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Avidyne IFD540, Installation Manual

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Avidyne IFD540 Installation Manual Download Page 117

 

IFD5XX Installation Manual 

600-00299-000 

Page 117 of 198 

Revision: 02 

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10.3  Software Update 

The following procedures should be followed when performing optional or mandatory 
software change to the IFD System: 

1.

 

Acquire the software image and associated loading procedure 
from the manufacturer. 

2.

 

Verify the software part number configuration before and after 
maintenance is performed on the airborne equipment using the 
loading procedure instructions. 

3.

 

It is the responsibility of maintenance personnel to ensure the 
identified part is recorded in the necessary maintenance logs.  

4.

 

It is the maintenance personnel’s responsibility to ensure that the 
software part identification has been logged.  When new 
software is loaded into the unit, the correct software part 
number should be verified according to the instructions 
accompanying the software change before the unit is returned to 
service.  Hardware versions are identified on the data label by 
brackets following the main part number. 

Changes to software part number, version, and/or operational characteristics should be 
reflected in the Operator’s Manual, Aircraft Flight Manual, Aircraft Flight Manual 
Supplement, and/or any other appropriate document. 

Summary of Contents for IFD540

Page 1: ......

Page 2: ...ges 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 Avidyne is a registered trademark of Avidyne Corporation Document Number 600 00299 000 Control Category CC2 Revision Description ECO Date 00 Initial Release ECO 14 207 07 09 14 01 Release 10 0 1 0 ECO 14 283 08 21 1...

Page 3: ... Navigation Specification 15 1 4 Power Requirements 15 1 5 Regulatory Compliance 15 1 5 1 Applicable TSOs 15 1 5 2 TSO Deviations 17 1 5 3 Non TSO Functions 19 1 5 4 Partial TSO Functions 20 1 5 5 Open Problem Report 20 1 6 Software and Hardware Design Assurance Levels 21 1 7 Environmental Qualification Forms 22 1 8 Databases 22 1 9 Fault Detection and Exclusion FDE 22 1 10 STC Approved Model List...

Page 4: ... Antenna Bonding 38 3 2 Antenna Environmental Qualifications 38 3 3 GPS Antenna 38 3 3 1 GPS Location 39 3 3 2 GPS Antenna Bonding 41 3 3 3 GPS Antenna Cable 41 3 3 4 GPS Coaxial Cable Connector 42 3 3 5 Approved GPS Antennas 42 3 3 6 GPS Interference 43 3 3 7 Ground Plane 43 3 3 8 Dual IFD5XX Installations 43 3 3 9 Anti Ice Protection 43 3 4 VHF Communication Antenna 43 3 4 1 Antenna Environmenta...

Page 5: ...ation 45 4 3 Wire Routing 45 4 4 Shield Grounds 45 4 5 Wire Harness Overbraid 45 4 5 1 Existing Equipment 45 4 5 2 Severe Lightning Transient Environment 45 4 5 3 Copper Overbraid Installation 46 4 6 IFD5XX Connectors 46 4 7 Byteflight Digital Data Bus Consideration Dual IFD Installations 46 4 7 1 Databus Wiring Replacement Installations 46 4 7 2 Databus Wiring New Installations 47 4 8 Circuit Pro...

Page 6: ... 5 6 Electrical Bonding 54 5 7 Aircraft Considerations 54 5 8 Weight and Balance 55 5 9 Compass Safe Distance 55 6 System Installation 56 6 1 Pin Function List 56 6 1 1 P1001 Main Connector 56 6 1 2 P1002 Communication Connector 58 6 1 3 P1006 Navigation Connector 59 6 1 4 P1050 Additional I O Connector 60 6 1 5 Altitude Gray Code 61 6 1 6 Main Course Deviation Indicator Output 62 6 1 7 Serial Dat...

Page 7: ...6 12 ADS B Transponder Output 75 6 13 Autopilot 76 6 14 TAWS EGPWS Output 76 7 Configuration and Checkout 77 7 1 Wiring Check 77 7 2 Mounting Check 77 7 3 Chassis ID Setting 77 7 4 Unit Installation 78 7 5 Configuration 78 7 5 1 Maintenance Mode 78 7 5 2 ARINC 429 Port Configuration Page 1 of 10 79 7 5 3 RS 232 Port Configuration Page 2 of 10 84 7 5 4 Main System Configuration Page 3 of 10 87 7 5 ...

Page 8: ...pplement Check 104 7 6 3 Instructions for Continued Airworthiness 104 7 6 4 Aircraft Weight and Balance 104 7 6 5 Electrical Load Analysis 105 7 6 6 GPS Signal Acquisition 105 7 6 7 VHF COM Checkout 105 7 6 8 VOR LOC GS Checkout 106 7 6 9 Autopilot 106 7 6 10 Magnetic Compass Swing 106 7 6 11 IFD5XX Bezel and Display Lighting 106 7 6 12 External Annunciators and Switches 106 7 6 13 Placards 106 7 ...

Page 9: ...e 117 11 Periodic Maintenance 118 11 1 Equipment Calibration 118 11 2 VOR Checks 118 11 3 Cleaning 118 12 Factory Service Policies and Procedures 119 12 1 Technical Support 119 12 2 General Service Procedures 119 13 Bezel and Display Cleaning 120 Appendix A Environmental Qualification Form 121 Appendix B STC Permission 122 Appendix C Mechanical Drawings 123 Appendix D Electrical Interface Drawings...

Page 10: ...th a certification basis of Amendment 23 45 or later unless approved installation data is listed in the Master Document List of the STC All early amendment metal construction non pressurized aircraft antenna installations must be installed consistent with accepted industry practices The installation must be structurally sound and in accordance with FAA Advisory Circular 43 13 1B and 43 13 2B All o...

Page 11: ...000 ACR 530 00225 000 Rev 02 510 00286 000 Rev 02 510 00287 000 Rev 01 510 00310 000 Rev 00 510 00311 000 Rev 00 510 00312 000 Rev 00 FPSM 530 00226 000 Rev 00 510 00294 000 Rev 00 510 00291 000 Rev 00 LIO App 530 00227 000 Rev 00 510 00293 000 Rev 00 510 00292 000 Rev 00 LIO I O 530 00228 000 Rev 00 510 00288 000 Rev 00 510 00289 000 Rev 00 510 00290 000 Rev 00 510 00291 000 Rev 00 GPS 530 00229 ...

Page 12: ...h Density D Subminiature male P1002 25 position Standard D Subminiature female P1006 44 position High Density D Subminiature male Electrical Requirements Voltage 9 33 VDC Current 4 4A main 6 5A COM 0 25A NAV at 14VDC 2 2A main 4A COM 0 50A NAV at 28VDC Dimming Bus 28VDC 14VDC 5VDC 5VAC Cooling Requirements Not Required Operating Limits Reference Appendix A Environmental Qualification Form Table 2 ...

Page 13: ...ccuracy 3 4 meters Fault Detection RAIM RAIM FDE WAAS Beta 3 Compliant 5 Hz Sensitivity 123 dBm GPS System Design Assurance SDA DO 178B Level B DO 254 Level B GPS Source Integrity Level SIL 3 Enroute Source Integrity Level Supplement SILSUPP 0 per hour Navigation Accuracy Category Velocity NACV Category 3 ADS B installations should use a NACv of 1 unless GPS tests support a higher category Receive...

Page 14: ...dB S N N 30 mod 1KHz Spurious Response 10mV spurious signal produces no more output than a desired signal at 6dB S N N Transmitter Power 16W 28V 10W 14V Typical Transmitter Duty Cycle Recommended 10 maximum Modulation Capability 70 Carrier Noise Level 39dB S N N Frequency Stability 2 5 ppm Demodulation Audio Distortion 12 70 modulation Sidetone Fidelity 300 2500 Hz Demodulation Audio Response 6dB ...

Page 15: ...able 6 VHF Navigation Specification 1 4 Power Requirements The IFD5XX is capable of operating from 9 33 VDC The following table shows the typical current requirements for 14VDC and 28VDC aircraft electrical systems Voltage 14VDC 28VDC Main Power 4 4A 2 2A COM Power 6 5A 4 0A NAV Power 0 25A 0 50A Table 7 Power Requirements 1 5 Regulatory Compliance 1 5 1 Applicable TSOs This section identifies Tec...

Page 16: ... Receiving Equipment Operating within the Radio Frequency Range of 108 117 95 Megahertz MHz TSO C44c Fuel Flowmeters TSO C110a Airborne Passive Thunderstorm Detection Equipment TSO C113a Airborne Multipurpose Electronic Display TSO C118 Traffic Alert and Collision Avoidance System TCAS Airborne Equipment TCAS I TSO C128a Devices that Prevent Blocked Channels Used in Two Way Radio Communications Du...

Page 17: ... TSO Deviation s TSO C34e ILS Glideslope Receiving Equipment 1 Environmental qualification performed in accordance with DO 160G rather than DO 160B TSO C36e Airborne ILS Localizer Receiving Equipment 1 Environmental qualification performed in accordance with DO 160G rather than DO 160B TSO C40c VOR Receiving Equipment 1 Environmental qualification performed in accordance with DO 160G rather than D...

Page 18: ...dio Technical Commission for Aeronautics RTCA Document No RTCA DO 197A Minimum Operational Performance Standards for An Active Traffic Alert and Collision Avoidance System I Active TCAS 1 Section Two 2 September 12 1994 with the exceptions listed in appendix 1 of TSO 147 in lieu of the corresponding minimum operational performance standards specified in the TSO TSO C128a Equipment that Prevents Bl...

Page 19: ...ce with DO 160G rather than DO 160B 2 De cluttering on chart page not provided 3 Location of traffic symbols in the absence of heading information TSO C169a VHF Radio Communications Transceiver Equipment 1 Environmental qualification performed in accordance with DO 160G rather than DO 160B Table 9 IFD5XX TSO Deviations Table 9 above lists the TSO Deviations and a brief description of the nature of...

Page 20: ...play Only TSO C118 Traffic Alert and Collision Avoidance System TCAS Airborne Equipment TCAS I Display Only TSO C147 Traffic Advisory System TAS Airborne Equipment Display Only TSO C157a Aircraft Flight Information Services Broadcast FIS B Datalink Systems and Equipment Display Only Table 10 Partial Function TSOs 1 5 5 Open Problem Report At the time of this revision the IFD5XX does not have any o...

Page 21: ...tions of the IFD5XX system and their corresponding software design assurance level All complex electronic hardware devices were developed in compliance with DO 254 Level B Component Function DO 178B Design Assurance Level IFD5XX Traffic D Lightning D Digital Moving Map not including Terrain C Terrain Alerting C Wx Datalink D FMS B VHF Communication C VHF Navigation C GPS Navigation B Checklist C F...

Page 22: ...D5XX is installed per the directions in this Installation Manual it complies with the governing requirements for GPS Primary Means of Navigation in Oceanic and Remote Airspace more than 200 nm from the nearest airport when used with any commercially available RAIM FDE Prediction Program Examples of these prediction programs include the FAA s raimprediction net Fltplan com www sapt faa gov and the ...

Page 23: ...via field approval the Avidyne Helicopter tray must be used reference Table 13 The installation of antennas on composite and or pressurized aircraft requires engineering guidance beyond the scope of this manual With respect to the Approved Model List STC the physical mounting of the antenna is specifically excluded from the approval in the case of installation on the pressure vessel of a pressuriz...

Page 24: ...Kit 850 00182 000 Black Bezel Ship Kit 850 00183 100 Grey Bezel IFD5XX Unit 700 00182 000 700 00182 100 USB Flash Drive X X Table 12 IFD5XX Ship Kit 1 11 2 Optional Ship Kits Component Fixed Wing Aircraft Ship Kits Helicopter Ship Kit IFD5XX Tray 850 00188 000 850 00188 001 IFD5XX Components Only no tray 820 00113 000 820 00113 000 IFD5XX Tray and Install Kit 850 00188 002 850 00188 003 Table 13 I...

Page 25: ...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 Coaxial Cables Wire Splices Solder Sleeves Antenna s Diplexers ...

Page 26: ...unctionality and TOD chime to the headsets If the unit being replaced was a TAWS enabled device used for 91 135 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 ...

Page 27: ... button to select frequencies in the com preset list to be loaded into the 1 Standby com slot Section 6 1 9 4 Com Frequency Active Standby Swap Enables external command e g yoke mounted button to swap the Active and 1 Standby com frequencies Section 6 1 9 4 Nav Frequency Active Standby Swap Enables external command e g yoke mounted button to swap the Active and 1 Standby nav frequencies Section 6 ...

Page 28: ... Altimeter or Blind Encoders Bendix King KEA 130A Bendix King 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 Garmin MX20 Garmin GMX200 Garmin GPSMAP 195 Gar...

Page 29: ...ndix King KAH 460 Inertial System KAU 461 also Collins AHC 85 Inertial System Laseref Honeywell HG 1075AB HG 1095AG Inertial Systems Litef LTR 81 Inertial System Litton LTN 90 100 Inertial System Litton LTN 91 Inertial System Litton LTN 92 Inertial System EHSI Sandel SN3308 Sandel SN3500 Fuel Shadin 91053XP Digital Fuel Mgmt System Shadin 91204XM Digital Fuel Mgmt System Shadin 91802 X Fuel Airdat...

Page 30: ...n 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 Lightning L3 WX500 Avidyne TWX670 Datalink Garmin GDL 69 69A Avidyne MLB700 WSI AV 300 350 Autopilot Bendix King KFC400 Bendix King KCP320 Bendix King KFC325 Bendix King KFC300 Bendix King KFC225 Bendix King KFC200 Bendix Kin...

Page 31: ...ury 21 Century 31 41 Century 2000 Century Triden Century AK 1081 GPSS Converter Collins APC 65 Series Collins FGC 65 Collins FYD 65 STec 20 STec 30 STec 40 STec 50 STec 55 STec 55X STec 60 PSS STec 60 1 STec 60 2 STec 65 STec ST901 GPSS Converter Miscellaneous Garmin GAD42 Interface Adapter EGPWS Bendix King KGP560 DME Bendix King KN 61 Bendix King KN 62 62A Bendix King KN 63 Bendix King KN 64 ...

Page 32: ...RC Cessna RTA 476A Nav Indicator Garmin GI 102 A Garmin GI 106 A Bendix King KI 202 Bendix King KI 203 Bendix King KI 204 Bendix King KI 206 Bendix King KI 208 Bendix King KI 208A Bendix King KI 209 Bendix King KI 209A Bendix King KI 525A Bendix King KPI 552 B Bendix King KPI 553 A B Century NSD 360A Century NSD 1000 Collins 331A 6P Collins 331A 9G Collins PN 101 Mid Continent MD 222 402 406 Mid C...

Page 33: ...rmin 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 PS Engineering 8000 8000BT Bendix King KMA 24 Bendix King KMA 26 Bendix King KMA 28 Bendix King KMA 24H 406 ELT Artex ME406 Ameri King AD 451 Ack E 04 Narco Not specified Pointer 3000 Kannad Not specified Table 17 IFD5XX Com...

Page 34: ...D5XX unit GPS Antenna TSO C190 or approved antennas listed in Section 3 3 5 VHF Communication Antenna is needed for communication functions Navigation Antenna s is needed for VOR LOC GS functions Remote Annunciator is required if the IFD5XX is not in the field of view of the pilot reference Section 5 1 2 IFD5XX should be interfaced to an Airdata source for automatic altitude leg sequencing optiona...

Page 35: ... to the aircraft 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 VOR LOC ILS instrument approach procedures procedures using VHF radio guidance RNP instrument approach procedures using the following...

Page 36: ...FD5XX GPS Nav Comm Autopilot Datalink WSI XM etc Lightning Detection Traffic System Transponder Fuel Management System Audio Panel CDI HSI DME EFIS MFD Switches Annunciators NAV Antenna Com Antenna GS Antenna GPS Antenna CrossSync to 2nd IFD ELT EGPWS Encoding Altimeter Figure 1 Full IFR Installation ...

Page 37: ... Antenna Installed Section 3 5 Communication Antenna Installed Section 3 4 Is the IFD5XX or remote annunciator lights installed within the Pilot s Field of View Section 5 1 or 5 2 Does the aircraft have an approved GPS antenna installed on the aircraft Or can the GPS antenna be installed per this manual Section 3 3 5 Does the aircraft have a previously approved Marker Beacon System installed in th...

Page 38: ...and AC 43 13 1B Chapter 4 Also reference Appendix C in this manual The GPS antenna listed in Table 14 can be installed on unpressurized metal airplanes with a certification basis of Amendment 23 43 or earlier using the data below All other GPS Antenna installations are beyond the scope of this manual and a separate installation approval is required The Avidyne GPS antenna Avidyne Part Number 200 0...

Page 39: ...ll MS20470AD rivets in the outer row of the doubler If the adjacent rivets are countersunk or dimpled install either MS20426AD or NAS1097AD rivets per the table below Reference Table 93 for rivet type and doubler thickness appropriate for the aircraft s skin thickness Fuselage Thickness Doubler Thickness Doubler Drawing 0 016 0 025 0 020 See Figure C 37 0 032 0 050 0 032 Table 19 Doubler Thickness...

Page 40: ...A and RTCA DO 160G The No Installation Area can be determined using Figure 2 The distance found by using Figure 2 defines a zone immediately aft of the nose of the aircraft or propeller in the case of single engine propeller driven aircraft where the GPS antenna should not be installed Aircraft locations aft of the No Installation Area are acceptable to install the GPS antenna Figure 3 below shows...

Page 41: ...PS Antenna Bonding The GPS Antenna should have 2 5 milliohm resistance to the aircraft fuselage 3 3 3 GPS Antenna Cable The GPS Antenna Cable must be RG 142B RG 400 or an equivalent 50 double shielded coaxial cable The GPS antenna cable loss should not be greater than 6 5dB or less than 1 5 dB Each connector on the GPS coaxial cable will add an additional 0 2 dB loss to the cable The GPS antenna c...

Page 42: ...proved for any type of WAAS operations In this case the Antenna Type selection as described in Section 7 5 10 must be selected as Non WAAS This will result in the FMS functionality of the IFD5XX inhibiting selection of any WAAS SBAS approach in the database Installing an antenna listed in Table 20 requires additional installation approval Model Number Description Supplier CI 428 200 GPS WAAS Anten...

Page 43: ...nti Ice Protection If the aircraft is approved for flight into known icing verify the GPS antenna is installed in location that is not susceptible to ice buildup or complies with FAA AC 20 138 paragraph 13 2 3 4 VHF Communication Antenna The VHF communication antenna should be installed using this manual FAA AC 43 13 AC 20 67B and the antenna manufacturer s guidance The antennas should be installe...

Page 44: ... the connector manufacturer s assembly instructions 3 5 4 Diplexer The IFD5XX requires separate Glideslope and Navigation antenna inputs A diplexer will be required if a single navigation coax delivers both VHF navigation and Glideslope navigation signals to the IFD5XX location such as if a combined Nav Glideslope antenna is used or a Nav Glideslope diplexer is installed to combine signals at the ...

Page 45: ... between redundant systems to prevent loss of navigation due to a single event 4 4 Shield Grounds 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 install...

Page 46: ...M81969 1 02 P1006 M24308 4 266 M39029 58 360 ORG BLU BLK M22520 02 01 M22520 2 09 M81969 1 04 M81969 1 04 P1050 M24308 4 268 M39029 58 360 ORG BLU BLK M22520 02 01 M22520 2 09 M81969 1 04 M81969 1 04 Ground Block 583861 7 TE Connectivity 5 583853 4 TE Connectivity 91535 1 TE Connectivity 91073 1 TE Connectivity Table 21 D Sub Connector Tools 4 7 Byteflight Digital Data Bus Consideration Dual IFD I...

Page 47: ...nstalled in a location easily accessible to the pilot and must be resettable trip free devices The Circuit Breaker must be clearly identified and visible under all lighting conditions Circuit breaker size is identified in installation data shown in Appendix D Electrical Interface Drawings Note that 14v aircraft may be required to replace the installed circuit breaker and power wiring to accommodat...

Page 48: ...XX as shown in Figure 6 Avionics Bus 1 Avionics Bus 2 IFD540 COM IFD540 COM Aircraft Ground Aircraft Ground IFD540 COM IFD540 COM Aircraft Ground Aircraft Ground Preferred Alternate Avionics Bus Main Bus Figure 6 Dual IFD5XX Power Distribution Aircraft 6000 lbs If installing a 3rd party NAV and or COM and IFD5XX connect the IFD5XX as shown in Figure 7 Avionics Bus 2 Other COM NAV Aircraft Ground A...

Page 49: ... on performing an aircraft electrical load analysis The purpose of the ELA is to show compliance to 14 CFR 23 1351 and 23 1353 h 4 11 Low Power Behaviors The IFD5XX can accept input power ranging from 9VDC to 33VDC but has the following low power behaviors Input Voltage Level Behavior 18VDC High power USB charging dedicated charging port drawing 2 1A 18VDC USB port drops from High power USB chargi...

Page 50: ...ts must have this annunciation at each pilot station or unobstructed view of the IFD5XX display The IFD5XX should be located in a position easily reached by both pilots 5 1 1 Determining the Field of View The navigation source selection field of view is approximately 30 or 13 856 horizontally from the center of the attitude indicator or centerline of the pilot s seat yoke The navigation annunciati...

Page 51: ...is 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 as shown in Figure 8 external annunciation is not needed Install external annunciation lights in the acceptable field of view ...

Page 52: ...e 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 The annunciators must be able to be tested prior to flight The field of view in Figure 8 is based on 35 from the Instrument T centerline at 24 aft of the pa...

Page 53: ...1 Rear Tray Support Instrument Panel a The existing instrument panel must be fabricated from 2024 T3 aluminum with a minimum thickness of 0 050 The tray brackets must be fabricated from 3 4 x 3 4 x 1 16 2024 T3 aluminum angle extrusion for mounting the tray as shown in Figure C 33 b If new components are fabricated the fabrication methods must follow the requirements of FAA Advisory Circular 43 13...

Page 54: ...near other hot equipment In the event the system feels excessively hot or if an Overtemp Caution Advisory System message is presented on the display there are some diagnostic tools provided in the IFD5XX to assist in finding more optimal cooling installations In Maintenance Mode select the Status tab along to bottom edge of the display and then press the Info Line Select Key as needed until Temps ...

Page 55: ...3 13 1B Change 1 Acceptable Methods Techniques and Practices Aircraft Inspection and Repair Chapter 10 and AC 120 27E Aircraft Weight and Balance Control 5 9 Compass Safe Distance The IFD5XX should be installed 12 or more away from the aircraft s magnetic compass Perform an aircraft compass swing calibration after completing the IFD5XX installation Note The 12 minimum distance is a TSO driven valu...

Page 56: ... 3 Waypoint Annunciate Output 4 Terminal Annunciate Output 5 Approach Annunciate Output 6 Message Annunciate Output 7 OBS Annunciate Output 8 Weight on Wheels WOW Output 9 Integrity Annunciate Output 10 Annunciate D Output 11 Annunciate E Output 12 Reserved Output 13 GPS Select Output 14 ILS GPS Annunciate Approach Output 15 Aircraft Power 2 Input 16 Time Mark Out Output 17 Main Lateral Superflag ...

Page 57: ...r F Input 36 Main OBS Stator G 2 5V Common OBS Output 37 Audio 1 HI Alert audio Output 38 Audio 1 LO Alert audio Output 39 LTG Bus HI Input 40 LTG Bus LO GND Input 41 GPS RS232 Out 3 Output 42 GPS RS232 In 3 Input 43 Main OBI Clock Output 44 Main OBI Data Output 45 Main OBI Sync Output 46 GPS Arinc 429 Out A Output 47 GPS Arinc 429 Out B Output 48 GPS Arinc 429 In 1 A Input 49 GPS Arinc 429 In 1 B...

Page 58: ...Altitude A2 Input 69 Altitude A1 Input 70 Altitude D4 Input 71 OBS Mode Select Input 72 Aircraft Power 2 Input 73 CDI Source Select Input 74 COM Remote Recall Input 75 Reserved 76 LTG BUS 2 HI Input 77 Aircraft GND 78 Aircraft GND Table 24 P1001 Pin Description 6 1 2 P1002 Communication Connector Pins Description Signal Type 1 Reserved 2 Ethernet 1 TX Output 3 Ethernet 1 TX Output 4 COM Microphone...

Page 59: ... in as of Release 10 1 0 0 25 Reserved Synchro Reference Signal as of Release 10 1 0 0 Table 25 P1002 Pin Description 6 1 3 P1006 Navigation Connector Pins Description Signal 1 VOR LOC To Output 2 VOR LOC From VOR LOC 2 5V Common Output 3 VOR LOC Flag Output 4 VOR LOC Flag VOR LOC 2 5V Common Output 5 VOR LOC Left Output 6 VOR LOC Right VOR LOC 2 5V Common Output 7 Com Monitor Audio HI Output 8 VO...

Page 60: ...utput 34 Com Monitor Audio LO Output 35 VOR ILS Arinc 429 In B Input 36 VOR ILS Arinc 429 In A Input 37 Parallel DME 800KHz Output 38 Glideslope Superflag Output 39 Parallel DME 400KHz Output 40 Parallel DME 200KHz Output 41 Aircraft GND 42 Nav Par DME 100KHz Output 43 Nav Par DME 50KHz Output 44 Aircraft Power Input Table 26 P1006 Pin Description 6 1 4 P1050 Additional I O Connector Pins Descript...

Page 61: ...g pins Description Connector Pin Signal Type Altitude D4 P1001 70 Input Altitude A1 P1001 69 Input Altitude A2 P1001 68 Input Altitude A4 P1001 67 Input Altitude B1 P1001 66 Input Altitude B2 P1001 65 Input Altitude B4 P1001 64 Input Altitude C1 P1001 63 Input Altitude C2 P1001 62 Input Altitude C4 P1001 61 Input Altitude Common P1001 60 Input Table 28 Altitude Gray Code Description NOTE Some tran...

Page 62: ...1001 22 Output Main Up P1001 27 Output Main Down P1001 28 Output Table 29 Main Course Deviation Output 6 1 6 2 TO FROM Indication Flag The To From Flag indication flags are on the following connector and pins Description Connector Pin Signal Type Main To P1001 25 Output Main From P1001 26 Output Table 30 Main TO From Flag Output 6 1 6 3 Navigation Flags The Navigation Flags is on the following con...

Page 63: ...gation 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 6 1 6 5 OBS The OBS is on the following connector and pins Description Connector Pin Signal Type Main OBS Rotor C P1001 31 Output Main OBS Rotor Ground P1001 32 Output Main OBS Stator D P1001 33 Input Main OBS Stator E P1001 34 Output Ma...

Page 64: ...1001 13 Output ILS GPS Approach P1001 14 Output Table 34 Annunciator Output All inputs sink up to 500 mA when activated 6 1 6 7 Switch Inputs Description Connector Pin Signal Type OBS Mode Select P1001 71 Input CDI Source Select P1001 73 Input Table 35 Switch Inputs The inputs are considered active if voltage to ground 1 9V or resistance to ground 375 These inputs are considered inactive if voltag...

Page 65: ...t 5 P1050 60 Output RS 232 Input 5 P1050 61 Input RS 232 Output 6 P1050 62 Output RS 232 Input 6 P1050 63 Input Table 37 RS 232 Input Output 6 1 8 ARINC 429 Description Connector Pin Signal Type GPS ARINC 429 OUT A P1001 46 Output GPS ARINC 429 OUT B P1001 47 Output GPS ARINC 429 IN 1 A P1001 48 Input GPS ARINC 429 IN 1 B P1001 49 Input GPS ARINC 429 IN 2 A P1001 50 Input GPS ARINC 429 IN 2 B P100...

Page 66: ...iption Connector Pin Signal Type COM MIC Audio HI P1002 6 Input COM MIC Audio LO P1002 18 Input INTERCOM MIC HI P1002 5 Input INTERCOM MIC LO P1002 17 Input Table 40 VHF Communication Audio 520 input impedance supply 9V via 620 6 1 9 3 Com Audio VOR ILS Audio Description Connector Pin Signal Type Com Audio HI P1002 7 Output Com Audio LO P1002 19 Output VOR ILS Audio HI P1006 16 Output VOR ILS Audi...

Page 67: ...6 15 Output Glideslope Superflag P1006 38 Output Table 43 Navigation Superflag Output The output supplies not less than 500 mA on a 28 volt system and 250 mA on a 14 volt system with the output voltage not less than Aircraft voltage 3VDC when the flag is to be out of view The output voltage with respect to ground is less than 3 VDC when the flag is to be in view 6 1 10 2 RMI OBI Electrical Charact...

Page 68: ...t Used for 2x5 parallel DME tuning NAV DME Common must be pulled low for the IFD5XX to channel the DME DME is active if the voltage to ground is 1 9 V or the resistance to ground is 375 Outputs is not more than 1 0V while sinking 20 mA 6 1 11 2 King Serial DME Tuning Description Connector Pin Signal Type NAV Serial DME DATA P1006 19 Output NAV Serial DME Clock P1006 18 Output Serial DME CHAN REQ P...

Page 69: ... Model Data Format Notes Avidyne Corporation TAS6XX 9900BX RS232 or ARINC 429 RS 232 preferred L3 Communications SKY497 SKY899 ARINC 429 Bendix King KTA 870 KMH880 ARINC 429 Garmin GTS800 820 850 ARINC 429 Table 48 Traffic Systems 6 4 Lightning Detection System The IFD5XX can be connected to Lightning Detection Systems via RS232 The IFD5XX supports the following Lightning Detection Systems Manufac...

Page 70: ...udio Panels Manufacturer Model Data Format Notes Avidyne AMX240 Analog Audio Garmin SL10 SL10MS SL10M SL10S SL15 SL15M GMA340 GMA347 Analog Audio Honeywell Bendix King KMA24 KMA24H 70 71 KMA26 KMA28 Analog Audio PS Engineering PMA6000 PMA 7000 Series PMA 8000 Series Analog Audio Table 51 Audio Panels 6 7 GAD 42 The IFD5XX can be connected to the Garmin GAD42 Interface Adapter If the IFD5XX is repl...

Page 71: ...IFD5XX Installation Manual 600 00299 000 Page 71 of 198 Revision 02 strapping method as described in Garmin P N 190 00159 00 GAD42 Installation Manual Section 5 1 ...

Page 72: ...corrected altitude from multiple sources in the following formats ARINC 429 RS232 or a Gray Code altitude encoder If multiple altitude sources are connected the IFD5XX will use the altitude sources in this order highest first 1 ARINC 429 ADC 2 ARINC 429 EFIS 3 ARINC 429 Traffic Advisory System 4 RS232 FADC 5 RS 232 Altitude Encoder 6 Parallel Altitude Encoder Gray Code 6 8 1 2 Baro corrected Altit...

Page 73: ...The IFD5XX can accept heading information from Heading Systems in the following formats ARINC 429 or RS232 If multiple heading sources are connected to the IFD5XX the IFD5XX will use the heading sources in this order highest first 1 ARINC 429 INS IRU 2 ARINC 429 EFIS 3 ARINC 429 from GAD42 4 ARINC 429 from EHSI 5 ARINC 429 from GTX 33 330 6 ARINC 429 Traffic Advisory System 7 RS232 FADC 8 RS232 Li...

Page 74: ...armin MX20 RS232 Aviation No Alt format for MX20 version 5 5 and earlier Aviation format for MX20 version 5 6 and later Garmin GMX200 RS232 Aviation format for all GMX200 versions Avidyne Corporation EX500 EX600 EX5000 ARINC 429 Use GAMA format 2 low speed MFD software P N 530 00193 or later is required Avidyne Corporation FlightMax FSD Series RS232 GAMA output may also be used However flight plan...

Page 75: ...s Pin Name Connector Pin I O Terrain not available annunciate P1050 9 Output Terrain Warning Annunciate P1050 10 Output Terrain Caution Annunciate P1050 11 Output TAWS Inhibit Annunciate P1050 12 Output Table 56 Terrain Awareness Annunicator Output 6 12 ADS B Transponder Output The IFD5XX will transmit ADS B compliant GPS position data to the following compatible ADS B capable transponders Manufac...

Page 76: ...9 GPSS KFC400 ARINC 429 Century I II III IV 21 31 41 2000 Trident Analog Deviation Discrete AK 1081 ARINC 429 GPSS S TEC Cobham System 20 30 40 50 55 61 62 GPSS 65 Analog Deviation Discrete System 55X Analog Deviation Discrete ARINC 429 GPSS ST 901 ARINC 429 GPSS Collins APS 65 Analog Deviation Discrete Table 58 Autopilot Systems 6 14 TAWS EGPWS Output The IFD does not accept any data for use or d...

Page 77: ...to the equipment connected to the IFD5XX 7 2 Mounting Check Verify the IFD5XX tray is securely installed to the airframe 7 3 Chassis ID Setting For dual IFD5XX installations it is imperative that the proper Chassis ID settings are established for each IFD via dip switches located along the right side of the IFD5XX outer chassis Not doing so will result in multiple error messages and degraded perfo...

Page 78: ... the IFD5XX is replacing a GNS 530 W use Appendix F Configuration Setup of this manual to first record the configuration of the GNS530 W that is being replaced by the IFD5XX and then using that recorded data use the IFD5XX Maintenance Mode pages as defined in this section and Appendix F Configuration Setup to properly set up and record configurations 7 5 1 Maintenance Mode The Maintenance Mode can...

Page 79: ...NC 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 Selection will have the following options Selection Description Low Standard low speed ARINC 429 nominally 12 5 Kb per second High High speed ARINC 429 nominally 100Kb per second Table 61 ARINC 429 Speed Selection ...

Page 80: ...ected course information from the following Flight Control systems Bendix King KFC400 Garmin GAD 42 Selected course heading and true airspeed data from Garmin GAD 42 Garmin GDU Selected course heading altitude temperature and speed information from the following systems Garmin GDU G500 G600 Garmin GTX 330 Garmin GTX330 No TIS This ARINC 429 speed should be set to the high speed Garmin GTX 330 w Tr...

Page 81: ...ndel SN 3500 Avidyne EXP5000 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...

Page 82: ...9 data as defined by the GAMA General Aviation Subset 2nd Edition including GAMA Graphics Protocol A This format outputs intersection symbols as generic waypoint symbols The output data includes navigation and flight plan information including graphical representation of the flight plan procedures to the following systems Honeywell Primus 1000 GAMA 429 Graphics w INT ARINC 429 data as defined by t...

Page 83: ...X Accepts 429 inputs with SDI 0 or 1 TX Generates all 429 outputs with SDI 1 LNAV 2 Number 2 Copilot long range navigator RX Accepts 429 inputs with SDI 0 or 2 TX Generates all 429 outputs with SDI 2 Table 64 SDI Selection VNAV Selection Description Disable Labels ARINC 429 labels associated with GPS based vertical guidance labels 117G and 327G are not transmitted in the output data stream Note If...

Page 84: ...ection Description Off No device s connected to input of this channel Arnav EI fuel Serial fuel flow information from the following units ARNAV FC 10 FT 10 Electronics International FP 5L CrossSync Serial transfer of flights plans and user waypoints and cross side data e g Datalink traffic lightning etc between IFD5XX units Note This is only an option for CHNL 3 GDL 69 Serial data input for in fli...

Page 85: ...9000T 9200T Shadin fadc Shadin 9628XX X Fuel Air Data Computer Insight TAS 1000 Air Data Computer Shadin Fuel Serial fuel flow information from the following units Shadin 91053XM Digital Fuel Management System Shadin 91204XM Digital Fuel Management System JP Instrument EDM 700 or EDM 760 Engine Monitor Other JPI systems e g JPI FS 450 can use this setting but see the specific format guidance from ...

Page 86: ...0 Engine Monitor Shadin 91204XM Digital Fuel Management System Shadin 91053XP Digital Fuel Management System Shadin 9628XX X Fuel Air Data Computer Stormscope Series II with NAVAID Moving Map Aviation no Alt Serial position velocity and navigation data to the following units Garmin MX20 V5 5 or earlier Horizon DDMP Insight TAS 1000 Air Data Computer CrossSync Serial transfer of flights plans and u...

Page 87: ...System Configuration Page 3 of 10 This is a general page for miscellaneous configurations Figure 13 Main System Configuration Page The Main System Configuration Page Page 3 of 10 allows the configuration of the following Airframe Options and GPS Parameters on the IFD5XX Fuel Type Selections Select Fuel in the Configure field the following options can be selected Selection Description Avgas The air...

Page 88: ...aircraft tail number associated with the user JSUM account External TAWS Selections Selection Description Yes Select if an external EGPWS or TAWS device e g KGP 560 is connected to the IFD5XX This will enable the IFD5XX to send position data to the device and it will disable FLTA and TA functionality as well as aural alerts in the IFD5XX No Select when no external EGPWS or TAWS device is connected...

Page 89: ...are automatically detected by the IFD5XX Figure 14 Main Lighting Configuration Page Photo Response Time Sets the speed at which the brightness changes when photocell is selected as the lighting source Both the Bezel and Display fields have a range of 1 to 5 and the factory default is 3 Photo Slope The Photo Slope sets the sensitivity of the display bezel to changes in the input when the dimming so...

Page 90: ...ft dimmer Both the Bezel and Display fields have a range of 15 to 100 and the factory default is 60 dimBus Minimum The dimBus Minimum sets the minimum brightness when the aircraft dimmer is the dimming source Both the Bezel and Display fields have a range of 1 to 50 and the factory default is 1 dimBus Maximum The dimBus Maximum sets the maximum brightness when the aircraft dimmer is the dimming so...

Page 91: ...IFD5XX Installation Manual 600 00299 000 Page 91 of 198 Revision 02 The AviCurve tracks the aircraft dimming bus as follows Figure 15 Lighting Curve AviCurve Figure 16 Lighting Curve Proportional Curve ...

Page 92: ...te the IFD5XX to the aircraft avionics lighting bus Selection Description dimBus Type DC select this option if the dimming bus is a DC bus AC select this option if the dimming bus is an AC bus The IFD needs to know the bus type in order to alter internal configuration as well as properly perform the calibration dimBus Max Voltage Sets the maximum aircraft dimming bus voltage Range is 0 28V dimBus ...

Page 93: ... scale full deflection to the left up Full Left The remote CDI will be deflected to the left up Center The remote CDI will be centered Full Right The remote CDI will be deflected to the right down Max Right The remote CDI will be off scale full deflection to the right down Table 73 Main CDI Test Page NAV Flag LAT VERT Selection Description Hidden The lateral and vertical flag on the external indic...

Page 94: ...X 2 Ignore Options Selection Description Ignore SEL CRS for GPS Yes No Nav Source knob used in OBS Yes ignore analog or 429 selected course OBS mode then uses the Nav Source knob to dial the course Ignore SEL CRS for VLOC Yes No Yes Lateral navigation flag displays VOR validity deviation data for VOR is always centered No deviation and flag data is based on OBS selection Table 76 Ignore Options Se...

Page 95: ...escription Declutter The vertical deviation bar will be in parked in the maximum UP position when the vertical flag is removed except in the following cases VLOC is selected on the Nav Source knob and an ILS frequency is tuned GPS is selected on the Nav Source knob and valid GPS approach is active precision GPS with vertical guidance Normal The vertical deviation bar will be in the center position...

Page 96: ...full deflection to the left up Full Left The external CDI will be deflected to the left up Center The external CDI will be centered Full Right The external CDI will be deflected to the right down Max Right The external CDI will be off scale full deflection to the right down Table 80 Navigation CDI Test Page NAV Flag LAT VERT Selection Description Hidden The lateral and vertical flag on the externa...

Page 97: ...l calibrate the external CDI HSI to the IFD5XX 1 Select 150 on the CDI HSI 2 Verify the Selected Course is displayed on the IFD5XX and press the ENTR button on the IFD5XX 3 After calibrating verify 30 increments on the CDI HSI are properly displayed on the IFD5XX 2 DME Channel Mode This configuration allows you to set the format for the DME tuning data output Selection Description UNINSTALLED No D...

Page 98: ...on 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 Low Standard Low speed ARINC 429 High High speed ARINC 429 Table 85 VOR LOC GS ARINC 429 Speed Configuration ...

Page 99: ...uts with SDI 1 VOR ILS 2 Number 2 Copilot VOR ILS Receiver RX Accepts 429 inputs with SDI 0 or 2 TX Generates all 429 outputs with SDI 2 Table 86 VOR LOC GS SDI Selection DME Mode Selection Description Directed Freq 1 If the IFD5XX is connected to a single channel or multi channel ARINC429 DME Direct Freq 1 will channel Receiver 1 Directed Freq 2 If the IFD5XX is connected to a multi channel ARINC...

Page 100: ...er 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 10th foot Figure 21 GPS Height ...

Page 101: ...rence 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 Selection Description Attenuation This parameter sets the attenuation GDL 69 69A Reference the Garmin GDL69 69A installation manual for more information Model This parameter sets the mode...

Page 102: ... If this is a new installation of an IFD5XX i e not replacing an existing GNS530 W or if the GAD42 had to be replaced for service then the GAD42 must be configured via a manual strapping method as described in Garmin P N 190 00159 00 GAD42 Installation Manual Section 5 1 If the IFD5XX displays a GAD 42 Needs Service message return the GAD 42 unit to the manufacturer 7 5 13 Other System Diagnostics...

Page 103: ...IFD5XX Installation Manual 600 00299 000 Page 103 of 198 Revision 02 Figure 24 Software Version Page Figure 25 Fan Status Page ...

Page 104: ... for update procedures 7 6 2 Airplane Flight Supplement Check Complete and install the IFD5XX Airplane Flight Manual Supplement in the aircraft s Flight Manual or Pilot s Operating Manual 7 6 3 Instructions for Continued Airworthiness Complete and install the IFD5XX Instruction for Continued Airworthiness in the aircraft maintenance records 7 6 4 Aircraft Weight and Balance Update the Aircraft s W...

Page 105: ... COM Interference After installation the VHF Communication should be tested In 1 MHz increments between 118 136 000 MHz transmit for 35 seconds on each frequency Verify no interference between VHF Comm and other aircraft systems Evaluate the GPS system on the following frequencies The GPS system should not experience complete signal loss on when transmitting on the VHF Comm 25 kHz channels 121 150...

Page 106: ...ng for the IFD5XX can be set to an appropriate level for Day and Night flight conditions Likewise verify any external HSI CDIs can be properly adjusted for day and night lighting conditions 7 6 12 External Annunciators and Switches If installed verify external annunciators and switches are operating correctly Verify the external annunicator lighting can be adjusted for Day and Night flight conditi...

Page 107: ...t RMI 135 Selected Course OBS 150 when interfaced to an HSI with course pointer Desired Track 150 Distance To Go 10 0 NM Time To Go 4 minutes Active Waypoint AVDYN Groundspeed 150 knots Present Position N39 04 05 W094 53 86 Waypoint Alert Active Phase of Flight Enroute Message Alert Active GPS Integrity Invalid Roll Steering if applicable Flight Director commands 0 bank level flight for 5 seconds ...

Page 108: ...formation 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 Note If the IFD5XX is connected to a Primary Flight Display it must be turned off before performing this check ...

Page 109: ...orrect and in the Pilot s field of view 8 2 VHF COM Flight Check Verify inflight the IFD5XX VHF communication transceiver in the high mid and low frequency ranges Test the VHF at least 50 nautical miles and at an appropriate altitude 8 3 VOR Flight Checks Verify inflight the IFD5XX VHF navigation receiver by tuning a local VOR station within 50 nautical miles Verify the audio tone is heard and cou...

Page 110: ... Page 110 of 198 Revision 02 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 ...

Page 111: ...considered to be a qualified pair Pilot Name Description of Glove Test Step Circle one Touch the standby frequency window and verify a virtual keyboard is displayed Pass Fail Type 121 7 press the ENTER button on the virtual keyboard and confirm 121 700 is the displayed frequency in the 1 Standby Com window Pass Fail Press each of the page tabs displayed on the present page and verify the IFD chang...

Page 112: ...LTA functions The IFD is shipped from the factory with this database already loaded and updates are anticipated to be a rare occurrence Table 91 Database Update Cycle In the event the terrain data ever needs updating this is also performed through the front panel USB port 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...

Page 113: ... 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 LSKs and the IFD knob as required to ensure check marks are associated with all the desired files to upload to the IFD Now press the Proceed LSK to begin the file upload ...

Page 114: ...ovide 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 3 min US Charts 180 MB 5 min Worldwide Charts 430 MB 13 min US Nav Data 8 MB 3 min Europe Nav Data 10 MB 2 min Australian Nav Data 1 5 MB 30 sec Worldwide Nav Data 15 MB 7 Min ...

Page 115: ...ou are all done press the Done LSK which will restart the IFD into flight mode Remove the USB fob and perform a normal start up It is highly recommended to verify the data was updated from the Setup LSK of the SYSTEM tab on the AUX page If an IFD is in normal operating mode not maintenance mode the presence of a USB fob is ignored and these pages cannot be accessed 10 2 Datalogs Download There is ...

Page 116: ...he Logs tab Ensure a USB fob is inserted in the IFD front bezel USB port and then use a combination of the left side LSKs and the bottom right IFD knob to select the desired combination of logs and type of action to perform Figure 32 Datalogs Download Page Pressing the Proceed LSK will immediately start downloading all logs listed in the center of the page with green check marks adjacent to them I...

Page 117: ...software image and associated loading procedure from the manufacturer 2 Verify the software part number configuration before and after maintenance is performed on the airborne equipment using the loading procedure instructions 3 It is the responsibility of maintenance personnel to ensure the identified part is recorded in the necessary maintenance logs 4 It is the maintenance personnel s responsib...

Page 118: ...eventative 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 11 3 Cleaning The front display and bezel may require cleaning periodically reference Section 13 ...

Page 119: ...le 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 When calling or emailing for product related help please ...

Page 120: ...Never spray cleaner directly on the screen In general isopropyl alcohol is a safe and effective cleaner Methanol and most acidic solutions can be toxic or damaging to glass coatings if misused Excessive or unnecessary cleaning should be avoided to prevent damage to the coated optical filter surfaces Never allow excess amounts of cleaning agents to dry if they have formed into pools streaks or drop...

Page 121: ...nce 13 Category X no test performed Salt Spray 14 Category X no test performed Magnetic Effects 15 Equipment qualified to Class Z Power Input 16 Equipment qualified to Category B Voltage Spike 17 Equipment qualified to Category A Audio Frequency Conducted Susceptibility 18 Equipment qualified to Category B Induced Signal Susceptibility 19 Equipment qualified to Category ZC Radio Frequency Suscepti...

Page 122: ...so includes any international validations of the STC e g EASA ANAC etc Copies of the STC data are available on the Avidyne website Technical Publications page or upon request The latest data revisions are listed in Avidyne 700 00182 XXX Master Document List AVIFD 306 Installers must abide by the conditions and limitations stated in both the STC and in the Installation Manual in order to maintain c...

Page 123: ...IFD5XX Installation Manual 600 00299 000 Page 123 of 198 Revision 02 Appendix C Mechanical Drawings Figure C 33 Tray Installation ...

Page 124: ...IFD5XX Installation Manual 600 00299 000 Page 124 of 198 Revision 02 Figure C 34 Instrument Panel Cutout ...

Page 125: ...IFD5XX Installation Manual 600 00299 000 Page 125 of 198 Revision 02 Figure C 35 GPS Antenna Installation Forward ...

Page 126: ...Skin Countersunk Rivets 0 032 NAS1097AD4 Countersunk NAS1097AD4 Countersunk 0 032 0 050 Protruding Head Rivets 0 032 MS20470AD4 NAS1097AD4 Countersunk Table 93 Rivet Doubler Selection Rivet type is dependent on the type of rivets in the adjacent fuselage structure If the adjacent rivets in the structure around the bay selected for the doubler installation are protruding head type install MS20470AD...

Page 127: ...IFD5XX Installation Manual 600 00299 000 Page 127 of 198 Revision 02 Figure C 37 GPS Antenna Doubler ...

Page 128: ...ure D 14 VOR ILS Indicator Interconnect 150 Figure D 15 Main Indicator Interconnect 151 Figure D 16 Main Indicator KI209 Interconnect 152 Figure D 17 Main Indicator KI208 Interconnect 153 Figure D 18 Main Indicator MD200 20X Interconnect 154 Figure D 19 RMI OBI Interconnect 155 Figure D 20 King Serial DME Tuning Interconnect Panel Mount 156 Figure D 21 King Serial DME Tuning Interconnect Remote Mo...

Page 129: ...armin 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 Figure D 39 ELT Interconnect 178 ...

Page 130: ... ANTENNA COM ANTENNA VOR LOC ANTENNA GLIDESLOPE ANTENNA GPS ANTENNA COM ANTENNA NAV ANTENNA DIPLEXER S G S VOR 18 AWG 18 AWG 22 AWG LIGHTING BUS HIGH LIGHTING BUS LOW AIRCRAFT POWER AIRCRAFT POWER P1001 P1002 P1006 P1003 P1004 P1005 P1007 2A AIRCRAFT POWER 11 2 3 11 10 18 AWG 4 AIRCRAFT POWER 3 2 5 22 AWG 3 2 6 7 NAV FLAG CIRCUIT BREAKER 5A for 28VDC 7 5 for 14VDC 5A for 28VDC 7 5 for 14VDC 22 AWG...

Page 131: ...NNA COM ANTENNA VOR LOC ANTENNA GLIDESLOPE ANTENNA GPS ANTENNA 1 COM ANTENNA 1 NAV ANTENNA DIPLEXER S G S 1 VOR 1 G S 2 VOR 2 IFD540 2 GPS ANTENNA COM ANTENNA VOR LOC ANTENNA GLIDESLOPE ANTENNA GPS ANTENNA 2 COM ANTENNA 2 8 7 7 P1003 P1004 P1005 P1007 P1007 P1005 P1003 P1004 Page 2 of 3 ...

Page 132: ...IRE GAUGE INTO P1002 PINS IS 20 AWG 6 THE AIRCRAFT POWER INPUT P1006 44 PROVIDES POWER FOR THE VOR LOC SUPERFLAG P1006 15 AND GLIDESLOPE SUPERFLAG P1006 38 OUTPUTS NO POWER CONNECTION IS REQUIRED ON P1006 44 IF THESE FLAG OUTPUTS ARE NOT USED 7 THE GPS ANTENNA COAXIAL CABLE MUST BE DOUBLE OR TRIPLE SHIELDED AND THE LOSS INCLUDING CONNECTORS MUST BE GREATER THAN 1 5 dB AND LESS THAN 6 5 dB 8 COMMAN...

Page 133: ...KEA 346 AT 3000 DB15 DB15 DB15 MALE J4 P1 P1 P1 Trans Cal Bendix King 1 2 3 4 5 9 10 11 13 12 6 1 2 3 4 5 9 10 11 13 12 6 1 2 3 4 5 9 10 11 13 12 6 1 2 3 4 5 9 10 11 13 12 6 2 3 4 5 9 10 11 13 12 6 A B C M N P D L U V R Encoding Altimeter Or Blind Encoder D4 A1 A2 A4 B1 B2 B4 C1 C2 C4 COMMON NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 REFER TO MANUFACTURER S DOCUMENTATION FO...

Page 134: ... ARNAV Insight Elect ronics Int ernat ional GTX327 FC 10 FT 10 FS 450 EDM 760 EDM 700 Minif lo L 91204XT 38 D Minif lo L 91204XT D Digif lo L 91053XP Digif lo L 91053XT D Digidat a 91802 F ADC 200 F ADC 2000 G3 FP 5L P3271 1P1 P1 15 PINF F J2 P2 20 13 2 4 6 SHELL 1 SHELL 1 SHELL 6 2 6 2 5 2 J D 5 2 6 9 11 2 15 SHELL Shadin JP Inst rument s Eventide Insight Electronics International MX20 GMX200 GTX...

Page 135: ...ICAL VERSIONS OF THE MAIN SOFTWARE REFERENCE SECTION 4 FOR WIRING INFORMATION 6 MAPMX MAIN SOFTWARE VERSION 3 10 AND LATER IS THE PREFERRED COMMUNICATION PROTOCOL FOR THE MX20 GMX200 OTHER INPUT PORTS ON MX20 GMX200 MAY BE USED INSTEAD OF THE PORT SHOWN REFER TO APPROPRIATE MANUFACTURER S INSTALLATION DOCUMENTATION 7 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORM...

Page 136: ...CEIVER B NAV 2 RECEIVER A NAV 2 RECEIVER B 47 20 64 63 38 25 P4652B P4652A Bendix King EFS 40 50 SG 465 67 53 16 29 47 20 64 63 38 25 P1 Collins EFIS 84 DPU 84 142 138 122 126 125 129 P1 Collins EFIS 84 DPU 84 142 138 122 126 125 129 4 4 NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 AT IFD540 UNIT TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD EDGE CONNECTOR T...

Page 137: ... B LRN LNAV 2 RECEIVER A LRN LNAV 2 RECEIVER B NAV 1 RECEIVER A NAV 1 RECEIVER B NAV 2 RECEIVER A NAV 2 RECEIVER B ARINC 429 EFIS DISPLAY 2 LNAV TRANSMITTER A LNAV TRANSMITTER B LRN LNAV 1 RECEIVER A LRN LNAV 1 RECEIVER B LRN LNAV 2 RECEIVER A LRN LNAV 2 RECEIVER B NAV 1 RECEIVER A NAV 1 RECEIVER B NAV 2 RECEIVER A NAV 2 RECEIVER B NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2...

Page 138: ...IZE 429 3 RX A 429 3 RX B CDI SOURCE CONTROL RCVR TO FLAG FROM FLAG CDI L CDI R NAV VALID FLAG NAV VALID FLAG GSI UP GSI DOWN GS VALID FLAG GS VALID FLAG ILS 2 ENERGIZE P3 P2 Sandel SN3308 9 27 5 21 11 29 10 28 26 7 5 Autopilot LOCALIZER ENGAGE LEFT RIGHT LATERAL FLAG LATERAL FLAG UP DOWN VERTICAL FLAG VERTICAL FLAG P1 33 3 12 27 17 35 37 19 18 36 16 34 15 33 8 48 49 46 47 14 25 26 21 22 23 24 27 ...

Page 139: ...RSE OBS LEG GPS 1 OFF DEVIATION ANALOG IN GPS 2 OFF OBS ROT NORMAL CDI SRC SEL P2 3 OBS CAL 000 0 RCVR 1 2 P2 12 NAV 1 2 MUST TEMPORARILY BE SET TO ANALOG AND ILS MUST BE SET TO VALID LOW FOR PROPER OPERATION OF THE VDI 5 THESE PINS ON THE SANDEL SN3308 ARE CONFIGURABLE AND CAN BE CHANGED TO SUIT THE PARTICULAR INSTALLATION 6 AUTOPILOT SHOWN FOR REFERENCE ONLY REFER TO APPROPRIATE AUTOPILOT INTERC...

Page 140: ...B GPS ARINC 429 IN 1 B P1001 48 49 Bendix King Collins Honeywell Laseref Litef KAU 461 AHC 85E HG 1075AB HG 1095AB LTR 81 LTN 90 100 LTN 91 LTN 92 P1B P1 INSERT B INSERT B INSERT B J1B 26 27 16 14 G7 G8 G7 G8 G7 G8 49 50 Litton IRU AHRS TRANSMITTER A IRU AHRS TRANSMITTER B P1001 48 49 GPS ARINC 429 IN 1 A GPS ARINC 429 IN 1 B P1001 56 57 GPS RS 232 OUT 1 GPS RS 232 IN 1 RS 232 RXD RS 232 TXD Insig...

Page 141: ...N 3 0 INCHES CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL 3 IF THE GPS ARINC 429 IN 1 PORT P1001 48 AND 49 IS ALREADY USED FOR ANOTHER PURPOSE THE GPS ARINC 429 IN 2 PORT P1001 50 AND 51 MAY BE CONNECTED INSTEAD 4 REFER TO SECTION 7 FOR ARINC 429 CHANNEL SETTINGS 5 REFER TO SECTION 7 FOR RS 232 CHANNEL SETTINGS 6 REFER TO MANUFACTURER S DOCUMENTATION FOR ...

Page 142: ... GPS ARINC 429 OUT B NAV ARINC 429 IN A NAV ARINC 429 IN B NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 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 3 RE...

Page 143: ...DISPLAY GROUND SOFT KEY 1 TEST ALT SOFT KET 4 OPR STB POWER SWITCH HI POWER SWITCH LO RS 232 RX 2 RS 232 TX 2 RS 232 GROUND 2 REMOTE MUTE TRAFFIC ANNUNCIATE OUT SWITCH ARINC 429 OUT 1A ARINC 429 OUT 1B ARINC 429 IN 1A ARINC 429 IN 1B TRAFFIC OPERATE STANDBY SELF TEST SELECT TAWS AUDIO ACTIVE OUT Bendix King KTA 870 KMH 880 KTA 970 KMH 980 L3 Communications SKY 497 SOFTWARE V1 6 OR HIGHER L3 Commun...

Page 144: ...M IS INSTALLED AND ITS DATA MAY BE DISPLAYED ON THE IFD5XX UNIT 6 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION PINOUTS OF OTHER INPUTS SHOWN FOR REFERENCE ONLY 7 IN ORDER FOR SKYWATCH DATA TO BE DISPLAYED ON THE IFD5XX UNIT S MAP PAGE THE IFD5XX UNIT MUST HAVE A DIGITAL HEADING SOURCE OR THE SKYWATCH MUST HAVE A SYNCHRO OR SERIAL HEADING SOURCE A STEPPER H...

Page 145: ...AN 3 0 INCHES CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL 3 ARINC 429 IN 1 P3301 32 AND 35 INPUT ALLOWS AUTOMATED START AND STOP OF FLIGHT TIMER AND PLACES THE TRANSPONDER IN GROUND GND MODE UPON LANDING 4 IF EXTERNAL STBY SELECT IS CONNECTED IN THIS INSTALLATION USE GTX 330 ARINC 429 OUT 1 A AND 1 B PINS 37 AND 34 RATHER THAN ARINC 429 OUT 2 A AND 2 B P...

Page 146: ... CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL 3 IN ORDER FOR WX 500 DATA TO BE DISPLAYED ON THE IFD540 UNIT S MAP PAGE THE IFD540 MUST HAVE A DIGITAL HEADING SOURCE OR THE WX 500 MUST HAVE A SYNCHRO OR SERIAL HEADING SOURCE A STEPPER HEADING SOURCE WILL NOT ALLOW WX 500 DATA TO BE DISPLAYED ON THE MAP PAGE 4 IF AN RS 232 OUTPUT PORT IS CONFIGURED FOR THE ...

Page 147: ...RES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 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 3 CONNECTION TO RS 232 PORT 2 OF THE IFD540 UNIT IS SHOWN IF PORT 2 IS ALREAD...

Page 148: ... 15 16 17 7 34 28 P1006 9 13 10 14 11 15 12 30 10 14 17 19 18 20 NA NA 7 12 8 13 26 32 27 33 8 13 6 14 25 34 NA NA 9 13 10 14 11 15 12 30 GND LUG 17 19 18 20 NA NA 9 10 GND LUG P H R V GND LUG 12 13 GND LUG NA NA 9 10 GND LUG P H R V GND LUG 12 13 GND LUG NA NA 4 5 21 22 37 39 38 40 GND LUG 7 8 24 25 NA NA 9 10 GND LUG P H R V GND LUG 12 13 GND LUG NA NA T 16 GND LUG 3 E C H GND LUG P 13 GND LUG N...

Page 149: ...T 6 INTERCOM WIRING OPTION 7 THE COM REMOTE TRANSFER INPUT P1002 15 MAY BE USED FOR EMERGENCY OPERATION OF THE COM TRANSMITTER IF THE REMOTE TRANSFER SWITCH IS ACTIVE FOR THREE SECONDS THE ACTIVE COM FREQUENCY WILL CHANGE TO 121 50 MHZ 8 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION PINOUT OF OTHER UNITS SHOWN FOR REFERENCE ONLY 9 SHIELDS FOR AUDIO CABLES S...

Page 150: ...C FLAG VOR LOC SUPERFLAG VOR LOC COMPOSITE OUT ILS ENERGIZE GLIDESLOPE UP GLIDESLOPE DOWN FLAG GLIDESLOPE FLAG GLIDESLOPE SUPERFLAG VOR OBS ROTOR H VOR OBS ROTOR C COR OBS STATOR D VOR OBS STATOR E G VOR OBS STATOR F P1006 5 6 1 2 3 4 15 8 29 32 31 30 38 10 9 13 11 12 NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 THIS INTERCONNECT APPLIES ONLY WHEN IT IS DESIRED FOR A SEPARATE...

Page 151: ...5 36 2 1 14 NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 THIS INTERCONNECT APPLIES ONLY WHEN IT IS DESIRED FOR A SEPARATE INDICATOR TO DISPLAY IFD540 VOR ILS INFORMATION REGARDLESS OF THE CDI BUTTON STATUS 3 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE ONLY 4 AT IFD540 UNIT TERMINATE SHIELD G...

Page 152: ... 10K OHM WATT RESISTORS AS SHOWN 3 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE ONLY 4 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 CHASS...

Page 153: ...10K OHM WATT RESISTORS AS SHOWN 3 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE ONLY 4 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 CHASSI...

Page 154: ...R G P1001 21 22 25 26 23 24 2 1 27 28 29 30 32 31 33 34 35 36 NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 THE 200 202 203 DOES NOT HAVE VERTICAL DEVIATION INDICATOR DO NOT USE FOR IFR NAVIAGATION 3 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION PINOUTS OF OTHER UNITS SHOWN FOR REFERENCE ONLY 4 AT IFD540 UNIT TERMINATE SHIELD GROUNDS TO...

Page 155: ...ESS OTHERWISE NOTED 2 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 3 IF IT IS DESIRED TO USE A SEPARATE SWITCH FOR THE RMI POINTER INSTALL AS PER BOTTOM DIAGRAM AND SELECT ALWAYS GPS FOR THE OBI SOURCE FIELD OF THE MAIN CDI OBS CONFIG P...

Page 156: ...ME COMMON N C NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 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 3 THE IFD540 MUST BE CONFIGURED AT INSTALLATION T...

Page 157: ...ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 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 3 THE IFD540 MUST BE CONFIGURED AT INSTALLATION TO OUTPUT KING SERIAL D...

Page 158: ...DME 4MHZ SER DME RNAV MODE PAR DME 3MHZ PARALLEL DME 1MHZ PARALLEL DME 800KHZ PARALLEL DME 400KHZ PARALLEL DME 200KHZ PARALLEL DME 100KHZ PARALLEL DME 50KHZ DME COMMON P1006 12 9 8 11 7 4 6 H 5 C J D M N C N C NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 THE IFD540 MUST BE CONFIGURED FOR PARALLEL 2X5 DME CHANNELING MODE FOR PROPER OPERATION WITH THIS MODEL OF DME TRANSCEIVER ...

Page 159: ...22 KN 61 KN 65 P611 P651 Bendix King Parallel Slip Code Tuned DME M0 M1 M2 M3 K0 K1 K2 K3 K50 DME COMMON 4 3 2 1 9 8 7 6 10 12 14 15 16 17 32 33 34 35 36 22 NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 THE IFD540 MUST BE CONFIGURED TO OUTPUT SLIP CODE DME TUNING DATA FOR PROPER OPERATION IN THIS CONFIGURATION 3 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INT...

Page 160: ... PANEL UNSWITCHED IN HI UNSWITCHED IN LO T GND Lug 31 32 54 55 T GND Lug 31 32 T GND Lug 14 31 4 3 5 6 2 NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 THE TERRAIN ALERTING ON THE IFD5XX DOES NOT SATISFY ANY PART 91 135 REQUIRMENT FOR A TAWS SYSTEM INSTALLING AN EXTERNAL ANNUNCIATOR IS NOT REQUIRED 3 WHEN TWO TAWS EQUIPPED UNITS ARE INSTALLED IN AN AIRCRAFT ONLY ONE SHOULD UTIL...

Page 161: ... CDI NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 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 3 ONLY CONNECTIONS SUPPORTED BY THE AUTOPILOT ARE REQUIRED...

Page 162: ...EV FLAG GS DEV FLAG GS DEV UP GS DEV DOWN 429 GPS IN A 429 GPS IN B GPS SELECT GND GPS ILS ENERGIZE A P IN 2 22 23 24 25 7 31 12 9 10 26 U 17 B 21 Y V 19 C D M K AA C A 23 24 25 26 46 47 7 14 15 12 52 34 2 1 3 4 30 31 24 25 29 48 49 3 2 22 27 10 11 28 48 49 TO MAIN CDI NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED ALL GAMA 429 CONFIGURATIONS OF THE GPS ARINC 429 OUTPUT PROVIDE D...

Page 163: ...AL FLAG MAIN LATERAL FLAG MAIN LEFT MAIN RIGHT MAIN VERTICAL FLAG MAIN VERTICAL FLAG MAIN UP MAIN DOWN ILS GPS APPROACH P1001 23 24 21 22 29 30 27 28 14 13 14 AUTOPILOT LAT DEV FLAG LAT DEV FLAG LAT DEV LT LAT DEV RT GS DEV FLAG GS DEV FLAG GS DEV UP GS DEV DOWN LOC SWITCHING IN 3 B A B A 32 31 45 46 44 2 3 4 5 1 7 8 6 5 2 1 4 3 9 7 8 6 5 2 1 4 3 9 TO MAIN CDI B A 7 8 6 5 2 1 4 3 9 2 Figure D 27 C...

Page 164: ...66 GPS ARINC 429 OUT A GPS ARINC 429 OUT B VLOC ANNUNCIATE 1 2 3 8 4 5 2 1N4444 OR EQUIV NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED THE CENTURY IV REQUIRES THAT AN ISOLATION DIODE BE INSTALLED ON THE LOC SWITCHING INPUT AS SHOWN 3 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 ...

Page 165: ... UP GS DOWN 429 GPS IN A 429 GPS IN B GPS STEERING GPS TRACK GAIN LOC SWITCH 3 13 14 31 30 49 32 13 14 31 30 49 32 1 2 18 19 36 37 38 24 6 23 21 16 77 58 46 45 24 6 23 21 16 77 58 46 45 TO MAIN CDI 5 9 10 42 14 13 26 14 13 26 1 2 18 19 S TEC ST 901 GPSS CONVERTER IFD540 P1001 46 47 1 J3 GPS ARINC 429 OUT A GPS ARINC 429 OUT B VLOC ANNUNCIATE 8 9 22 6 ARINC DATA IN A ARINC DATA IN B GPS OVERRIDE 3 ...

Page 166: ...UT 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 IF THE VLOC ANNUNCIATE SIGNAL IS ONLY USED BY THE AUTOPILOT THIS MAY BE CONNECTED DIRECTLY FOR CONVERTERS 01278 599 AND BELOW 4 AIRCRAFT POWER GPSS STEERING GPS TRACK GAIN TO OTHER SYSTEM GPS ANNUNCIATE S TEC ...

Page 167: ...CAL SUPERFLAG OUT ILS GPS APPROACH P1001 21 22 27 28 23 24 29 30 17 18 14 35 AUTOPILOT VOR LOC DEV LT VOR LOC DEV RT GS DEV UP GS DEV DOWN NAV LL FLAG NAV LL FLAG GS LL FLAG GS LL FLAG NAV HL FLAG NAV LL FLAG GS HL FLAG GS LL FLAG LOC FREQ GND 2 54 53 41 44 4 1 12 9 4 1 12 9 TO MAIN CDI NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED CONNECT EITHER THE LOW LEVEL FLAGS OR THE SUPER...

Page 168: ...GPS ARINC 429 OUT B P4202 Bendix King KFC 400 KCP420 X D KK J W F LNAV 1 RECEIVER A LNAV 1 RECEIVER B AFCS 429 GENERAL A AFCS 429 GENERAL B ROLL STEERING STRAP LNAV 2 RECEIVER A LNAV 2 RECEIVER B NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED IF THE GPS ARINC 429 IN PORT 1 IS ALREADY BEING USED GPS ARINC PORT MAY BE USED 3 LOWER CASE LETTERS SHOWN UNDERLINED 4 REFER TO MANUFACTUR...

Page 169: ...2 P1001 LAMP VOLTAGE FROM DIMMER CIRCUIT IFD540 VLOC ANNUNCIATE GPS ANNUNCIATE VIVISUN INDICATOR B G A 3 GPS VLOC P1 C D 1 P1 1 2 73 P1001 LAMP VOLTAGE FROM DIMMER CIRCUIT IFD540 VLOC ANNUNCIATE GPS ANNUNCIATE CDI SOURCE SELECT VIVISUN INDICATOR STACO INDICATOR CONNECTION VIVISUN INDICATOR CONNECTION VIVISUN INDICATOR SWITCH CONNECTION 4 5 6 Figure D 31 External Navigation Source and GPS Annunciat...

Page 170: ...NNUNCIATION IS VLOC GPS ALTHOUGH NAV GPS WILL BE ACCEPTABLE 4 STACO SWITCH INDICATOR P N 992561 1241762200 14V SYSTEMS AND P N 992561 1241862200 28V SYSTEMS SHOWN 5 VIVISUN INDICATOR P N 95 40 17 B6 AW724 28V SYSTEMS SHOWN INDICATOR MAY BE CONVERTED TO 14V OPERATION BY REPLACING 28V LAMPS WITH 14V LAMPS P N 14 113 6 VIVISUN INDICATOR WITH MOMENTARY SWITCH P N 95 45 11 B6 AW724 28V SYSTEMS SHOWN IN...

Page 171: ...MOTE CDI SWITCH OPTIONAL REMOTE OBS MODE SWITCH OPTIONAL REMOTE COM RECALL SWITCH OPTIONAL NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 TIME MARK OUT P1001 16 OUTPUTS A 1 MILISECOND WIDE PULSE ONCE PER SECOND 3 COM REMOTE RECALL P1001 74 INPUT MAY BE USED TO SCROLL THROUGH A LIST OF PRESET COM FREQUENCIES 2 2 Figure D 32 Switch Interconnect ...

Page 172: ... IN A NAV ARINC 429 IN B NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 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 3 SEE GARMIN GAD 42 INSTALLATION MANUA...

Page 173: ... OR GREATER UNLESS OTHERWISE NOTED 2 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 3 REFER TO THE MANUFACTURER S DOCUMENTATION FOR COMPLETE PIN OUT AND INTERCONNECT INFORMATION...

Page 174: ...UT A GPS ARINC 429 OUT B ARINC 429 RX A ARINC 429 RX B ARINC 429 RX A ARINC 429 RX B GPS ARINC 429 OUT A GPS ARINC 429 OUT B VOR ILS ARINC 429 OUT A VOR ILS ARINC 429 OUT B NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 AT IFD540 UNIT TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE 3 WIRE HARNESS OVERBRAID...

Page 175: ...9 RX NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 AT IFD540 UNIT TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE 3 WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED 4 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION Figure D 36 Avidyne EX500 600 5000 Interconne...

Page 176: ...OUT B VOR ILS ARINC 429 OUT A VOR ILS ARINC 429 OUT B NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 AT IFD540 UNIT TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE 3 WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED 4 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMAT...

Page 177: ...T AND INTERCONNECT INFORMATION IF THE AIRCRAFT HAS AN EXISTING WEIGHT ON WHEELS OUTPUT DO NOT CONNECT 4 4 IFD540 RS232 OUTPUT 2 58 P1001 AVIDYNE AXP340 Secondary TRANSPONDER 3 GPS RS232 INPUT NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED 3 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMAT...

Page 178: ... INPUT NOTES 1 ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED 2 WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED 3 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION IF RS 232 PORT 1 IS NOT AVAILABLE USE ANY OTHER AVAILABLE PORT 4 4 Figure D 39 ELT Interconnect ...

Page 179: ...ars buildings etc Interference Verify another piece of aircraft equipment is not interfering with the GPS system VHF Com is not transmitting Wiring Check the aircraft s PTT switch Check Audio Panel if installed Check wiring The IFD5XX is not tuning the DME Configuration Verify the IFD5XX is configured correctly Wiring Checking wiring DME Verify the DME is configured for the IFD5XX tuning type RS 2...

Page 180: ...hut down in Maintenance Mode Ensure fob is not in the USB slot and reapply power to the IFD Press the left or right side of the AUX page until the DONE Line Select Key is visible and press that LSK to force the IFD to restart into flight mode Unable to get out of Maintenance Mode or not sure how to Press the left or right side of the AUX page until the DONE Line Select Key is visible and press tha...

Page 181: ... approved antenna Yes No 2nd unit Yes No N A 530 W Hardware Part Number and Revision Number back of unit or aircraft logs _______________ _______________ 530 W Software Part Number Main SW Version on start up splash screen __ ________________ _______________ If multiple GNS 530 W were installed describe the slot location that this specific unit was removed from Cockpit Location of Unit s in Questi...

Page 182: ... the GNS 530 W 1st GNS 530 W 2nd GNS 530 W if applicable Traffic Datalink Lightning Sensor Autopilot Fuel Flow System Display s CDI s RMI s Transponder DME ADF Air Data IRU INS Other Other Other Please list the other avionics that are installed in the aircraft and connected to the IFD5XX Enter None or Don t Know as required The IFD5XX Setup pages will be captured on subsequent pages Identification...

Page 183: ...e Download Logs LSK followed by the Confirm LSK These tables contain all the data that can be entered at time of installation to ensure the IFD5XX is properly configured There are additional setup options that selectable by the pilot Display Options on AUX Setup tab that are not documented here IFD5XX Page Navigation To reach the IFD pages on which this data is to be entered select the CONFIG tab ...

Page 184: ...onfig Page 1 10 Speed Data In 1 In 2 Out SDI VNAV For new IFD5XX installations see Section 7 4 2 for selections and descriptions IFD5XX Main RS232 Config Page 2 10 GNS 530 W MAIN RS232 CONFIG Page Input Output CHNL 1 CHNL 2 CHNL 3 CHNL 4 CHNL 5 Input Output CHNL 1 CHNL 2 CHNL 3 CHNL 4 CHNL 5 CHNL 6 For new IFD5XX Installations see Section 7 4 3 for selections and descriptions ...

Page 185: ...G 012 00296 012 00401 GNS 530 W MAIN SYSTEM CONFIG Page Discretes if present CONFIGURE Discretes GPS SELECT COM PRESETS Note Com Presets are always enabled on the IFD5XX GNS 530 W MAIN SYSTEM CONFIG Page Airframe if present CONFIGURE Airframe AIRFRAME AIR GROUND if present Note The Air Ground selection is only present when helicopter is selected for the airframe and is a trigger to look for squat ...

Page 186: ... Installation Manual 600 00299 000 Page 186 of 198 Revision 02 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 ...

Page 187: ...PT IFD5XX MAIN INPUTS Page 4 10 OAT HDG B ALT SAT W DIR D ALT TAT GPS SC P ALT IAS VLC SC L FF TAS CDI R FF W SPD T FF T FOB JOYSTICK WPT Note There is no data to enter on the IFD5XX from this page it is for diagnostics only GNS 530 W INSTRUMENT PANEL SELF TEST For reference only CDI FUEL CAPACITY FLG VCDI FUEL ON BOARD VFLG TO FRM FUEL FLOW ANNUN RMI Set Fuel Flow OBS DTK No IFD5XX Equivalent Pag...

Page 188: ...cable PHOTO SLP OFST if applicable IFD5XX MAIN LIGHTING Page 5 10 Bezel Display Photo Response Time Photo Slope Photo Minimum Photo Maximum dimBus Transition dimBus Slope dimBus Minimum dimBus Maximum dimBus Curve Current Lighting Dimming Bus Calibration Bezel dimBus Type Display dimBus Max Voltage Mx Input dimBus Min Voltage See Section 7 4 5 for instructions on this page ...

Page 189: ...TC TIME No IFD5XX Equivalent Page GNS 530 W MAIN DISCRETE I O Page GRAY CODE DECODED ALTITUDE EXTERNAL SWITCH STATE RMT CDI OBS DISCRETE TOGGLE APR OBS ILS GPS APR GPS TERM INTEG VLOC MSG WPT Note Check off the squares as required to match the solid squares on the GNS 530 unit these check that discretes are wired correctly No IFD5XX Equivalent Page ...

Page 190: ...D COURSE Ignore SEL CRS for GPS Ignore SEL CRS for VLOC CDI OBI SOURCE V FLAG STATE For new IFD5XX installations see Section 7 4 6 for selections and descriptions GNS 530 W COM SETUP Page GNS 530W Only FREQ SQ 250 SPACING SQ 833 SIDETN MIC STORE CALIBRATION PTT XFR RX TX No IFD5XX Equivalent Page Use the User Options tab to select 25 or 8 33 kHz spacing Note The squares above do not need to be rec...

Page 191: ...e Section 7 4 7 for selections and descriptions GNS 530 W VOR LOC GS ARINC 429 CONFIG Page GNS 530W Only RX TX SPEED SDI DME MODE IFD5XX VOR LOC GS ARINC 429 CONFIG Page 8 10 RX TX SPEED SDI DME MODE For new IFD5XX installations see Section 7 4 8 for selections and descriptions GNS 530 W GPS Vertical Offset if present GPS Antenna Height Above Ground IFD5XX GPS Antenna Setup Page 9 10 GPS Antenna H...

Page 192: ...ENSE HDG FLAG SYNC ANGLE HDG STAB SYNC REF HDG VALID Note Squares should all be green if no issues No IFD5XX Equivalent Page GNS 530 W STORMSCOPE TEST Page if configured for Stormscope MODE STATUS TRIGGER COUNT HDG No IFD5XX Equivalent Page Note Stormscope and TWX testing in the IFD5XX is accomplished after a 3 minute suppression period in flight after which any faults are displayed ...

Page 193: ... A if 429 interface LIM B if 429 interface HDG if 429 interface BARO ALT if 429 interface RAD ALT if 429 interface TEST MODE if 429 interface Note Check off the squares as required to match the solid squares on the GNS 530 unit No IFD5XX Equivalent Page Note Traffic test is accomplished after a 3 minute suppression period in flight when any faults are announced There should be no Red X on the traf...

Page 194: ...ence of the traffic thumbnail and the Audio Volume Control page to control these parameters in the IFD5XX GNS 530 W GAD 42 Config Page if configured for an ARINC 429 input from GAD 42 MAIN RMI OBI ROLL STEERING NAV RMI OBI REMOTE CRS SEL SEL CRS DRIVE TAS INPUT DIST SERIAL GPS NAV 429 L H HEADING 429 L H GAD SW VER STATUS No IFD5XX Equivalent Page Note Manually strap the GAD42 or ensure stored con...

Page 195: ...IFD5XX Equivalent Page Use the User Options LSK and Volume Control LSK of the Audio Tab instead GNS 530 W TAWS Audio Config Page 2 if installed ALERT Reduced Terrain Clearance CAUT WARN ALERT Reduced Obstacle Clearance CAUT WARN ALERT Imminent Terrain Impact CAUT WARN ALERT Imminent Obstacle Impact CAUT WARN No IFD5XX Equivalent Page Use the User Options Tab instead ...

Page 196: ...g Page if installed ATTENUATION MODEL if displayed IFD5XX GDL Config Page if installed 10 10 ATTENUATION MODEL GNS 530 W DATALINK DIAGNOSTICS Page if installed QOS TERR SAT 1 SAT 2 TUNER No IFD5XX Equivalent Page Note Use the Datalink Status page on the AUX SYS tab for datalink status data ...

Page 197: ...TO LICENSE THIS SOFTWARE AND RELATED MATERIALS THE SOFTWARE ONLY ON THE CONDITION THAT THE USER AGREES TO THE TERMS OF THE PUBLISHED SOFTWARE LICENSE WHICH CAN BE ACCESSED VIA THIS WEB ADDRESS HTTP WWW AVIDYNE COM SUPPORT LICENSE ASP FCC APPROVAL AND CAUTIONS THIS DEVICE COMPLIES WITH PART 15 OF THE FCC RULES OPERATION IS SUBJECT TO THE CONDITION THAT THIS DEVICE DOES NOT CAUSE HARMFUL INTERFERENC...

Page 198: ...600 00299 000 Copyright 2014 Avidyne Corporation Rev 02 ...

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