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Avidyne Envision EXP5000 Installation Manual
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Avidyne Envision EXP5000 Installation Manual

Avidyne Envision EXP5000 Installation Manual

Primary flight display
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EXP5000
Primary Flight Display
Installation Manual
700-00006-000 PFD
For Release 7.1 and later
Document P/N 600-00141-010 REV 6

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Summary of Contents for Avidyne Envision EXP5000

  • Page 1 EXP5000 Primary Flight Display Installation Manual 700-00006-000 PFD For Release 7.1 and later Document P/N 600-00141-010 REV 6...
  • Page 3 Magnetometer/OAT Sensor Software Part Number: 530-00124-000. All materials copyrighted including images that represent this software Copyright 2009 Avidyne Corporation. All rights reserved. The latest installation manuals are available to authorized Avidyne dealers on the web at www.avidyne.com. Avidyne® is a registered trademarks of Avidyne Corporation.
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  • Page 5: Table Of Contents

    2.5 Pre-Modification Planning ......................10 2.5.1 Pre-Modification Checklist ....................10 2.5.2 Requirements and Limitations ....................10 2.5.3 Electrical Load Analysis......................11 2.6 Installing the Envision EXP5000 PFD ................... 12 2.6.1 Installation Planning ......................12 2.6.2 Mechanical Installation ......................13 2.6.3 Electrical Installation ......................14 3 System Setup .........................
  • Page 6 Installation Manual P/N 600-00141-010 REV 6 B.1 700-00006-000 PFD Front and Top Dimensions................48 B.2 700-00006-000 PFD Right and Rear Dimensions ................ 49 Appendix C: Magnetometer/OAT Sensor Dimensions ............50 Appendix D: PFD Cutout Dimensions..................51 Appendix E: PFD Wiring Diagrams ..................52 E.1 Key to Electrical Symols .......................
  • Page 7 Installation Manual P/N 600-00141-010 REV 6 List of Tables Table 1: PFD Technical Specifications......................2 Table 2: Magnetometer/OAT Sensor Technical Specifications ..............2 Table 3: TSOs Applicable to PFDs with 530-00200-( ) Software ..............3 Table 4: TSO Authorizations for Magnetometer/OAT Sensor ..............4 Table 5: Partial Function TSOs ........................
  • Page 8 Installation Manual P/N 600-00141-010 REV 6 List of Figures Figure 1: Pilot’s Field of View ........................13 Figure 2: PFD Connectors.......................... 14 Figure 3: PFD Controls..........................17 Figure 4: System Page ..........................18 Figure 5: Airspeed Indicator Configuration Page..................20 Figure 6: Avionics Page, Release 7.1 and Later ..................

  • Page 9: General Information

    1C, when used in conjunction with the documents listed in Table 8, “Required Documents,” on page 8. This manual may also be used as a guide for installation of the Avidyne Envision EXP5000 PFD and Magnetometer/OAT Sensor in Class III aircraft listed on the AML (see AML R34-0447 for additional documents required for installation under the STC).

  • Page 10: Technical Specification

    Installation Manual P/N 600-00141-010 REV 6 1.2 Technical Specification 1.2.1 PFD Unit Table 1: PFD Technical Specifications Specification Description/Requirement Standard Features Display High Brightness Sunlight Readable Color Active Matrix LCD Diagonal size 10.4 inches Resolution SVGA 800 X 600 Interfaces ARINC 429 (to GPS/VHF navigators), TTL and Analog (to Autopilot) Minimum Viewing Angle 60 degrees horizontal and +45/-15 degrees vertical...

  • Page 11: Tso Information

    Installation Manual P/N 600-00141-010 REV 6 1.3 TSO Information This section covers information regarding TSOs applicable to the PFD and Magnetometer/OAT Sensor. 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 12: Table 4: Tso Authorizations For Magnetometer/Oat Sensor

    Installation Manual P/N 600-00141-010 REV 6 Table 3: TSOs Applicable to PFDs with 530-00200-( ) Software TSO# Description Type/ Ranges Categories TSO-C55a FUEL AND OIL QUANTITY INSTRUMENTS (RECIPROCATING ENGINE AIRCRAFT) TSO-C88b AUTOMATIC PRESSURE ALTITUDE REPORTING CODE GENERATING EQUIPMENT TSO-C106 AIR DATA COMPUTER TSO-C113 AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS...

  • Page 13: Table 6: Function Not Covered Bytsos

    Installation Manual P/N 600-00141-010 REV 6 The PFD performs some functions that are not covered by TSOs. It is the installer’s responsibility to ensure that when the PFD is installed, it will meet the required minimum performance standards for those functions. Those functions performed by the PFD but not covered by TSO are listed in Table 6. Table 6: Function Not Covered byTSOs Non-TSO Functions Display of Vspeed labels...
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  • Page 15: Installation Instructions

    The software part number is displayed on the Initialization Display window, described in the Note: Avidyne Pilot’s Guide for your aircraft, as well as on the System Setup Main window, described in Section 3.1, “Accessing the Setup Pages” on page 17.

  • Page 16: Additional Documents

    R34-0443 Instructions for Continued Airworthiness for Avidyne EXP5000 PFD with Magnetometer / OAT Sensor on Part 23 Airplanes R34-0446 AFM Supplement for Installation of Avidyne EXP5000 PFD with Magnetometer / OAT Sensor on Part 23 Airplanes R34-0444 Master Data List...
  • Page 17 Installation Manual P/N 600-00141-010 REV 6 Table 9: Parts Required But Not Supplied Item Part Number Description Vendor Remarks D-436-38 SPLICE RAYCHEM SEE NOTE 5 D-150-0175 SPLICE, SHIELDED RAYCHEM SEE NOTE 5 704-15K36 DIODE, TRANSIENT MICROSEMI SEE NOTE 1, 5 SUPPRESSOR MS25036-107 TERMINAL RING, #6 AWG...

  • Page 18: Pre-Modification Planning

    Installation Manual P/N 600-00141-010 REV 6 2.5 Pre-Modification Planning 2.5.1 Pre-Modification Checklist Complete Table 10 to ensure that the aircraft to be modified is a candidate for installation of the EXP5000 PFD using the AML-STC. All rows must PASS in order to use the AML-STC as the certification basis for the EXP5000 installation.

  • Page 19: Electrical Load Analysis

    Installation Manual P/N 600-00141-010 REV 6 2.5.3 Electrical Load Analysis Perform an electrical load analysis to verify that the aircraft complies with 14 CFR 23.1351(a). This can be accomplished by adding the loads in Table 11 to the aircraft’s total electrical load for each affected bus.

  • Page 20: Installing The Envision Exp5000 Pfd

    Avidyne recommends that you install the PFD with the MFD (if equipped) uninstalled to provide better access. Install the pitot and static lines after the PFD has been installed into the panel to avoid kinking the hoses.

  • Page 21: Mechanical Installation

    Installation Manual P/N 600-00141-010 REV 6 2.6.2 Mechanical Installation 2.6.2.1 Location and Viewing Angle The PFD is designed to be panel-mounted and held in place by four captive 10-32 screws. A standard 1/4” wide slotted screwdriver is required. Install each screw with 30 +/− 0.5in-lb. of torque. Locate the PFD in the panel so that the pilot can easily reach all knobs and controls.

  • Page 22: Electrical Installation

    Installation Manual P/N 600-00141-010 REV 6 2.6.2.4 Pitot-Static Interface The PFD connects directly to the aircraft pitot-static system. Reference drawing D34-1147.Use the following pressure connectors: Quantity Part Number Description Supplier PMC1703 3/16” tube ID, barb style, quick clip, Acetal Colder Products The Pitot (Pt) and Static (Ps) connections on the PFD are marked accordingly.
  • Page 23 Installation Manual P/N 600-00141-010 REV 6 2.6.3.2 Electrical and Sensor Interfaces Power to the PFD is provided directly from the aircraft, there is no on/off switch. The PFD primary voltage is nominally 28 VDC. The PFD should be wired to the aircraft dimming bus (if equipped) to control the bezel button backlight brightness via the cockpit panel brightness control.
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  • Page 25: System Setup

    Installation Manual P/N 600-00141-010 REV 6 3 System Setup This section discusses the setup procedures for software release 7.1.X, part number 530-00200-( ) After making any configuration changes, you must cycle power to the PFD. Note: 3.1 Accessing the Setup Pages You will use the System Setup and Information pages to set up the EXP5000.

  • Page 26: System Page

    Installation Manual P/N 600-00141-010 REV 6 Logging Page and System Info Pages—Used by qualified Avidyne Service Technicians to diagnose problems with the PFD. Not discussed in this installation manual. 3.2 System Page Figure 4: System Page The System Page provides summary information about the PFD and its current setup. The information on the System Page depends on the your aircraft and PFD software version.

  • Page 27: Adjusting The Pitch Offset

    Installation Manual P/N 600-00141-010 REV 6 The buttons on the System Page are: A/C Model—For Envision installations, the aircraft Model is Aftermarket. This value cannot be changed. Back to PFD—Saves your changes and returns you to the flight state of the PFD display. This button is available on all System Setup and Information Pages.

  • Page 28: Configuring The Asi (Airspeed Indicator)

    Installation Manual P/N 600-00141-010 REV 6 3.2.2 Configuring the ASI (Airspeed Indicator) For most aircraft, the Airspeed Indicator Configuration page displays the current factory defaults. The ASI displays the V-Speeds and other important information. If you make changes to the VSpeeds, follow the procedure below exactly. Any deviation Note: may cause the VSpeed edits not to be saved, which may result in inaccurate indications on the Airspeed Indicator.

  • Page 29: Table 13: Required V-Speeds

    Installation Manual P/N 600-00141-010 REV 6 Setting the airspeed and altimeter automatically sets the vertical speed scale, even though Note: vertical speed does not display on the Airspeed Indicator Configuration page. – When set to 44 knots /440 feet, the vertical speed scale is ±2000 fpm. –...

  • Page 30: Table 14: Optional V-Speeds

    Installation Manual P/N 600-00141-010 REV 6 Optional V-Speeds—The optional V-Speeds applicable to your aircraft model and ASI type display under the Optional V-Speeds. Table 14 displays the V-Speeds that may display for each type of ASI. Enter the values for your aircraft in the last column. Table 14: Optional V-Speeds V-Speed Speed Definition...

  • Page 31: Avionics Page

    Installation Manual P/N 600-00141-010 REV 6 3.3 Avionics Page To set up the avionics for the PFD: 1. Rotate the left knob to select the Avionics Page: Figure 6: Avionics Page, Release 7.1 and Later The avionics on the aircraft are shown. Make sure that the information on this page matches the installed avionics on your aircraft.
  • Page 32 Installation Manual P/N 600-00141-010 REV 6 OAT Source—Select the OAT source: ADC (Air Data Computer), or None. In some installations using the internal air data sensors, the OAT probe on the magnetometer is mounted inside the aircraft and will not provide accurate temperature readings. If an accurate OAT source is not available, the OAT Source must be set to None.

  • Page 33: Configuring The Gns Unit

    Installation Manual P/N 600-00141-010 REV 6 3.4 Configuring the GNS Unit You must also configure the Garmin 420/430/530 GNS unit to communicate with the PFD after selecting the avionics as discussed in Section 3.3, “Avionics Page” on page 23. See the Users Guide for your GNS unit for detailed operating information. Note: Except where specified, instructions that reference Garmin 420/430/530 also apply to the Note:...

  • Page 34: Table 17: Vor/Loc/Gs Arinc 429 Configuration Page

    Installation Manual P/N 600-00141-010 REV 6 Applies when dual GNS units are installed, otherwise ignore. 4. For GNS-430/530 and “W” Units only (for GNC-420 units, go to step 5): a. Turn the right inner knob until the MAIN INPUTS 2 Page displays. Verify that CDI = GPS.

  • Page 35: Display Format/Units Page

    Installation Manual P/N 600-00141-010 REV 6 3.5 Display Format/Units Page To set EXP5000 display options: 1. Scroll the left knob to the Display tab. 2. The Display Format/Units Page displays: 3. Select the display options you want as follows: Table 18: Display Page Options Button Options Default...
  • Page 36 For aircraft equipped with Flight Director, setting the ARS display to the flying W suppresses Note: the Flight Director command bars. Avidyne suggests that you only set the flying W ARS symbol for non-Flight Director equipped aircraft. 4. When you are done, press Back to PFD or use the left knob to select another System Setup page.

  • Page 37: Calibration Page

    Installation Manual P/N 600-00141-010 REV 6 3.6 Calibration Page To calibrate the EXP5000: 1. Rotate the left knob to open the Calibration page. 2. The Calibration Page displays: Figure 7: Calibration Page 3. Select the button for each item to calibrate. The selections are: IRU Cal —...

  • Page 38: Calibrating The Iru

    Installation Manual P/N 600-00141-010 REV 6 3.6.1 Calibrating the IRU For Envision installations, you may need to enter the IRU pitch and roll values manually. The default value is zero degrees in pitch and roll. Ensure that the aircraft is level before checking instrument panel offset angles.

  • Page 39: Calibrating The Magnetometer

    The calibration procedure is done in a known magnetically clean area at least 200 ft. from metal structures of any kind and not above areas that may have underground fuel tanks or steel rebar in the concrete ramp. Avidyne suggests using an approved compass rose for this procedure.

  • Page 40: Figure 9: Initial Magnetometer Calibration Page

    Installation Manual P/N 600-00141-010 REV 6 On the last heading calibration point (330°), it may take up to a minute for “Done” to display. Note: If any of the 12 calibration points display Failed rather than Done, press Redo Previous to “undo” the previous step and repeat the calibration.
  • Page 41 Installation Manual P/N 600-00141-010 REV 6 If you stop the calibration process (for example, by exiting the Magnetometer Calibration Page Note: or shutting off power to the PFD) before completion, you will lose the stored calibration parameters. You will need to rerun the calibration from the beginning. 10.

  • Page 42: Calibrating The Adu

    Installation Manual P/N 600-00141-010 REV 6 3.6.3 Calibrating the ADU If an out of tolerance condition is observed when conducting air data testing described in Part 43 Appendix E, the error may be corrected by recalibrating the ADU To calibrate the ADU: 1.
  • Page 43 Note: Return to PFD.", reboot the PFD, wait 2 minutes for the air data to stabilize, and re-run the ADU Calibration. If it fails again, contact Avidyne Technical Support. 6. Press Back to PFD. 7. Re-run the air data test described in Part 43 Appendix E and verify that the ADU calibration corrected any error.
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  • Page 45: Post-Installation Checks

    Installation Manual P/N 600-00141-010 REV 6 4 Post-Installation Checks This section applies to all current releases of the EXP5000, listed in Section 1, “General Information” on page 1. During the post-installation check you need to verify the items that apply to the aircraft: Ground Checks, page 37 Cleaning the EXP5000 Screen, page 39 Inflight Setup and Checkout, page 40...

  • Page 46: Table 20: Gps Nav/Comm Check (1 X Gns 430W/530W, 1 X Gnc-420)

    Installation Manual P/N 600-00141-010 REV 6 4.1.1.2 Single GPS-NAV-COM, Single GPS Combination (1 x GNS-430/530, 1 x GNC- 420) To begin the check, press Nav until GPS1 displays. Check that the GNS-430 1 CDI button displays GPS. As you press the buttons listed in Table 20, check that the PFD Nav button and GNS-430/530 display the expected values as detailed in Table 20.

  • Page 47: Pitot-Static Leak Check

    Installation Manual P/N 600-00141-010 REV 6 4.1.2 Pitot-Static Leak Check Perform a pitot-static leak check anytime the pitot-static ports are disconnected from (and then reconnected to) the PFD. Ensure that you perform the pitot-static leak check in accordance with the specific Aircraft Maintenance Manual.

  • Page 48: Inflight Setup And Checkout

    Installation Manual P/N 600-00141-010 REV 6 4.3 Inflight Setup and Checkout For S-Tec 55X or 65, ensure that the autopilot is configured as a KCS-55-compatible unit. See Note: S-Tec documentation for details. Perform all in flight tests and calibrations as described in the following sections: Autopilot Roll Centering Adjustment (S-Tec 55X or 65), page 40 Autopilot Checkout, page 40 Star Aviation In-Flight Tests, page 41...

  • Page 49: Star Aviation In-Flight Tests

    Installation Manual P/N 600-00141-010 REV 6 9. Select Back to PFD. 10. Verify that the HDG mode accurately tracks the Heading Bug. 11. If the aircraft has an FD, verify that the FD Steering Command Bars are above the ARS (aircraft reference symbol) with no gap between the two.
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  • Page 51: Factory Service Policies

    Prior to returning a unit for service, contact Avidyne at 888-723-7592 to obtain a Return Merchandise Authorization (RMA) number. Securely pack the unit in the original 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.
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  • Page 53: Appendix A: Environmental Qualification Forms

    P/N 600-00141-010 REV 6 Appendix A: Environmental Qualification Forms PFD RTCA/DO-160E ENVIRONMENTAL QUALIFICATION FORM NOMENCLATURE: PART NO: 700-00006-000 MANUFACTURER: AVIDYNE CORPORATION ADDRESS: 55 OLD BEDFORD ROAD, LINCOLN, MA 01773 Table 22: DO-160E ENVIRONMENTAL QUALIFICATION TESTS Conditions RTCA/DO-160D Conducted Test Category...

  • Page 54: Table 23: Do-160D Environmental Qualification Tests

    Installation Manual P/N 600-00141-010 REV 6 PFD RTCA/DO-160D ENVIRONMENTAL QUALIFICATION FORM NOMENCLATURE: PART NO: 700-00006-000 MANUFACTURER: AVIDYNE CORPORATION ADDRESS: 55 OLD BEDFORD ROAD, LINCOLN, MA 01773 Table 23: DO-160D ENVIRONMENTAL QUALIFICATION TESTS Conditions RTCA/DO-160D Conducted Test Category Section Low Temp 4.5.1...

  • Page 55: Table 24: Magnetometer/Oat Sensor Rtca/Do-160D Environmental Qualification Form

    Installation Manual P/N 600-00141-010 REV 6 NOMENCLATURE: MAGNETOMETER/OAT SENSOR PART NO: 700-00011-000 MANUFACTURER: AVIDYNE CORPORATION ADDRESS: 55 OLD BEDFORD ROAD, LINCOLN, MA 01773 Table 24: MAGNETOMETER/OAT SENSOR RTCA/DO-160D ENVIRONMENTAL QUALIFICATION FORM Conditions RTCA DO-160D Conducted Test Category Section Low Temp 4.5.1...

  • Page 56: Appendix B: Envision 700-00006-000 Pfd Dimensions

    Installation Manual P/N 600-00141-010 REV 6 Appendix B: Envision 700-00006-000 PFD Dimensions B.1 700-00006-000 PFD Front and Top Dimensions 9.73 7.88 5.32 Top View 10.69 8.50 Front View Figure 12: PFD 700-00006-000 Top and Front View - 48 -...

  • Page 57: 700-00006-000 Pfd Right And Rear Dimensions

    Installation Manual P/N 600-00141-010 REV 6 B.2 700-00006-000 PFD Right and Rear Dimensions 9.39 3.00 REAR SUPPORT BRACKET 1.18 8.42 Right View 10.084 7.890 7.14 4X 10-32 SCREWS (CAPTIVE) Rear View Figure 13: PFD 700-00006-000 Right and Rear View - 49 -...

  • Page 58: Appendix C: Magnetometer/Oat Sensor Dimensions

    Installation Manual P/N 600-00141-010 REV 6 Appendix C: Magnetometer/OAT Sensor Dimensions 3.187 B.C. 15° MOUNTING LOCATIONS EQUALLY SPACED ON A 3.187 B.C. 120.0° 120° .156 SLOT, 3 PL 3.50 O.D. 1.875 21.0 5/16" RECOMMENDED MOUNTING HOLE SIZE 2.53 .060 1.875 14.0 Figure 14: 700-00011-000 Magnetometer/OAT Sensor Dimensions 1.

  • Page 59: Appendix D: Pfd Cutout Dimensions

    Installation Manual P/N 600-00141-010 REV 6 Appendix D: PFD Cutout Dimensions 7.94 7.89 2X 7.68 6X R 2X .20 2X 0 4X - .03 3X - .24 Figure 15: PFD Cutout Dimensions (Landscape) THRU BACKSIDE OF PANEL 45.0° INSTALL SOLID 100 RIVET FROM FAR SIDE 8 PLACES...

  • Page 60: Appendix E: Pfd Wiring Diagrams

    Installation Manual P/N 600-00141-010 REV 6 Appendix E: PFD Wiring Diagrams E.1 Key to Electrical Symols The following symbols are used in the wiring diagrams that follow. NOTES SYMBOLS SPECIFIC NOTE APPLIES WIRING SYMBOLS TWISTED PAIR OPTIONAL WIRING OVERBRAID SHIELD CHASSIS GROUND Figure 17: Key to Electrical Symbols - 52 -...

  • Page 61: Pfd Magnetometer, Oat, Power, And Lighting Interconnect

    Installation Manual P/N 600-00141-010 REV 6 E.2 PFD Magnetometer, OAT, Power, and Lighting Interconnect AVIDYNE AVIDYNE 700-00006-XXX 700-00011-XXX-() ENVISION EXP5000 MAGNETOMETER/ J730 OAT SENSOR J734 MAG/OAT +24VDC OUT +24 VDC MAG/OAT POWER GND RXD + MAG/OAT 422 TX + RXD -...

  • Page 62: Mfd Interconnect - Rs232

    Installation Manual P/N 600-00141-010 REV 6 E.3 MFD Interconnect – RS232 AVIDYNE AVIDYNE 700-00006-000 700-00004-XXX ENVISION EXP5000 700-00030-XXX EX5000 J1401 FLIGHTMAX MFD RS232 1 GND RS232 1 RX COM7 TX SHIELD GND SHIELD GND EXP5000 J1401 COM 7 TX DETAIL A NOTES: 1.

  • Page 63: Pfd Interconnect With Gns-430/Gns-430W/Gnc-420

    Installation Manual P/N 600-00141-010 REV 6 E.4 PFD Interconnect with GNS-430/GNS-430W/GNC-420 AVIDYNE 700-00006-000 ENVISION EXP5000 J732 GNS-430 No. 2 P1001 GPS ARINC 429 TX A ARINC 429 CH 3 RX A GPS ARINC 429 TX B ARINC 429 CH 3 RX B...

  • Page 64: Pfd Interconnect With Nav Relay, Gns-430/430W, And S-Tec 55X

    ARINC 429 RX B GPS ARINC 429 TX A GPS ARINC 429 TX B AVIDYNE SHIELD GND 700-00006-XXX ENVISION EXP5000 J732 S-TEC 55X A/P ROLL STEERING 429A ARINC 429 CH 0 TX A ROLL STEERING 429B ARINC 429 CH 0 TX B...

  • Page 65: S-Tec 55X Analog Signal Interconnect

    Installation Manual P/N 600-00141-010 REV 6 E.6 S-TEC 55X Analog Signal Interconnect AVIDYNE 700-00006-000 ENVISION EXP5000 S-Tec 55X Autopilot J733 L-R +LT ANALOG GND L-R -RT ANALOG OUTPUT 5 SHIELD GND DC HDG HI ANALOG OUTPUT 2 HDG RETURN ANALOG GND...

  • Page 66: S-Tec 55X Digital/Discrete Signal Interconnect

    Installation Manual P/N 600-00141-010 REV 6 E.7 S-TEC 55X Digital/Discrete Signal Interconnect AVIDYNE 700-00006-XXX S-Tec 55X Autopilot ENVISION EXP5000 J732 ANNUN LOAD DISCRETE INPUT 2 ANNUN CLOCK DISCRETE INPUT 0 ANNUN DATA DISCRETE INPUT 1 SHIELD GND ALT ENGAGE SIGNAL...

  • Page 67: Autopilot / Flight Director Relay, S-Tec 55X

    1. ALL WIRES ARE 22 AWG MIN UNLESS OTHERWISE NOTED 2. FLIGHT DIRECTOR RELAY PART NUMBER: KHS-17D11-24 (TYCO) RETAINING SPRING PART NUMBER: 20C297 (TYCO) AVIDYNE CORPORATION DIODE PART NUMBER: IN4001 SOCKET PART NUMBER: 27E894 (TYCO) 3. AP ON LIGHTED PUSHBUTTON SWITCH...

  • Page 68: Pfd Interconnect With Nav Relay, Gns-430/430W, And S-Tec 65 Autopilot

    ARINC 429 RX B GPS ARINC 429 TX A GPS ARINC 429 TX B AVIDYNE 700-00006-XXX SHIELD GND ENVISION EXP5000 J732 S-Tec 901 Roll Steering ROLL STEERING 429A ARINC 429 CH 0 TX A ROLL STEERING 429B ARINC 429 CH 0 TX B...

  • Page 69: Analog Signal Interconnect - S-Tec 65 Autopilot

    Installation Manual P/N 600-00141-010 REV 6 E.10 Analog Signal Interconnect - S-TEC 65 Autopilot AVIDYNE 700-00006-000 ENVISION EXP5000 S-Tec 65 Autopilot J733 RFGC NAV +LT ANALOG GND NAV +RT ANALOG OUT 5 SHIELD GND SHIELD GND DC HEADING ERROR HI...

  • Page 70: Discrete Signal Interconnect - S-Tec 65 Autopilot

    Installation Manual P/N 600-00141-010 REV 6 E.11 Discrete Signal Interconnect - S-TEC 65 Autopilot AVIDYNE 700-00006-000 ENVISION EXP5000 S-Tec 65 Autopilot J732 DISCRETE IN 11 PITCH SOLENOID LOGIC SHIELD GND SHIELD GND PFGC GS FLAG HI DISCRETE OUT 1 GS FLAG LO...

  • Page 71: Adf Interconnect With Shadin Converter

    Installation Manual P/N 600-00141-010 REV 6 E.12 ADF Interconnect with Shadin Converter AVIDYNE 700-00006-000 ENVISION EXP5000 Shadin 933752-000 J732 ARINC 429 OUTPUT A ARINC 429 CH 5 RX A ARINC 429 OUTPUT B ARINC 429 CH 5 RX B SHIELD GND...

  • Page 72: Adf Interconnect With Dfs-43A

    Installation Manual P/N 600-00141-010 REV 6 E.13 ADF Interconnect with DFS-43A AVIDYNE 700-00006-000 ENVISION EXP5000 DFS-43A J732 J1001 ARINC 429 CH 5 RX A ARINC 429 OUTPUT A ARINC 429 CH 5 RX B ARINC 429 OUTPUT B SHIELD GND...

  • Page 73: Radar Altimeter Interconnect

    Installation Manual P/N 600-00141-010 REV 6 E.14 Radar Altimeter Interconnect AVIDYNE 700-00006-000 Radar Altimeter ENVISION EXP5000 J732 SELF TEST DISC IN DISCRETE OUTPUT 4 ARINC 429 OUTPUT A ARINC 429 CH 5 RX A ARINC 429 OUTPUT B ARINC 429 CH 5 RX B...

  • Page 74: System Interconnect, Garmin 430S

    Installation Manual P/N 600-00141-010 REV 6 E.15 System Interconnect, Garmin 430s Table 25: J732 Pin Assignments Pin Name ARINC 429 CH 0 TX A ARINC 429 CH 0 TX B Shield ARINC 429 CH 1 RX A ARINC 429 CH 1 RX B Shield ARINC 429 CH 2 RX A ARINC 429 CH 2 RX B...

  • Page 75: Table 27: Ch 1/Ch3 (Gns430 Gps Arinc429 Messages)

    Installation Manual P/N 600-00141-010 REV 6 ARINC channels 0-5 are low speed. Channels 6 and 7 are high speed. Note: Table 27: CH 1/CH3 (GNS430 GPS ARINC429 Messages) Label Message 074G DATA RECORD HEADER 075G ACTIVE WPT TO/FROM 100G SELECTED COURSE 113G CHECKSUM DESIRED TRACK...

  • Page 76: Table 28: Ch 2/Ch4 (Gns430 Vhf Arinc429 Messages)

    Installation Manual P/N 600-00141-010 REV 6 Table 28: CH 2/CH4 (GNS430 VHF ARINC429 Messages) Label Message 034G FREQ LOC DEV GS DEV VOR RADIAL - 68 -...

  • Page 77: Appendix F: System Interconnect, S-Tec 55X

    Installation Manual P/N 600-00141-010 REV 6 Appendix F: System Interconnect, S-TEC 55X Table 29: S-Tec 55 or 55X System Interconnect (See Figure 21 through Figure 24) A/P Mode & Wiring Source Wiring Data Description Signal Destination Heading – PFD: Autopilot: Mag Heading is combined with Heading Bug to create Heading Bug Heading Datum.
  • Page 78 Installation Manual P/N 600-00141-010 REV 6 Table 29: S-Tec 55 or 55X System Interconnect (Continued)(See Figure 21 through Figure 24) A/P Mode & Wiring Source Wiring Data Description Signal Destination Nav – ILS Active PFD P732-56 Autopilot: The Loc Active signal is an open collector discrete output from the PFD to the autopilot.
  • Page 79 Installation Manual P/N 600-00141-010 REV 6 Table 29: S-Tec 55 or 55X System Interconnect (Continued)(See Figure 21 through Figure 24) A/P Mode & Wiring Source Wiring Data Description Signal Destination All Modes PFD: Autopilot: The annunciator data from the autopilot to the PFD is a Annunciator proprietary serial 3 wire clocked data containing 17 bits.

  • Page 80: Table 30: Ch7 Transmit (Adahrs And Gpss/Nav Messages) P/N 700-00006-000/-002

    Installation Manual P/N 600-00141-010 REV 6 ARINC channels 0-5 are low speed. Channels 6 and 7 are high speed. Note: Table 30: CH7 Transmit (ADAHRS and GPSS/Nav Messages) P/N 700-00006-000/-002 Name Label Format Transmit Interval Pressure Altitude ARINC 429 BNR 100 to 167 ms Magnetic Heading ARINC 429 BNR...

  • Page 81: Appendix G: System Interconnect, S-Tec 65 Autopilot

    Installation Manual P/N 600-00141-010 REV 6 Appendix G: System Interconnect, S-Tec 65 Autopilot Table 32: S-Tec 65 Autopilot System Interconnect (See Figure 25 through Figure 27) A/P Mode & Wiring Source Wiring Data Description Signal Destination Heading – PFD P733-26 RFGC Pin 19: Mag Heading is combined with Heading Bug to create Heading Bug...
  • Page 82 Installation Manual P/N 600-00141-010 REV 6 Table 32: S-Tec 65 Autopilot System Interconnect (See Figure 25 through Figure 27) (Continued) A/P Mode & Wiring Source Wiring Data Description Signal Destination Nav – CDI Flag PFD P732-17 RFGC Pin 24: The PFD transmits a discrete level DC signal to the autopilot DISCRETE OUT 0 NAV FLAG HI that represents validity of CDI.

  • Page 83: Appendix H: System Interconnect - External Air Data Module

    Installation Manual P/N 600-00141-010 REV 6 Appendix H: System Interconnect - External Air Data Module The following table identifies the labels that the EXP5000 expects from an external ADM (Air Data Module). Table 33: CH 4 External Air Data Module Name Label Format...

  • Page 84: Appendix I: System Interconnect, Adf

    Installation Manual P/N 600-00141-010 REV 6 Appendix I: System Interconnect, ADF Table 34: ADF System Interconnect, KR-87 with Shadin 933752-000 (See Figure 28) Signal Wiring Source Wiring Destination Data Description ADF ARINC 429 Shadin Receive ARINC 429 label(s) Port J1-4 J732-46 162 ADF Bearing ARINC 429 OUTPUT A...
  • Page 85 Product. Any Product that has been repaired by Avidyne or replaced by Avidyne under this warranty will be subject to remainder of the original warranty term applicable to the repaired or replaced Product or will be warranted under the warranty terms above for ninety days from the date of repair or replacement, whichever period is longer.
  • Page 87 AVIDYNE CORPORATION 55 Old Bedford Road Lincoln, MA 01773 Telephone: 781-402-7400 Toll Free: 800-AVIDYNE (800-284-3963) FAX:781-402-7599 www.avidyne.com P/N 600-00141-010 REV 6 September 11, 2012...