's electrical load is within limits, reference Section 4.10. 7.6.6 GPS Signal Acquisition After installation, position the aircraft outside with clear unobstructed view of the sky.

  • Page 106: Vor/Loc/ Gs Checkout

    IFD5XX Installation Manual 7.6.7.3 Receiver/Transmitter Operation Test VHF Com’s ability to receive and transmit to another VHF Com station. Verify using a low/middle/high frequency. 7.6.8 VOR/LOC/ GS Checkout If installed, test the VOR/LOC/GS system using a local frequency or test set. Verify the OBS (selected course) is functioning, CDI/HSI/PFD is indicting correctly, and NAV audio is received.

  • Page 107: Self-Test Page

    IFD5XX Installation Manual 7.6.14 Self-test Page For the duration that the notification of legal rights page is displayed during normal power up on the ground, all remote annunciator lamps are lit up and the system generates a specific set of electrical outputs for the purpose of self-test and troubleshooting. Table 89 below defines the outputs transmitted during this time.

  • Page 108: Ahrs/Iru Interface Check

    IFD5XX Installation Manual 7.6.16 AHRS/IRU Interface Check Verify the IFD5XX is receiving heading information from an external source. This can be verified on the Main Input Page in maintenance mode, reference Section 7.5.5. If power is removed from the external heading source, the Main Input Page will display dashed lines for heading.

  • Page 109: Flight Checks

    IFD5XX Installation Manual 8. Flight Checks The IFD5XX must be flight tested to verify the installation is operating properly. The following items should be tested in flight to verify the IFD5XX function. 8.1 GPS Flight Test Verify the following in flight: Verify the GPS reception during all phases of flight.

  • Page 110: Sensors

    IFD5XX Installation Manual Evaluate the autopilot's response to a GNSS fault (e.g., pulling the IFD5XX Circuit Breakers) 8.6 Sensors Verify the IFD5XX interface to other aircraft sensors are operating correctly (e.g., Traffic, Lightning, Weather, etc). 600-00299-000 Page 110 of 198 Revision: 02...

  • Page 111: Glove Validation Procedures

    IFD5XX Installation Manual 9. Glove Validation Procedures Many types of gloves can be used with the IFD touch screen display. The key parameter for the effectiveness of a glove with touch screen is the distance between the finger and the glass and to a lesser extent, the type of material separating the skin from the glass.

  • Page 112: Software And Database Update Procedures

    Use one of the formatted fobs supplied by Avidyne (marked by the Avidyne logo printed on one side). In the event one of those fobs are not available, either call Avidyne for a replacement fob (a nominal fee will be charged) or purchase a replacement through other means.
  • Page 113 IFD5XX Installation Manual Figure 27: Update Databases LSK You will be prompted to “Confirm” or “Cancel”. Assuming you selected “Confirm”, you should see a dialog box presented in the middle of the screen and all uploadable files on that fob will be individually listed and check marks may be visible next to each file name. Figure 28: Confirm and Cancel LSK Use the “Select All”, “Un-select All”...
  • Page 114 IFD5XX Installation Manual Figure 29: LSK Options A progress bar will be presented to help provide an idea of how much longer the upload will take. Figure 30: Progress Bar Typical upload times are: Worldwide Obstacles (1.5 MB) – 5 sec Eastern US Charts (100 MB) –...

  • Page 115: Datalogs Download

    For multiple IFD installations, the database uploads must be performed individually for each IFD to be updated. Due to some of the upload durations, Avidyne recommends creating a fob for each IFD to be updated so that the updates can happen in parallel and not stacked serially, thereby extending the overall time to accomplish a full update.
  • Page 116 Event Log – This log contains miscellaneous data such as all alerts, keystrokes, system status and error messages, etc. It is designed to be diagnostics log for Avidyne Service Center technicians and not expected to be used by owners/operators. It logs at an on-condition rate;...

  • Page 117: Software Update

    IFD5XX Installation Manual In order to provide an indication of download progress, a progress bar will be presented with both a symbolic aircraft indicating download in progress and a % complete estimate. The files to be downloaded can have one of several states – “OK”, “In progress…”, “Pending”, “Skipped”, “Active”, “Failed”.

  • Page 118: Periodic Maintenance

    IFD5XX Installation Manual 11. Periodic Maintenance The IFD5XX does not require any periodic or preventative maintenance. Maintenance on the IFD5XX is on condition. 11.1 Equipment Calibration The IFD5XX has no required servicing tasks. 11.2 VOR Checks Every 30 days, verify the limits of the VOR per 14 CFR §91.171. Only required for IFR operations.

  • Page 119: Factory Service Policies And Procedures

    For After Hours Technical Support, via the following: AOG Support: 877-900-4AOG (4264) 12.2 General Service Procedures Repair of the IFD5XX are performed at authorized Part 145 service centers and the Avidyne factory. Prior to returning a unit for service, contact Avidyne at 1-888-723-7592 to obtain a Return Merchandise Authorization (RMA) number.

  • Page 120: Bezel And Display Cleaning

    The use of any 3rd party screen protector, especially those that adhere directly to the IFD display glass, is not endorsed by Avidyne due to the touch-screen nature of the display and may void the warranty for any display related issue.

  • Page 121: Appendix A: Environmental Qualification Form

    ‡ Plug & Play VFR Installations – Installer has option to use existing tray; New VFR Installations – Installer should use Avidyne's Helicopter Tray, reference Table 13; All IFR Installations – Installer must use Avidyne’s Helicopter Tray, reference Table 13.

  • Page 122: Appendix B: Stc Permission

    Avidyne Corporation hereby grants to all National Aviation Authorities (FAA, CAA, JAA, etc) approved installers the use of data from STC SA00343BO to install the Avidyne IFD5XX System. This also includes any international validations of the STC (e.g. EASA, ANAC, etc).

  • Page 123: Appendix C: Mechanical Drawings

    IFD5XX Installation Manual Appendix C: Mechanical Drawings Figure C - 33: Tray Installation 600-00299-000 Page 123 of 198 Revision: 02...
  • Page 124 IFD5XX Installation Manual Figure: C - 34: Instrument Panel Cutout 600-00299-000 Page 124 of 198 Revision: 02...
  • Page 125 IFD5XX Installation Manual Forward Figure C - 35: GPS Antenna Installation 600-00299-000 Page 125 of 198 Revision: 02...
  • Page 126 IFD5XX Installation Manual ‡ Fuselage Skin Adjacent Structure Doubler Outer Rivet Row in Inner Four Rivet in Thickness Rivet Type Thickness Doubler Doubler 0.016" - 0.025" Dimpled skin / 0.020" MS20426AD3 MS20426AD3 Countersunk Rivets (Double Dimple) (Double Dimple) 0.016" - 0.025" Protruding Head 0.020"...
  • Page 127 IFD5XX Installation Manual Figure C - 37: GPS Antenna Doubler 600-00299-000 Page 127 of 198 Revision: 02...

  • Page 128: Appendix D: Electrical Interface Drawings

    IFD5XX Installation Manual Appendix D: Electrical Interface Drawings Figure D - 1: Lighting, Power, and Antenna Interconnect ..............130 Figure D - 2: Blind Altitude Encoders Interconnect ................133 Figure D - 3: RS-232 Serial Data Interconnect ..................134 Figure D - 4: EFIS Interconnect .......................136 Figure D - 5: Generic EFIS Interconnect ....................137 Figure D - 6: EHSI ARINC 429 Interconnect, Dual IFD5XX, Sandel SN3308 Interconnect ....138 Figure D - 7: ARINC 429/RS-232 Air Data/IRU/AHRS Interconnect ..........140...
  • Page 129 Figure D - 33: Garmin GAD 42 Interconnect ..................172 Figure D - 34: Garmin G600 Interconnect ....................173 Figure D - 35: Avidyne Entegra Interconnect ..................174 Figure D - 36: Avidyne EX500/600/5000 Interconnect ...............175 Figure D - 37: Aspen EFD1000 Interconnect ..................176 Figure D - 38: Transponder Interconnect ....................177...
  • Page 130 IFD5XX Installation Manual AVIDYNE IFD540 P1001 AIRCRAFT POWER 1 AIRCRAFT POWER 18 AWG 22 AWG 5A for 28VDC AIRCRAFT POWER 1 7.5 for 14VDC 22 AWG AIRCRAFT POWER 2 AIRCRAFT POWER 18 AWG 22 AWG 5A for 28VDC AIRCRAFT POWER 2 7.5 for 14VDC...
  • Page 131 IFD5XX Installation Manual IFD540 #1 P1003 GPS ANTENNA GPS ANTENNA 1 P1004 COM ANTENNA COM ANTENNA 1 P1005 VOR/LOC ANTENNA P1007 GLIDESLOPE ANTENNA G/S 1 VOR 1 DIPLEXER NAV ANTENNA IFD540 #2 G/S 2 VOR 2 P1007 GLIDESLOPE ANTENNA P1005...
  • Page 132 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. IF AIRCRAFT HAS MULTIPLE POWER BUSSES, IT IS RECOMENDED THAT IFD540 POWER CONNECTIONS BE CONNECTED AS DESCRIBED IN SECTION 4. AIRCRAFT POWER INPUT TO THE IFD5XX MAY BE 9-33 VDC.
  • Page 133 ACK Technologies Trans-Cal Sandia Bendix/King Terra Or Blind Encoder A-30 SSD-120 IA-RS232C-D SAE 5-35 KEA 130A KEA 346 AT 3000 IFD540 DB15 DB15 DB15 (MALE) P1001 ALTITUDE D4 ALTITUDE A1 ALTITUDE A2 ALTITUDE A4 ALTITUDE B1 ALTITUDE B2 ALTITUDE B4...
  • Page 134 GPS RS-232 IN 1 RS-232 OUT HI SHELL SHELL SHELL SHELL RS-232 OUT LO P1001 IFD540 GPS RS-232 IN 3 GPS RS-232 OUT 3 GPS RS-232 IN 3 GPS RS-232 OUT 3 PORTABLE RS-232 DEVICE GPS RS-232 OUT 4 RS-232 IN...
  • Page 135 IFD5XX Installation Manual NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE. REFER TO SECTION 7 FOR RS-232 CHANNEL SETTINGS REFER TO THE GTX 327 TRANSPONDER INSTALLATION MANUAL, 190-00187-02, FOR COMPLETE INFORMATION.
  • Page 136 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE – THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
  • Page 137 IFD5XX Installation Manual ARINC 429 EFIS DISPLAY #1 IFD 540 #1 P1001 LNAV TRANSMITTER A GPS ARINC 429 IN 1 A LNAV TRANSMITTER B GPS ARINC 429 IN 1 B GPS ARINC 429 OUT A LRN/LNAV 1 RECEIVER A GPS ARINC 429 OUT B LRN/LNAV 1 RECEIVER B LRN/LNAV 2 RECEIVER A P1006...
  • Page 138 IFD5XX Installation Manual ARINC 429 EHSI Sandel DISPLAY #1 SN3308 IFD 540 #1 P1006 NAV ½ RELAY SENSE VOR/ILS 1 (RELAXED) VOR/ILS ARINC 429 OUT A 429-2 RX-A VOR/ILS ARINC 429 OUT B 429-2 RX-B VOR/ILS 2 (ENERGIZED) AIRCRAFT POWER VHF NAV 2 SWITCHING RELAY P1001 GPS 2 SWITCHING RELAY...
  • Page 139 IFD5XX Installation Manual NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE. IFD540 #1 SETUP MAIN ARINC 429 CONFIG:...
  • Page 140 IFD5XX Installation Manual AIR DATA Shadin B&D Bendix/King IFD540 COMPUTER ADC 2000 2600 2601 2800 90004-003 KDC 281 KDC 481 P1001 J2 (DB15) J1 (M S CONN) P201 P2811 P4811 GPS ARINC 429 IN 1 A TRANSMITTER A GPS ARINC 429 IN 1 B...
  • Page 141 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE. THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
  • Page 142 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE – THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
  • Page 143 IFD5XX Installation Manual Bendix/King KTA 870/KMH 880 KTA 970/KMH 980 P1001 IFD540 GPS ARINC 429 IN 1 A CDU 429 A TX GPS ARINC 429 IN 1 B CDU 429 B TX ANNUNCIATE D TAS TEST IN ANNUNCIATE E TAS STBY...
  • Page 144 SKYWATCH MUST BE CONFIGURED FOR AN ARINC 735 TYPE 1 DISPLAY. FOR GTX 8XX CONFIGURATION SETTINGS, SEE THE GTX 8XX INSTALLATION MANUAL. IN ORDER FOR AVIDYNE TAS TRAFFIC TO BE DISPLAYED ON THE IFD5XX, A HEADING SOURCE IS REQUIRED. Page 2 of 2...
  • Page 145 AND 1 B, (PINS 37 AND 34) RATHER THAN ARINC 429 OUT 2 A AND 2 B (PINS 30 AND 28) SHOWN. ALTITUDE DATA WILL NOT BE TRANSMITTED OVER ARINC 429 PORT 2 TO THE IFD540 UNIT WHEN EXTERNAL STBY SELECT IS GROUNDED.
  • Page 146 RS-232 INPUT OF THE SAME PORT MAY NOT BE USED. REFER TO SECTION 7.0 FOR RS-232 CHANNEL SETTINGS. CONNECTION TO RS-232 PORT #2 OF THE IFD540 UNIT IS SHOWN. IF PORT #2 IS ALREADY IN USE, ANY OTHER AVAILABLE RS-232 PORT MAY BE USED AS WELL.
  • Page 147 LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL. CONNECTION TO RS-232 PORT #2 OF THE IFD540 UNIT IS SHOWN. IF PORT #2 IS ALREADY IN USE, ANY OTHER AVAILABLE RS-232 PORT MAY BE USED AS WELL.
  • Page 148 PMA 6000 KMA 24H GMA 340 GMA 347 AMX240 PMA 8000(B/BT) KMA 24 KMA 26 KMA 28 SL 1 5 SERIES PMA 7000 -70/-71 IFD540 P1002 BOTTOM J3471 J1 (BOTTOM) BOTTOM P241 P261 J1 (BOTTOM) P241 COM AUDIO HI 9/(10)
  • Page 149 IF THE AUDIO PANEL DOES NOT HAVE A LO INPUT. IT SHOULD BE CONNECTED TO A GROUND LUG AT THE AUDIO PANEL. THE IFD540 INTERCOM FUNCTION SHOULD ONLY BE USED IF THERE IS NO OTHER INTERCOM SYSTEM IN THE AIRCRAFT.
  • Page 150 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. THIS INTERCONNECT APPLIES ONLY WHEN IT IS DESIRED FOR A SEPARATE INDICATOR TO DISPLAY IFD540 VOR/ILS INFORMATION (REGARDLESS OF THE SELECTED NAVIAGATION SOURCE). REFER TO MANUFACTURER’S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION. PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE ONLY.
  • Page 151 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. THIS INTERCONNECT APPLIES ONLY WHEN IT IS DESIRED FOR A SEPARATE INDICATOR TO DISPLAY IFD540 VOR/ILS INFORMATION (REGARDLESS OF THE CDI BUTTON STATUS). REFER TO MANUFACTURER’S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION. PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE ONLY.
  • Page 152 PROPER CONNECTION OF THE RELAY ENGAGE INPUT OF THE KI 209A IS DEPENDENT ON ITS POWER SUPPLY VOLTAGE. REFER TO KI 209A DOCUMENTATION FOR PROPER CONNECTION. IF THE IFD540 IS INSTALLED, AND ANOTHER VOR/ILS RECEIVER IS AVAILABLE TO DRIVE THE NAVIAGATION INDICATOR, AN EXTERNAL SOURCE SELECTION SWITCH MUST BE USED IN LIEU OF THE GPS ANNUNICATE OUTPUT.
  • Page 153 PROPER CONNECTION OF THE RELAY ENGAGE INPUT OF THE KI 208A IS DEPENDENT ON ITS POWER SUPPLY VOLTAGE. REFER TO KI 208A DOCUMENTATION FOR PROPER CONNECTION. IF THE IFD540 IS INSTALLED, AND ANOTHER VOR/ILS RECEIVER IS AVAILABLE TO DRIVE THE NAVIAGATION INDICATOR, AN EXTERNAL SOURCE SELECTION SWITCH MUST BE USED IN LIEU OF THE GPS ANNUNICATE OUTPUT.
  • Page 154 SHOWN FOR REFERENCE ONLY. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE – THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
  • Page 155 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. IF IT IS DESIRED FOR THE RMI POINTER TO SWITCH WITH THE CDI BUTTON ON THE FRONT PANEL OF THE IFD540. INSTALL AS PER THE TOP DIAGRAM. AND SELECT TRACK CDI FOR THE OBI SOURCE FIELD OF THE MAIN CDI/OBS CONFIG PAGE.
  • Page 156 TERMINATE SHIELD GROUNDS TO BACK PLATE – THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL. THE IFD540 MUST BE CONFIGURED AT INSTALLATION TO OUTPUT KING SERIAL DME TUNING DATA UNDER THE DME CHANNEL MODE.
  • Page 157 AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL. THE IFD540 MUST BE CONFIGURED AT INSTALLATION TO OUTPUT KING SERIAL DME TUNING DATA UNDER THE DME CHANNEL MODE. REFER TO MANUFACTURER’S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION. PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE ONLY.
  • Page 158 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. THE IFD540 MUST BE CONFIGURED FOR PARALLEL 2X5 DME CHANNELING MODE FOR PROPER OPERATION WITH THIS MODEL OF DME TRANSCEIVER. THE IFD540 MUST BE CONFIGURED FOR NARCO 890/891 DME CHANNELING MODE FOR PROPER OPERATION WITH THIS MODEL OF DME TRANSCEIVER.
  • Page 159 DME COMMON NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. THE IFD540 MUST BE CONFIGURED TO OUTPUT SLIP CODE DME TUNING DATA FOR PROPER OPERATION IN THIS CONFIGURATION. REFER TO MANUFACTURER’S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION.
  • Page 160 IFD5XX Installation Manual TAWS ANNUNCIATOR GARM IN M ID-CONTINENT PANEL 01 3-0079-XX M D41 -1 0XX IFD540 P1050 TERRAIN NOT AVAIL ANNUNCIATE TERR N/A ANNC IN TERRAIN WARNING ANNUNCIATE TERR PULL UP ANNC IN TERRAIN CAUTION ANNUNCIATE TERR CAUTION ANNC IN...
  • Page 161 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE – THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
  • Page 162 KFC 325 (KC 190) (KC 140) (KC 295) (KC 225) (KCP 320) (KC 19X) (KCP 220) (KCP 299) IFD540 J2TP P1001 MAIN LATERAL +FLAG LAT DEV FLAG + MAIN LATERAL -FLAG LAT DEV FLAG - MAIN +LEFT LAT DEV +LT...
  • Page 163 TO MAIN CDI CENTURY CENTURY CENTURY CENTURY I CENTURY II CENTURY III CENTURY IV CENTURY 21 31/41 2000 TRIDEN IFD540 CD92 CD34 CD34 CD58 CD66 CD194 CD191 CD191 CD191 P1001 MAIN LATERAL +FLAG LAT DEV FLAG + MAIN LATERAL -FLAG...
  • Page 164 LOC SWITCHING INPUT AS SHOWN. SETUP ITEMS, MAIN SYSTEM CONFIG PAGE: GPS SELECT: AUTO INSTALL JUMPER AS REQUIRED TO SET AK 1081 ARINC 429 INPUT SPEED TO MATCH IFD540 OUTPUT SETTING. REFER TO MANUFACTURER’S DOCUMENTATION FOR ADDITIONAL DETAILS. Page 2 of 2...
  • Page 165 System 60- System System Thirty System 40 System 50 System 55 System 55X System 60-1 System 60 PSS Twenty 2/65 IFD540 P1001 0109 0110 0109 0110 MAIN LATERAL +FLAG NAV FLAG + MAIN LATERAL -FLAG NAV FLAG - MAIN +LEFT...
  • Page 166 FOR CONVERTERS 01278-( ) S/N 600A AND ABOVE. INSTALL JUMPER AS REQUIRED TO SET AK 1081 ARINC 429 INPUT SPEED TO MATCH IFD540 OUTPUT SETTING. REFER TO MANUFACTURER’S DOCUMENTATION FOR ADDITIONAL DETAILS. IF THE GPS ANNUNCIATE SIGNAL IS ONLY USED BY THE AUTOPILOT, THIS MAY BE CONNECTED DIRECTLY.
  • Page 167 TO MAIN CDI 65/ 65B/ 65C/ 6 FGC-65( ) APC 65A 5E/ 65F/ 65H/ 65 FYD-65 APC 65G IFD540 P1001 MAIN LATERAL +LT OUT VOR/LOC DEV +LT MAIN LATERAL +RT OUT VOR/LOC DEV +RT MAIN VERTICAL +UP OUT GS DEV +UP...
  • Page 168 IFD5XX Installation Manual ARINC 429 Bendix/King FLIGHT CONTROL KFC 400 SYSTEM KCP420 IFD540 #1 P1001 P4201 P4202 GPS ARINC 429 OUT A LNAV 1 RECEIVER A LNAV 1 RECEIVER B GPS ARINC 429 OUT B NAV SYSTEM 1 GPS ARINC 429 IN 1A...
  • Page 169 IFD5XX Installation Manual STACO INDICATOR CONNECTION STACO INDICATOR IFD540 P1001 VLOC VLOC ANNUNCIATE LAMP VOLTAGE FROM DIMMER CIRCUIT GPS ANNUNCIATE VIVISUN INDICATOR CONNECTION VIVISUN INDICATOR IFD540 P1001 VLOC VLOC ANNUNCIATE LAMP VOLTAGE FROM DIMMER CIRCUIT GPS ANNUNCIATE VIVISUN INDICATOR/SWITCH CONNECTION...
  • Page 170 THESE UNITS ALSO PROVIDE NAVIGATION SOURCE SELECTION ANNUNCIATION. MID- CONTINENT ANNUNCIATION CONTROL UNITS FOR BOTH 14V AND 28V SYSTEMS SHOWN. THIS DIAGRAM IS PROVIDED TO SHOW INTERCONNECTION BETWEEN IFD540 AND ACU ONLY. REFER TO MID-CONTINENT INSTALLATION MANUAL FOR ADDITIONAL INSTALLATION INFORMATION.
  • Page 171 IFD5XX Installation Manual IFD540 P1001 TIME MARK OUT REMOTE CDI SWITCH (OPTIONAL) CDI SOURCE SELECT REMOTE OBS MODE SWITCH (OPTIONAL) OBS MODE SELECT REMOTE COM RECALL SWITCH (OPTIONAL) COM REMOTE RECALL NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED.
  • Page 172 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE – THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
  • Page 173 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE – THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
  • Page 174 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE. WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED.
  • Page 175 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE. WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED.
  • Page 176 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT IFD540 UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE. WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED.
  • Page 177 IFD5XX Installation Manual IFD540 TRANSPONDER AVIDYNE Trigg Avionics AXP340 TT31 P1001 Primary Primary WEIGHT ON WHEELS SQUAT SWITCH IN NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED.
  • Page 178 IFD5XX Installation Manual IFD540 P1001 RS232 OUTPUT 2 GPS RS232 INPUT NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED. REFER TO MANUFACTURER’S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION.

  • Page 179: Appendix E: Troubleshooting Guide

    IFD5XX Installation Manual Appendix E: Troubleshooting Guide Component Trouble Probable Cause Solution IFD5XX The unit is not getting power to The unit is not getting power. Check Circuit Breaker the main connector Check wiring and unit seating in tray The IFD5XX is not computing a Wiring Check Coaxial Cables position...
  • Page 180 IFDs "Config Mismatch" CAS message Configuration mismatch Power cycle the IFD5XX units on IFD5XX (dual IFD5XX only) between the two IFD540 units Verify configuration on IFD5XX units If problem persists, send IFD5XX log data to Avidyne Technical...

  • Page 181: Appendix F: Configuration Setup

    IFD5XX Installation Manual Appendix F: Configuration Setup In order to support the requirements of some validations of the AML STC, this section should be easily removable and inserted into the aircraft logs. For those installations where an IFD5XX is replacing a GNS-530/W, please record the following parameters from the GNS-530/W setup pages before removing the unit (Note: this will need to be conducted for each GNS-530/W being replaced): WAAS Enabled (530W with approved antenna)? Yes...
  • Page 182 IFD5XX Installation Manual Please list the other avionics that are installed in the aircraft (please be as specific as possible with make and models of the gear) and connected to the GNS-530/W. Enter “None” or “Don’t Know” as required. The GNS-530/W Setup pages will be captured on subsequent pages.
  • Page 183 IFD5XX Installation Manual Transponder Air Data IRU/INS Other Other Other GNS-530/W Maintenance Mode Entry: GNS-530 configuration data is accessed from the GNS-530/W Maintenance Mode settings which is entered via holding ENTR button on 530/W bezel during power application. GNS-530/W Page Navigation: Use the inner right knob on the GNS-530/W to scroll through the maintenance mode pages.
  • Page 184 IFD5XX Installation Manual Garmin 530/W - MAIN ARINC 429 CONFIG IFD5XX - Main ARINC 429 Config Page (1/10) page Speed Data Speed Data In 1 IN 1 In 2 IN 2 VNAV VNAV (if present) For new IFD5XX installations, see Section 7.4.2 for selections and descriptions IFD5XX - Main RS232 Config Page (2/10) Input...
  • Page 185 IFD5XX Installation Manual GNS-530/W – MAIN SYSTEM CONFIG Page (Fuel) CONFIGURE Fuel FUEL TYPE GNS-530/W – MAIN SYSTEM CONFIG Page (Terrain) [if present] CONFIGURE Terrain TERRAIN TYPE TEST CARD? HW CONFIG 012-00296- 012-00401- GNS-530/W – MAIN SYSTEM CONFIG Page (Discretes) [if present] CONFIGURE Discretes GPS SELECT...
  • Page 186 IFD5XX Installation Manual IFD5XX – Main System Config page (3/10) Fuel Type GPS Select Airframe Tail Number External TAWS Tail Number is a free text field and is used for JSUM. 600-00299-000 Page 186 of 198 Revision: 02...
  • Page 187 IFD5XX Installation Manual IFD5XX – MAIN INPUTS Page (4/10) GNS-530/W – MAIN INPUTS Page W DIR L FF L FF R FF R FF W SPD T FF W SPD T FF JOYSTICK JOYSTICK Note: There is no data to enter on the IFD5XX from this page –...
  • Page 188 IFD5XX Installation Manual IFD5XX – MAIN LIGHTING Page (5/10) GNS-530/W – MAIN LIGHTING Page Bezel Display Display Photo LIGHTING Response Time SOURCE Photo RESP TIME Slope / MIN Photo SLOPE / Minimum OFFSET Photo PHOTO Maximum TRANS % dimBus Transition applicable) PHOTO dimBus...
  • Page 189 IFD5XX Installation Manual GNS-530/W – DATE / TIME SETUP Page (No Need to Fill In – For Reference Only) UTC DATE UTC TIME No IFD5XX Equivalent Page GNS-530/W – MAIN DISCRETE I/O Page GRAY DECODED CODE ALTITUDE EXTERNAL SWITCH STATE No IFD5XX Equivalent Page RMT CDI DISCRETE...
  • Page 190 IFD5XX Installation Manual IFD5XX – MAIN CDI / OBS CONFIG Page (6/10) GNS-530/W – MAIN CDI / OBS CONFIG Page FLAG FROM FLAG FROM VERT SELECTED COURSE VERT Ignore SELECTED COURSE SEL CRS for GPS SOURCE FLAG Ignore STATE SEL CRS VLOC SOURCE FLAG...
  • Page 191 IFD5XX Installation Manual IFD5XX – VOR/LOC/GS CDI Page (7/10) GNS-530/W – VOR/LOC/GS CDI Page FLAG FLAG FROM FLAG FLAG FROM VERT VERT SELECTED SELECTED COURSE COURSE CHANNEL CHANNEL MODE MODE GNS-530W Only For new IFD5XX installations, see Section 7.4.7 for selections and descriptions.
  • Page 192 IFD5XX Installation Manual GNS-530/W – Stormscope Config Page (if configured for Stormscope) STATUS: MODE: SW VERSION: ANT MOUNT: HDG FORMAT HDG FLG SENSE HDG FLAG SYNC ANGLE No IFD5XX Equivalent Page HDG STAB SYNC REF HDG VALID Note: Squares should all be green if no issues.
  • Page 193 IFD5XX Installation Manual GNS-530/W – STORMSCOPE DATA DOWNLOAD Page (if configured for Stormscope) SOFTWARE VERSIONs: No IFD5XX Equivalent Page GNS-530/W – Traffic Config Page (if configured for Traffic) LIM A (if 429 interface) No IFD5XX Equivalent Page LIM B (if 429 interface) Note: Traffic test is accomplished after a HDG (if 429...
  • Page 194 IFD5XX Installation Manual GNS-530/W – RYAN TCAD CONFIG Page (if configured for Ryan TCAD] MODE APPROACH MODE HEIGHT RANGE GND/FLD No IFD5XX Equivalent Page ELEVATION Note: Use the presence of the traffic VOLUME thumbnail and the Audio Volume Control page to control these MUTE parameters in the IFD5XX.
  • Page 195 IFD5XX Installation Manual GNS-530/W – TAWS Audio Config Page 1 (if installed) No IFD5XX Equivalent Page TAWS CONFIG (Use the User Options LSK and Volume Control LSK of the Audio Tab instead) VOICE GENDER VOLUME PLAY AUDIO GNS-530/W – TAWS Audio Config Page 2 (if installed) ALERT Reduced Terrain Clearance...
  • Page 196 IFD5XX Installation Manual GNS-530/W – GDL Config Page (if installed) IFD5XX – GDL Config Page (if installed) (10/10) ATTENUATION ATTENUATION MODEL (if displayed) MODEL GNS-530/W – DATALINK DIAGNOSTICS Page (if installed) TERR No IFD5XX Equivalent Page SAT 1 SAT 2 Note: Use the Datalink Status page on the AUX-SYS tab for datalink status data.
  • Page 197 Notice: WARRANTY: AVIDYNE WARRANTS THE PRODUCT MANUFACTURED BY IT AGAINST DEFECTS IN MATERIAL AND WORKMANSHIP FOR A PERIOD OF TWELVE (12) MONTHS FROM DELIVERY TO THE INSTALLER. A COMPLETE COPY OF THE WARRANTY DATA IS ACCESSIBLE VIA THIS WEB ADDRESS: HTTP://WWW.AVIDYNE.COM/SUPPORT/WARRANTY.ASP...
  • Page 198 ® 600-00299-000 © Copyright 2014 Avidyne Corporation Rev: 02...

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