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Avidyne Entegra Installation Manual

Avidyne Entegra Installation Manual

Entegra integrated flight display system
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Entegra Integrated Flight Display System
Installation Manual
600-00160-000 REV: 20

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  • Page 1 Entegra Integrated Flight Display System Installation Manual 600-00160-000 REV: 20...
  • Page 3 Release per ECO-18-292 1/16/20 Release per ECO-20-006 This document is applicable to the Entegra Integrated Flight Display System. All materials copyrighted, including images that represent this software. Copyright 2009-2020 Avidyne Corporation. All rights reserved. The latest installation manuals are available to authorized dealers on the web at www.avidyne.com.

  • Page 4: Table Of Contents

    Entegra Integrated Flight Display System Installation Manual Table of Contents General Information .................... 1 Introduction ......................1 Product Description ....................1 Applicability ......................3 System Interconnect ....................7 Technical Specifications ..................8 1.5.1 IFD5000i Integrated Flight Display ............... 8 1.5.2 ACD215 Control Display Unit ................9 1.5.3 GPS723 WAAS Global Positioning Satellite (GPS) Receiver ......
  • Page 5 1.9.1.2 PS Engineering Audio Panel ................41 1.9.2 Transponder ...................... 41 1.9.2.1 Avidyne AXP322 Remote ADS-B Compliant Transponder ......... 41 1.9.2.2 Avidyne AXP340 Panel Mount ADS-B Compliant Transponder ......42 1.9.2.3 Becker Transponders ..................42 1.9.3 UAT Receiver ....................42 1.10...
  • Page 6 Entegra Integrated Flight Display System Installation Manual Enhanced Vision System ..................48 System Setup ....................49 IFD Configuration Setup ..................49 3.1.1 General Information ................... 49 3.1.2 IFD Configuration Tool Setup ................49 3.1.3 Configuring the IFDs ..................52 3.1.4 Post IFD Configuration Checkout ............... 55 IRU Calibration .....................
  • Page 7 4.8.1 Enhanced Vision System ................... 75 Autopilots......................75 4.9.1 S-Tec 55x Autopilot Computer ................75 4.9.2 Avidyne DFC100 Autopilot Computer ..............75 4.10 Engine Data Acquisition Unit ................75 4.10.1 Fuel Quantity Indicator Calibration (PA-46 and PA-32 Only) ......75 4.10.2 EDC-33P-AVI Data Acquisition Unit Test ............
  • Page 8 F-20 SkyWatch TRC497/899 Traffic System Interconnect Diagram ....... 118 F-21 Avidyne TAS6XX Traffic System Interconnect Diagram ......... 119 F-22 Avidyne MLB100/SkyTrax100 ADS-B Weather Receiver Interconnect Diagram ..120 F-23 L3 WX500 Stormscope Interconnect Diagram ............121 F-24 TWX670 Lightning Sensor Interconnect Diagram ..........122 F-25 Bendix King KN62/62A/64 DME Transceiver Diagram ...........
  • Page 9 Entegra Integrated Flight Display System Installation Manual F-31 406MHz ELT Diagram ................... 129 F-32 RDR2000/2100 Diagram ..................130 Appendix G: Interface Control Data ................131 Appendix H: IFD Aircraft Configuration Worksheet ........... 132 600-00160-000 Rev:...

  • Page 11: General Information

    General Information 1.1 Introduction This manual contains information about the physical, mechanical, and electrical characteristics of the Avidyne Entegra Integrated Flight Display (IFD) System, and provides installation instructions for its components. 1.2 Product Description The IFD system consists of the following: •...
  • Page 12 [1] FMS400 along with the dual WAAS capable GPS receivers support TSO-C146d Gamma 1 operations only. FMS900W along with the same dual WAAS capable GPS receivers support TSO- C146d Gamma 3 operations. Contact Avidyne for further product definition. [2] FMS400 or the FMS900W can be installed.

  • Page 13: Applicability

    Entegra Integrated Flight Display System Installation Manual 1.3 Applicability This manual applies to the following part numbers: Model Hardware Software 9.2.1 9.2.2 9.2.3 9.2.4 Component Number Part Part Number Component Number Rev. # Rev. # Rev. # Rev. # Part Number Rev.
  • Page 14 Entegra Integrated Flight Display System Installation Manual Model Hardware Software 9.2.1 9.2.2 9.2.3 9.2.4 Component Number Part Part Number Component Number Rev. # Rev. # Rev. # Rev. # Part Number Rev. # Aircraft Configuration ACM100 700-00156-000 Module Magnetometer/OAT MAG300...
  • Page 15 Entegra Integrated Flight Display System Installation Manual Model Hardware Software 9.3 S/W 9.3.1 S/W 9.3.3 S/W Component Number Part Part Number Rev. # Rev. # Rev. # Number Part Number (or later Component approved (or later revision) approved revision) Inertial Reference Unit...
  • Page 16 [1] Modules are field replaceable components of the IFD [2] Not included in 700-00083-001 IFD configuration. [3] Not included in 700-00083-002 IFD configuration. Contact Avidyne for Release 9.1.1 or earlier Software Part Numbers. Release 9.3.2 was not released and is not a valid configuration. 600-00160-000 Rev: 20...

  • Page 17: System Interconnect

    Entegra Integrated Flight Display System Installation Manual 1.4 System Interconnect The following diagram depicts a typical system interconnect. Detail wiring interconnect information is described in Appendix F: Interconnect Diagrams Optional Optional Avidyne Avidyne Lightning Lightning Optional Optional Traffic Traffic Optional...

  • Page 18: Technical Specifications

    Entegra Integrated Flight Display System Installation Manual 1.5 Technical Specifications IFD5000i Integrated Flight Display 1.5.1 Specification Description/Requirement Standard Features 262,144 Color, In-Plane-Switching (IPS), Thin Film Transistor Display TFT, LCD Diagonal Size 10.4 inches Resolution XVGA (1024 x 768) Interfaces ARINC429, RS232, Analog & Discrete, Byteflight...

  • Page 19: Acd215 Control Display Unit

    Entegra Integrated Flight Display System Installation Manual ACD215 Control Display Unit 1.5.2 Specification Description/Requirement Standard Features Display LED display, F-STN, B&W mode, Transflective Diagonal Size 4.4” Resolution 240 x 64 Interfaces Byteflight Physical Characteristics Weight 2.3 lbs Height See Appendix C...

  • Page 20: Gps723 Waas Global Positioning Satellite (Gps) Receiver

    Entegra Integrated Flight Display System Installation Manual GPS723 WAAS Global Positioning Satellite (GPS) Receiver 1.5.3 Specification Description/Requirement Channels 10 GPS and 2 WAAS Velocity Max velocity: 1,000 knots TTFF (Time to First Fix) less than 5 minutes Reacquisition 20 seconds Position Update Interval 0.2 sec...

  • Page 21: Dvx740 Vhf Communications Transceiver

    Entegra Integrated Flight Display System Installation Manual DVX740 VHF Communications Transceiver 1.5.4 Specification Description/Requirement Audio Output 65 mW into a 150 Ohm load (headphone or line out) Audio Response 250 to 2500Hz within 6dB, down 18dB at 4kHz AGC Characteristics...

  • Page 22: Dvx740 Loc/Gs Receiver Specifications

    Entegra Integrated Flight Display System Installation Manual DVX740 LOC/GS Receiver Specifications 1.5.6 Specification Description/Requirement Glideslope Receiver Selectivity 6dB at least ±10kHz, 40dB no more than ±200kHz Sensitivity (flag) 10uV max Spurious response -60dB or better Centering accuracy 0 ± 0.02 DDM or better...

  • Page 23: Mag300 Magnetometer/Oat Sensor

    Entegra Integrated Flight Display System Installation Manual MAG300 Magnetometer/OAT Sensor 1.5.7 Specification Description/Requirement Standard Features Interfaces RS-422 Physical Characteristics Weight 0.52 Lbs Height 2.53” Width 3.75” Depth 3.75” Electrical Requirements Voltage 24 VDC supplied by IFDs Current Included in IFD Value...

  • Page 24: Regulatory Compliance

    Applicable TSOs 1.6.1 This section identifies Technical Standard Orders (TSOs) applicable to the Entegra IFD system. The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those installing this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards.
  • Page 25 Entegra Integrated Flight Display System Installation Manual Type/ TSO Number Title Ranges Categories Type B Airspeed Indicating TSO-C2d Airspeed Instruments Range is 20 to 300 KIAS Type II Turn Error – TSO-C3e Turn and Slip Instruments Category A TSO-C4c Bank and Pitch Instruments...
  • Page 26 Entegra Integrated Flight Display System Installation Manual Type/ TSO Number Title Ranges Categories Airspeed Indicating Range is 20 to 300 KIAS Vmo is set Maximum Allowable Airspeed TSO-C46a automatically Indicator Systems based on aircraft type selection when applicable Pressure Instruments – Fuel Oil, and...
  • Page 27 Entegra Integrated Flight Display System Installation Manual Type/ TSO Number Title Ranges Categories Automatic Pressure Altitude TSO-C88b Reporting Code Generating Equipment TSO-C106 Air Data Computer Airborne Passive Thunderstorm TSO-C110a Detection Equipment Air Traffic Control Radar Beacon Class N/A TSO-C112e System/Mode Select (ATCRBS/Mode...
  • Page 28 Entegra Integrated Flight Display System Installation Manual Type/ TSO Number Title Ranges Categories VHF Radio Communications Class C, E, 3 Transceiver Equipment Operating and 5 TSO-C169a Within The Radio Frequency Range 117.975 To 137.000 Megahertz Table 10: TSO Authorizations TSO Number...

  • Page 29: Partial Function Tsos

    Non-TSO Functions 1.6.3 There are some functions performed by Entegra IFD System that are not covered by TSOs. It is the installer’s responsibility to ensure that when the IFD is installed it will meet the required minimum performance standards for those functions. Those functions performed by the IFD but not covered by TSO are listed in Table 13.

  • Page 30: Tso Deviations

    Entegra Integrated Flight Display System Installation Manual Non-TSO Functions Display of percent power Lean assist function Display of navigational charts Display of checklists Remote marker beacon indicator Display of Trim Position Display of Oxygen Quantity Display of Ice Protection Fluid Quantity and Mode...
  • Page 31 Entegra Integrated Flight Display System Installation Manual Deviation TSO-C6e – Gyrocompass Compass rose minor tick marks are at 10 degree intervals rather than 5 degrees. Major tick marks are at 30 degree interval, as required. A digital readout with a resolution of 1 degree is also included.
  • Page 32 DO-160E only rather than a combination of AS407C and DO-160E. AS407C requirements apply to portions of the instrument not implemented by the Entegra IFD system. TSO-C45b – Manifold Pressure Instruments The manifold pressure gage title is “MAP” rather than "MANIFOLD PRESSURE" or "MANIF PRESS".
  • Page 33 Environmental qualification performed in accordance with DO-160E only rather than a combination of AS408C and DO-160E. AS408C requirements apply to portions of the instrument not implemented by the Entegra IFD system. TSO-C49b – Tachometer Used current standard AS404C rather than AS404B.
  • Page 34 DO-160E only rather than a (ATCRBS/Mode S) Airborne combination of DO-181E and DO-160G. DO- Equipment 181E requirements apply to portions of the instrument not implemented by the Entegra IFD system. DO-160E is appropriate for the equipment. TSO-C113 – Airborne Multipurpose Environmental qualification performed in...
  • Page 35 Entegra Integrated Flight Display System Installation Manual Deviation Environmental qualification performed in accordance with DO-160E rather than DO- 160G. TSO-C165 – Electronic Map Display De-cluttering not provided as required by the Equipment for Graphical Depiction of TSO on the Chart page due to the pre- Aircraft Position composed nature of the Jeppesen charts.

  • Page 36: Software And Hardware Design Assurance Levels

    All complex electronic hardware devices were developed in compliance with DO-254 Level B. The impact of any known software or hardware problems on proper installation of the Entegra IFD System is reflected in these instructions.
  • Page 37 Entegra Integrated Flight Display System Installation Manual DO-178B Design Component Function Assurance Level VHF Navigation GPS Navigation AP Display & Control Transponder Control & Display Master Warning and Caution and CAS EGPWS Alerts ADF Display and Control Charts Weather Radar...

  • Page 38: Avidyne Supplied Material

    Control & Display Magnetometer/OAT Assembly Heading, OAT Table 15: DO-178B Software Design Assurance Levels 1.7 Avidyne Supplied Material The Entegra IFD System has several kits available: 1) Product Ship Kits 2) Aircraft Installation Kits 3) Optional Ship Kits 600-00160-000 Rev: 20...

  • Page 39: Product Ship Kits

    Entegra Integrated Flight Display System Installation Manual Product Ship Kits 1.7.1 1.7.1.1 Cirrus R9 Ship Kits Note: Ship Kit content and/or Part Numbers may change without notice, verify before ordering. Ship Kit Ship Kit 850-00073-004 850-00073-001 Single Component Dual ADAHRS...
  • Page 40 [5] Pilot Guide, Flight Manual Supplement, & USB thumb drives for data updates and Pilot Guide are not included in the ship kit. They are supplied to the airplane owner directly by Avidyne. [6] Connect ONLY to WAAS GPS Antennas. See Table 36 for approved antennas.

  • Page 41: Piper R9 Ship Kits

    Entegra Integrated Flight Display System Installation Manual 1.7.1.2 Piper R9 Ship Kits Note: Ship Kit content and/or Part Numbers may change without notice, verify before ordering. Ship Kit Ship Kit 850-00073-004 850-00073-008 Component Single ADAHRS Dual ADAHRS System System QTY 2...
  • Page 42 [5] Pilot Guide, Flight Manual Supplement, & USB thumb drives for data updates and Pilot Guide are not included in the ship kit. They are supplied to the airplane owner directly by Avidyne. [6] Connect ONLY to WAAS GPS Antennas. See Table 36 for approved antennas.

  • Page 43: Aircraft Installation Kits

    6) Magnetometer/OAT Sensor - Ship Kit P/N 850-00015-000 • This Kit contains P/N 700-00011-000 Magnetometer/OAT Sensor. This Kit is needed for non-Avidyne PFD equipped aircraft when installing a dual ADAHRS packages. 7) Magnetometer/OAT Sensor - Ship Kit P/N 850-00015-001 •...
  • Page 44 Entegra Integrated Flight Display System Installation Manual 1) Cirrus 2X Dual ADAHRS Installation Kit contains the following: Nomenclature Unit Part Number Display Support Bracket 120-00820-000 Display Gusset 120-00821-000 Display Strap 120-00822-000 Display Doubler 120-00823-000 Magnetometer Bracket 120-00873-000 Coupling, Quick Disconnect 130-00215-000 Elbow Fitting –...
  • Page 45 Entegra Integrated Flight Display System Installation Manual 2) Cirrus 2X Single ADAHRS Installation Kit contains the following: Nomenclature Unit Part Number Display Support Bracket 120-00820-000 Display Gusset 120-00821-000 Display Strap 120-00822-000 Display Doubler 120-00823-000 Connector RD15M00000 Connector PLC18F0000 Backshell D15000Z400...
  • Page 46 Entegra Integrated Flight Display System Installation Manual 5) Dual Magnetometer Bracket Installation Kit: Nomenclature Unit Part Number Dual Magnetometer 120-00873-000 Bracket Table 25: Dual Magnetometer Bracket Kit 820-00092-004 6) Magnetometer/OAT Sensor Kit: This is P/N 700-00011-000 Magnetometer/OAT Sensor. Nomenclature Unit Part Number...
  • Page 47 Entegra Integrated Flight Display System Installation Manual 9) Adapter Harness Connector Kit: Nomenclature Unit Part Number Connector 030-00357-000 Connector 030-00136-000 Table 29: Adapter Harness Connector Kit 820-00092-006 10) Magnetometer/OAT Sensor Kit: This is P/N 700-00011-001 Magnetometer/OAT Sensor. (Piper PA- Nomenclature...
  • Page 48 Entegra Integrated Flight Display System Installation Manual Nomenclature Unit Part Number Autopilot Tray Support Bracket, Left 120-00937-001 Connector, Circular, 10-Position, 030-00203-000 Female Contact, Female 030-00527-000 Connector, 24-Position, Female 030-00623-000 Female Elbow, 90 Degree, Nylon ¼” 130-00216-000 Coupling, Quick Disconnect, 1/8 NPT...

  • Page 49: Activation Kits

    Entegra Integrated Flight Display System Installation Manual Activation Kits 1.7.3 The following kits are required to activate the associated functions. 1.7.3.1 Enhanced Vision System Activation Kit This Kit is only needed if connecting the IFD to a RS-170 Video input. Contact Avidyne for more details.

  • Page 50: Rd Party Supplied Equipment

    Note: The S-Tec 55X autopilot computer requires a software mod level as identified on the units S.W. mod label of “AF” and a S.W. version of 7 or higher to be compatible with the Entegra IFD. The S.W. version is displayed during the boot cycle of the autopilot computer. After applying power to the autopilot the initial boot page will display, blank out and then display the software version number.

  • Page 51: Optional Equipment

    Installation Manual 1.9 Optional equipment Audio Panel 1.9.1 1.9.1.1 Avidyne AMX240 Audio Panel If installing the optional AMX240 Audio Panel contact Avidyne to order the following part number: Comments Nomenclature Part Number AMX240 Audio Panel Ship Kit 850-00218-000 Table 38: Avidyne AMX240 Audio Panel Part Number 1.9.1.2...

  • Page 52: Avidyne Axp340 Panel Mount Ads-B Compliant Transponder

    MLB100/SkyTrax100 UAT Receiver with ARINC429 850-00223-000 MLB100/SkyTrax100 UAT Receiver without ARINC429 850-00223-001 Table 43: Avidyne UAT Receiver Equipment Part Numbers 1.10 Documentation All IFD Documentation is provided via the Avidyne Dealer Website, contact Avidyne for more details. 600-00160-000 Rev: 20...

  • Page 53: Installation Instructions

    The IFD Synthetic Vision System with Forward Looking Terrain Alerting must not be installed in aircraft with an operational Terrain Awareness System (TAWS) as defined by TSO-C151. If the Avidyne Terrain Alerting and Forward Looking Terrain Alerting is installed and operating on the IFD System, any existing EGPWS/TAWS system must be disabled. The Terrain Alerting and Forward Looking Terrain Alerting on the IFD system is not a TSO-C151 system, and does not satisfy any Part 91/135 TAWS requirements.
  • Page 54 Entegra Integrated Flight Display System Installation Manual • Follow acceptable avionics installation practices per AC43.13-1B, AC43.13-2B, or later FAA approved revisions. • VHF Radio installation instructions have been prepared to meet the guidance material defined in AC20-67B, “Airborne VHF Communications Equipment Installations”.
  • Page 55 VHF Communication/Navigation Antennas • The Entegra IFD System or later is designed to interface to existing VHF communication/navigation antennas. Existing coaxes can be reused to connect to IFDs. Existing coax connectors are to be replaced with connectors as specified in approved Entegra installation data.

  • Page 56: Cooling

    Entegra Integrated Flight Display System Installation Manual If installing new antennas, the antenna must meet the following TSOs: • The VHF Communication Antenna should meet one of the following Technical Standard Orders (TSO): TSO-C37( ), TSO-C38( ), TSO-C169( ). •...

  • Page 57: Electrical And Sensor Interfaces

    Power to the IFD and Control/Display Unit is provided directly from the aircraft, there is no on/off switch. The IFD and Control/Display Unit can operate from 18 to 32 VDC. Sensor Interface 2.5.2 See Appendix F for specific wiring interface instructions. Note: For Avidyne DFC100 Installations, reference the DFC100 STC Installation Data. Bezel Lighting 2.5.3 Each IFD should be wired to a 0-28 VDC aircraft dimming bus (if equipped) to control the bezel button and knob backlight brightness via the cockpit panel brightness control.

  • Page 58: Byteflight Data Bus

    Appendix F: Interconnect Diagrams, does not depict metal harness overbraid but it may be required. ByteFlight Data Bus 2.5.5 Avidyne’s ByteFlight Databus has unique set of interconnect requirements. Contact Avidyne for more information. 2.6 Pitot-Static Interface IFDs with 700-00083-000 Part Numbers will connect directly to the aircraft pitot-static system. The connectors are included in the installation kit.

  • Page 59: System Setup

    • IFD Configuration Data Utility software (“IFD Configuration Tool.exe”), Avidyne part number 570-00117-XXX. The IFD Configuration Tool can be downloaded from the Avidyne Dealer website. Note: Table 44 below lists the appropriate IFD Configuration Data Utility for each IFD software version.
  • Page 60 Entegra Integrated Flight Display System Installation Manual IFD Configuration Data IFD Software Utility Software Version¹ (or later approved revision) 9.0.0.0 570-00117-001 Rev. 00 9.0.1.0 570-00117-001 Rev. 01 9.0.2.X 570-00117-002 Rev. 00 9.1.0.0 570-00117-003 Rev. 01 9.2.X.0 570-00117-004 Rev. 00 9.3.0 570-00117-005 Rev.
  • Page 61 Figure 2: IFD Configuration Tool 2. Select the appropriate Aircraft Model from the drop down list. a) Do not select an aircraft model with “(NO DATA)” from the drop down. b) Contact Avidyne if the desired Aircraft Model is not listed. 600-00160-000 Rev:...

  • Page 62: Configuring The Ifds

    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 63 Entegra Integrated Flight Display System Installation Manual NOTE: After changing any of the IFDs configurations, the IFDs may display “IFD Fixing Setup” message, DO NOT Power down the IFD’s during this time period. 2. Power on the IFDs and allow it to initialize. This will take several minutes. Allow the ADAHRS box to disappear.
  • Page 64 8. Press the LSK “Check Disk”. Verify no errors are reported by the IFD. If errors are reported by the IFD, Contact Avidyne Technical Support for more information. 9. Select the Configuration file for the aircraft. Unselect any other aircraft configurations and/or databases, if listed.

  • Page 65: Post Ifd Configuration Checkout

    This procedure calibrates the Internal Reference Units (IRU) in both IFDs to compensate for the aircraft’s instrument panel tilt angles. In the event the default calibration offset values stored in the IFDs do not adequately calibrate the IRUs, Avidyne personnel are authorized to change the default offset calibration values.
  • Page 66 Entegra Integrated Flight Display System Installation Manual Note: The following procedure applies to ALL IFDs that contain ADAHRS. 3. Press the SYS function key on the IFD. 4. Select the “Setup” tab (See Figure 3). 5. Select “Update Databases” LSK by pressing on either side of the button. Press the “Confirm”.

  • Page 67: Air Data Unit

    Figure 5: IRU Calibration Page 9. Select “Restore Defaults”, verify the saved values are appropriate for the aircraft type (Contact Avidyne if needed) and then select “Save Offsets”. If the values shown are incorrect, enter the correct values and then select “Save Offsets”...

  • Page 68: Calibration

    Entegra Integrated Flight Display System Installation Manual If an “OUT OF RANGE” indication is displayed in the digital readout window of the IFD Altimeter Indicator, the tester shall decrease the target pressure in the test equipment in the smallest increment the particular test equipment can provide. This procedure is to continue until a valid pressure altitude value (non “OUT OF RANGE”...

  • Page 69: Charts Database Loading

    Note: If you see the message, "ADU Cal Failed. No valid response received from Air Data Unit. Select “Done" to reinitialize the IFD. Wait 2 minutes for the air data to stabilize, and re-run the ADU Calibration. If it fails again, contact Avidyne Technical Support.

  • Page 70: Navigation & Obstacle Database Loading

    3.5 Navigation & Obstacle Database Loading This section is to be performed after downloading the Navigation and Obstacle data from Jeppesen JSUM to one of the Avidyne Supplied USB thumb drives.. The following steps are performed on both IFDs: 1. Insert the USB thumb drive into the IFD.

  • Page 71: Gps Reset

    Entegra Integrated Flight Display System Installation Manual 3.6 GPS Reset If either GPS Receiver is unable to calculate a position after >10 minutes outside with an unobstructed view of the sky, the GPS may need to be reset. GPS Resets are primarily needed when the GPS Receiver last position fix saved to the memory is >1000 miles from its current...

  • Page 72: Axp322 Transponder Configuration (Optional)

    (see Figure 6 AXP322 Transponder Configuration Setup Page) Figure 6: AXP322 Transponder Configuration Setup Page This page will configure the Avidyne AXP322 Remote transponder. Reference the AXP322 installation manual as needed. The transponder must be configured to operate. 600-00160-000 Rev: 20...
  • Page 73 Enter "Yes" if the aircraft is equipped with UAT ADS-B In receiver, “NO” if the aircraft is not equipped with a UAT ADS- B in receiver Squat Input Enter the squat switch input type. Select "Avidyne". A/C Class Enter the aircraft category A/C Speed Enter the aircraft speed GPS Lat.

  • Page 74: Radar Configuration

    Entegra Integrated Flight Display System Installation Manual 3.8 Radar Configuration The Radar configuration module for the RDR2000 should be configured as followed. (Extra Aircraft only) OPERATION STRUT OVERRIDE: F [= False] CONFIG: TARGET ALERT: T [= True] MAP GAIN ADJUST:...

  • Page 75: Post-Installation Checks And Calibrations

    Entegra Integrated Flight Display System Installation Manual Post-Installation Checks and Calibrations This section will test the various functions of IFD. Prior to Starting this section, verify the IFDs are properly configured and not displaying any Caution/Warning Messages on the Status Page.

  • Page 76: Magnetic Compass Swing

    ■ The calibration procedure is done in a known magnetically clean area at least 200 ft. from metal structures of any kind and not on surfaces that may contain underground fuel tanks or steel rebar (concrete ramp). Avidyne suggests using an approved compass rose for this procedure.
  • Page 77 Entegra Integrated Flight Display System Installation Manual corner of the display indicates zero seconds. The “Technician Maintenance Mode” ” page will be displayed (seeFigure 6: AXP322 Transponder Configuration Setup Page). 10. Press “Proceed” LSK. 11. Press the right side of the “SYS” page function key to select the “Cal” tab. The “Magnetometer Calibration”...

  • Page 78: Fuel Quantity Calibration

    19. Verify heading accuracy of both left and right IFDs on cardinal headings (+/- 2 deg from right to left IFDs and 4 deg max. from compass rose or sight compass). 20. Contact Avidyne for additional installation instructions if the IFD’s continue to have Heading errors.
  • Page 79 Entegra Integrated Flight Display System Installation Manual Tank 1 and 2 FQ Calibration 1. Assure right IFD is off. 2. Assure EDC-33P is powered on. 3. Place the Left IFD in “Technician Mode” by performing the following steps: 1) Select SYS function key and tab over to “Setup”.
  • Page 80 Entegra Integrated Flight Display System Installation Manual 21. Fill tank to 32 gallons into Tank 1 as indicated by the fuel delivery system gauge. 22. Select the “Accept Value” LSK. 23. Select “5” in the “Cal Point” LSK. 24. Fill tank to 40 gallons into Tank 1 as indicated by the fuel delivery system gauge.
  • Page 81 Entegra Integrated Flight Display System Installation Manual Figure 9: Empty Calibration Point Example Figure 10: Calibration Point 1 Example 600-00160-000 Rev:...

  • Page 82: Two Point Calibration Procedure

    Entegra Integrated Flight Display System Installation Manual Figure 11: Full Calibration Point Example Two Point Calibration Procedure 4.7.2 The following procedure only applies to R9 installations that include a fuel quantity indicator and a Electronics International EDC-33P. Refer to aircraft maintenance manual for applicability.
  • Page 83 Entegra Integrated Flight Display System Installation Manual 6. Select “Fuel” in the “Cal Select” LSK. 7. Select “DAU” in the “Fuel Source” LSK. 8. Select “1” in the “Cal Tank” LSK. 9. Select “Empty” in the “Cal Point” LSK. 10. Assuring the tank is empty of usable fuel (only unusable fuel remains) select the “Accept Value”...
  • Page 84 Entegra Integrated Flight Display System Installation Manual Figure 12: Empty Calibration Point Example Figure 13:: Full Calibration Point Example 600-00160-000 Rev: 20...

  • Page 85: Sensors

    Note: This may take several minutes and several adjustments. Allow the Autopilot time to settle between adjustments. Avidyne DFC100 Autopilot Computer 4.9.2 Reference the Avidyne DFC Series Autopilot’s STC data for Post-Installation Setup and Checkout. Note: Inflight Calibrations are not required. 4.10 Engine Data Acquisition Unit Fuel Quantity Indicator Calibration (PA-46 and PA-32 Only) 4.10.1...
  • Page 86 If the "Accept Value" LSK is not displayed, the raw value may be outside the required tolerance for the fuel probe/sensor. Note the displayed raw value and the displayed LSKs and contact Avidyne Technical Support. 9. Right Tank Empty Calibration a.

  • Page 87: Edc-33P-Avi Data Acquisition Unit Test

    If the "Accept Value" LSK is not displayed, the raw value may be outside the required tolerance for the fuel probe/sensor. Note the displayed raw value and the displayed LSKs and contact Avidyne Technical Support. 13. Right Tank Full Calibration a.

  • Page 88: Radar Configuration

    Entegra Integrated Flight Display System Installation Manual 4.12 Radar Configuration Preliminary Radar Setup 1. Power on the IFDs and select the radar page 2. Enter into Technician mode on the IFD connected directly to the radar. Note that the other IFDs will display “Radar Sensor Error”.
  • Page 89 Entegra Integrated Flight Display System Installation Manual b. To decrement the value of the “Roll Angle” use the left inner knob to change the “Tilt Setting” between -5 and -10. When the “Tilt Setting” is set between -5 and -10, the value of the “Roll Angle”...

  • Page 90: System Flight Checks

    Entegra Integrated Flight Display System Installation Manual System Flight Checks 5.1 Autopilot Inflight Setup and Checkout (S-TEC Autopilot Only) The following AP calibration procedure is performed on the right IFD only. This procedure will calibrate both IFDs. Perform the following steps in-flight in smooth air.

  • Page 91: System Checkout

    Entegra Integrated Flight Display System Installation Manual Figure 15: Autopilot Calibration Procedure Page 5. Upon completing the procedure above, verify the following: a. HDG mode accurately tracks the Heading Bug. b. Flight Director Command Bars are above the aircraft reference symbol with no gap between the two.

  • Page 92: Radar Flight Test

    After completing all ground and flight tests, complete the IFD Aircraft Configuration Form in Appendix H. Attach it to the IFD Instructions for Continued Airworthiness (document number AVIFD- 016, available on the Avidyne Dealer website) and install both documents into the aircraft records. 5.3 Radar Flight Test Perform the stabilization flight test instructions found in the RDR2000 pilot’s guide to determine if...

  • Page 93: Cleaning The Ifd And Control/Display Unit Screens

    Entegra Integrated Flight Display System Installation Manual Cleaning the IFD and Control/Display Unit Screens If the IFD5000i and/or the Control/Display screen should become dirty due to fingerprints or dust, clean the screen using the following materials and methods: ● A clean, soft lint free cloth such as 3M Ultra-Brite Cloth # 2011 or similar.

  • Page 94: Factory Service Policies And Procedures

    3. Be prepared to download the aircraft flight logs and email/transmit them to Avidyne Customer Service. 4. The file system check function should only be used as directed by Avidyne support. Be prepared to use the “Check Disk” button on Technician pages.
  • Page 95 Entegra Integrated Flight Display System Installation Manual Securely pack the unit in the Avidyne shipping carton, write the RMA number on the outside of the carton, and return it to the address provided by the Avidyne Customer Service Representative. Include your name, complete shipping address, daytime telephone number, a complete description of the problem, the desired return date, and shipping method.

  • Page 96: Stc Permission

    Avidyne Corporation hereby grants to all National Aviation Authority (FAA, CAA, JAA) approved installers the use of data from STC SA00282BO to install the Avidyne R9 System. This also 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.

  • Page 97: Appendix A: Environmental Qualification Forms

    Entegra Integrated Flight Display System Installation Manual Appendix A: Environmental Qualification Forms INTEGRATED FLIGHT DISPLAY PART NO: 700-00083-( ) MANUFACTURER: AVIDYNE CORPORATION ADDRESS: 710 NORTH DRIVE, MELBOURNE, FL 34934 Table A1: DO-160E ENVIRONMENTAL QUALIFICATION RTCA/DO-160E Environmental Tests Test Category Section...
  • Page 98 Entegra Integrated Flight Display System Installation Manual CONTROL DISPLAY UNIT PART NO: 700-00150-( ) MANUFACTURER: AVIDYNE CORPORATION ADDRESS: 710 NORTH DRIVE, MELBOURNE, FL 34934 Table A2: DO-160E ENVIRONMENTAL QUALIFICATION TESTS RTCA/DO- Environmental Tests Test Category 160E Section Temperature and Altitude Low Temp 4.5.1...
  • Page 99 Entegra Integrated Flight Display System Installation Manual MAGNETOMETER/OAT SENSOR NO: 700-00011-( ) MANUFACTURER: AVIDYNE CORPORATION ADDRESS: 710 NORTH DRIVE, MELBOURNE, FL 34934 Table A3: DO160D ENVIRONMENTAL QUALIFICATION TESTS Conditions RTCA DO-160D Conducted Test Category Section Low Temp 4.5.1 Equipment qualified to Category D2 High Temp 4.5.2 &...
  • Page 100 Entegra Integrated Flight Display System Installation Manual AIRCRAFT CONFIGURATION MODULE PART NO: 700-00156-( ) MANUFACTURER: AVIDYNE CORPORATION ADDRESS: 55 OLD BEDFORD ROAD, LINCOLN, MA 01773 Table A4: DO-160E ENVIRONMENTAL QUALIFICATION TESTS RTCA/DO- Environmental Tests Test Category 160E Section Temperature and Altitude Low Temp 4.5.2...

  • Page 101: Appendix B: Ifd Cutout And Outline Dimensions

    Entegra Integrated Flight Display System Installation Manual Appendix B: IFD Cutout and Outline Dimensions Figure B-1 Integrated Flight Display Front and Right Views 600-00160-000 Rev:...
  • Page 102 Entegra Integrated Flight Display System Installation Manual Figure B-2 Integrated Flight Display Rear and Top Views 600-00160-000 Rev: 20...
  • Page 103 Entegra Integrated Flight Display System Installation Manual Figure B-3 Integrated Flight Display Instrument Panel Cutout 600-00160-000 Rev:...
  • Page 104 Entegra Integrated Flight Display System Installation Manual Figure B-4 Integrated Flight Display Coaxial Cable Connectors 600-00160-000 Rev: 20...

  • Page 105: Appendix C: Control Display Unit Outline Dimensions

    Entegra Integrated Flight Display System Installation Manual Appendix C: Control Display Unit Outline Dimensions Figure C-1 Control Display Unit Outline Dimensions 600-00160-000 Rev:...

  • Page 106: Appendix D: 700-00011-000, Magnetometer/Oat Sensor Outline Dimensions

    Entegra Integrated Flight Display System Installation Manual Appendix D: 700-00011-000, Magnetometer/OAT Sensor Outline Dimensions Figure D-1 Magnetometer/OAT Sensor Outline Dimensions 1. ARROW INDICATES FORWARD INSTALLATION DIRECTION. 2. CG SHOWN AS CABLES ARE SHOWN. 3. INSTALL OAT PROBE WITH NUT AND WASHER PROVIDED WITH ASSEMBLY AND LOCATE IN FREE AIR STREAM.

  • Page 107: Appendix E: 700-00011-001, Magnetometer/Oat Sensor Outline Dimensions

    Entegra Integrated Flight Display System Installation Manual Appendix E: 700-00011-001, Magnetometer/OAT Sensor Outline Dimensions Figure E-1 Magnetometer/OAT Sensor Outline Dimensions 1. ARROW INDICATES FORWARD INSTALLATION DIRECTION. 2. CG SHOWN AS CABLES ARE SHOWN. 3. INSTALL OAT PROBE WITH NUT AND WASHER PROVIDED WITH ASSEMBLY AND LOCATE IN FREE AIR STREAM.

  • Page 108: Appendix F: Interconnect Diagrams

    Entegra Integrated Flight Display System Installation Manual Appendix F: Interconnect Diagrams F-1 IFD5000i Power, Grounds, Bezel Lighting Interconnect Diagram 600-00160-000 Rev: 20...

  • Page 109: Ifd5000I Power, Grounds, And Lighting Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-2 IFD5000i Power, Grounds, and Lighting Interconnect Diagram 600-00160-000 Rev:...

  • Page 110: Stec 55X Autopilot Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-3 STEC 55X Autopilot Interconnect Diagram 600-00160-000 Rev: 20...

  • Page 111: Stec 55X Autopilot Interconnect Diagram (Continued)

    Entegra Integrated Flight Display System Installation Manual F-3 STEC 55X Autopilot Interconnect Diagram (Continued) 600-00160-000 Rev:...

  • Page 112: Mag300 Magnetometer Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-4 MAG300 Magnetometer Interconnect Diagram Also See Table 17 or Table 19 for additional installation details. 600-00160-000 Rev: 20...

  • Page 113: Data Acquisition Unit (Dau) Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-5 Data Acquisition Unit (DAU) Interconnect Diagram 600-00160-000 Rev:...

  • Page 114: Signal Interface Unit (Siu) Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-6 Signal Interface Unit (SIU) Interconnect Diagram 600-00160-000 Rev: 20...

  • Page 115: Avidyne Amx240 Audio Panel Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-7 Avidyne AMX240 Audio Panel Interconnect Diagram 600-00160-000 Rev:...

  • Page 116: Ps Engineering Pma8000B Audio Panel Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-8 PS Engineering PMA8000B Audio Panel Interconnect Diagram 600-00160-000 Rev: 20...

  • Page 117: Ps Engineering Pma8000 Audio Panel Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-9 PS Engineering PMA8000 Audio Panel Interconnect Diagram 600-00160-000 Rev:...

  • Page 118: Garmin Gma340 Audio Panel Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-10 Garmin GMA340 Audio Panel Interconnect Diagram 600-00160-000 Rev: 20...

  • Page 119: Mlb700 Weather Datalink Receiver Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-11 MLB700 Weather Datalink Receiver Interconnect Diagram 600-00160-000 Rev:...

  • Page 120: Honeywell Kgp560 Egpws Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-12 Honeywell KGP560 EGPWS Interconnect Diagram 600-00160-000 Rev: 20...

  • Page 121: Avidyne Axp322 Transponder Diagram

    1. ALL WIRES SHALL BE 22 GUAGE MIL-C-27500 (SHIELDED) OR EQIVALENT 2. TERMINATE SHIELDS TO THE CONNECTOR BACKSHELL OR CHASSIS GROUND AS CLOSE TO CONNECTOR AS POSSIBLE 3. REFER TO AVIDYNE AXP322 INSTALLATION MANUAL 600-00312-00 FOR FURTHER AXP322 INSTALLATION INSTRUCTIONS 600-00160-000 Rev:...

  • Page 122: Avidyne Axp340 Transponder Interconnect Diagram

    1. ALL WIRES SHALL BE 22 GUAGE MIL-C-27500 (SHIELDED) OR EQIVALENT 2. TERMINATE SHIELDS TO THE CONNECTOR BACKSHELL OR CHASSIS GROUND AS CLOSE TO CONNECTOR AS POSSIBLE 3. REFER TO AVIDYNE AXP340 INSTALLATION MANUAL 600-00308-00 FOR FURTHER AXP340 INSTALLATION INSTRUCTIONS 4. WOW SIGNAL FROM IFD IS "GROUND ON GROUND"...

  • Page 123: Becker Atc 4401-2-250Mode C Transponder Diagram

    Entegra Integrated Flight Display System Installation Manual F-15 Becker ATC 4401-2-250Mode C Transponder Diagram 600-00160-000 Rev:...

  • Page 124: Becker Bxp-6402-1R - (01) Mode S Transponder Diagram

    Entegra Integrated Flight Display System Installation Manual F-16 Becker BXP-6402-1R - (01) Mode S Transponder Diagram 600-00160-000 Rev: 20...

  • Page 125: Acd215 Control Display Unit Interconnect Diagram (Two Ifd5000I System)

    Entegra Integrated Flight Display System Installation Manual F-17 ACD215 Control Display Unit Interconnect Diagram (Two IFD5000i System) 600-00160-000 Rev:...

  • Page 126: Dfc100 Byteflight Diagram (Two Ifd5000I System)

    Entegra Integrated Flight Display System Installation Manual F-18 DFC100 ByteFlight Diagram (Two IFD5000i System) 600-00160-000 Rev: 20...

  • Page 127: Dfc100 Byteflight Diagram (Three Display)

    Entegra Integrated Flight Display System Installation Manual F-19 DFC100 Byteflight Diagram (Three Display) 600-00160-000 Rev:...

  • Page 128: Skywatch Trc497/899 Traffic System Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-20 SkyWatch TRC497/899 Traffic System Interconnect Diagram 600-00160-000 Rev: 20...

  • Page 129: Avidyne Tas6Xx Traffic System Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-21 Avidyne TAS6XX Traffic System Interconnect Diagram 600-00160-000 Rev:...

  • Page 130: Avidyne Mlb100/Skytrax100 Ads-B Weather Receiver Interconnect Diagram

    ALL WIRES SHALL BE 22 GUAGE MIL-C-27500 (SHIELDED) OR EQIVALENT. TERMINATE SHIELDS TO THE CONNECTOR BACKSHELL OR CHASSIS GROUND AS CLOSE TO CONNECTOR AS POSSIBLE. USING THE R9 CONFIGURATION TOOL SELECT “Avidyne ADS-B WX” FOR CONFIGURING THE R9 IFD. 600-00160-000 Rev: 20...

  • Page 131: L3 Wx500 Stormscope Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-23 L3 WX500 Stormscope Interconnect Diagram 600-00160-000 Rev:...

  • Page 132: Twx670 Lightning Sensor Interconnect Diagram

    Entegra Integrated Flight Display System Installation Manual F-24 TWX670 Lightning Sensor Interconnect Diagram 600-00160-000 Rev: 20...

  • Page 133: Bendix King Kn62/62A/64 Dme Transceiver Diagram

    Entegra Integrated Flight Display System Installation Manual F-25 Bendix King KN62/62A/64 DME Transceiver Diagram 600-00160-000 Rev:...

  • Page 134: Bendix King Kn63 Dme Transceiver Diagram

    Entegra Integrated Flight Display System Installation Manual F-26 Bendix King KN63 DME Transceiver Diagram 600-00160-000 Rev: 20...

  • Page 135: Shadin Adf Converter Diagram

    Entegra Integrated Flight Display System Installation Manual F-27 Shadin ADF Converter Diagram 600-00160-000 Rev:...

  • Page 136: Chelton Dfs 43A Adf System Diagram

    Entegra Integrated Flight Display System Installation Manual F-28 Chelton DFS 43A ADF System Diagram 600-00160-000 Rev: 20...

  • Page 137: Rs-170 Video Input Diagram

    Entegra Integrated Flight Display System Installation Manual F-29 RS-170 Video Input Diagram 600-00160-000 Rev:...

  • Page 138: Edc-33P-Avi Dau Diagram

    Entegra Integrated Flight Display System Installation Manual F-30 EDC-33P-AVI DAU Diagram 600-00160-000 Rev: 20...

  • Page 139: 406Mhz Elt Diagram

    Entegra Integrated Flight Display System Installation Manual F-31 406MHz ELT Diagram 600-00160-000 Rev:...

  • Page 140: Rdr2000/2100 Diagram

    Entegra Integrated Flight Display System Installation Manual F-32 RDR2000/2100 Diagram 600-00160-000 Rev: 20...

  • Page 141: Appendix G: Interface Control Data

    Entegra Integrated Flight Display System Installation Manual Appendix G: Interface Control Data Table: G1 ARINC 429 Transmit Out Messages Arinc 429 Out 4 (J121-15,36) - Both IFDs Low Speed Data Label Format Transmission Period Uncorrected Barometric Altitude ARINC 429 BNR...

  • Page 142: Appendix H: Ifd Aircraft Configuration Worksheet

    Entegra Integrated Flight Display System Installation Manual Appendix H: IFD Aircraft Configuration Worksheet IFD Aircraft Configuration Sheet Aircraft Description IRU Calibration Numbers Aircraft Make: Left Center Right Roll: Aircraft Model: Pitch: Aircraft Serial Number: Yaw: IFD Aircraft Configuration Audio Panel:...
  • Page 143 Entegra Integrated Flight Display System Installation Manual WARRANTY: AVIDYNE WARRANTS THE PRODUCT MANUFACTURED BY IT AGAINST DEFECTS IN MATERIAL AND WORKMANSHIP FOR A PERIOD OF TWENTY-FOUR (24) 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...

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