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BENDIXKing KSN 8 Series Installation Manual

Aeronav aml stc installation manual for helicopters
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Honeywell International, Inc.
9201-B San Mateo Blvd N.E.
Albuquerque, New Mexico 87113 U.S.A.
Telephone: 855-250-7027 (Toll Free U.S.A./Canada)
Telephone: 602-365-7027 (International Direct)
KSN 780/8XX/900 AERONAV AML STC
INSTALLATION MANUAL FOR HELICOPTERS
Document P/N 89000046-014 Rev 0
November 2019
Export Control
This document contains technical data and is subject to U.S. export regulations. These
commodities, technology, or software were exported from the United States in accordance
with the export administration regulations. Diversion contrary to U.S. law is prohibited.
ECCN: 7E994
© Honeywell International Inc. Do not copy without express permission of Honeywell.

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  • Page 1 Honeywell International, Inc. 9201-B San Mateo Blvd N.E. Albuquerque, New Mexico 87113 U.S.A. Telephone: 855-250-7027 (Toll Free U.S.A./Canada) Telephone: 602-365-7027 (International Direct) KSN 780/8XX/900 AERONAV AML STC INSTALLATION MANUAL FOR HELICOPTERS Document P/N 89000046-014 Rev 0 November 2019 Export Control This document contains technical data and is subject to U.S.
  • Page 2 Blank Page...
  • Page 3 3. Changes to this manual are provided to users who have registered via the website to receive updates. BendixKing Customer Support If you need to speak to personnel about Technical matters, the BendixKing Customer Support team provides 24/7 customer service. Telephone: 855-250-7027 (Toll Free U.S.A./Canada) •...
  • Page 4 RECORD OF REVISIONS NOTE: The revision level for every page of this document will be updated during the revision process. A list of effective pages is, therefore, not required. Revision Revision Date Description 12 November 2019 Initial Release 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page T-4 ©...
  • Page 5 The content contained herein is proprietary to the manufacture. The applicable STCs are associated with both the BendixKing and Manufacture part numbers cross-referenced in the table below. BENDIXKING/MANUFACTURE PART NUMBER CROSS-REFERENCE BendixKing Manufacture Product Description Part Number Part Number 89000039-003...

  • Page 6: Table Of Contents

    Databases ........................1-10 1.10 Fault Detection and Exclusion (FDE)................1-10 1.11 Part 27 Helicopter STC Approved Model List ..............1-12 1.12 BendixKing Supplied Material ..................1-13 1.12.1 Product Ship Kits ..................... 1-13 1.12.2 Optional Ship Kits ....................1-13 1.13 Materials Required but not Supplied ................1-14 2.
  • Page 7 3. Antenna Installation ..............3-1 Antenna Bonding ....................... 3-1 Antenna Environmental Qualifications ................3-1 GPS Antenna ........................3-1 3.3.1 GPS Antenna Location ....................3-2 3.3.2 GPS Antenna Bonding ....................3-5 3.3.3 GPS Antenna Cable ....................... 3-5 3.3.4 GPS Coaxial Cable Connector ..................3-5 3.3.5 Approved GPS Antennas ....................
  • Page 8 Shield Grounds ........................4-1 Wire Harness Overbraid ....................4-1 4.5.1 Existing Equipment ....................... 4-1 4.5.2 Severe Lightning Transient Environment ..............4-1 4.5.3 Copper Overbraid Installation ..................4-2 AeroNav XXX Connectors ....................4-2 Byteflight Digital Data Bus Consideration – Dual AeroNav Installations ......4-2 4.7.1 Databus Wiring - Replacement Installations ..............
  • Page 9 6.1.4 P1050 Additional I/O Connector ................... 6-5 6.1.5 Altitude Gray Code ......................6-6 6.1.6 Heading Input ....................... 6-7 6.1.7 Main Course Deviation Indicator Output ..............6-7 6.1.8 Serial Data ........................6-10 6.1.9 ARINC 429 ........................6-10 6.1.10 ARINC 453 ....................... 6-13 6.1.11 RS170 Video ......................
  • Page 10 7.5.3 RS-232 Port Configuration (Page 2) ................7-8 7.5.4 Main System Configuration (Page 3) ................7-12 7.5.5 Main Input Configuration (Page 4)................7-15 7.5.6 Main Lighting Configuration (Page 5) ................. 7-16 7.5.7 Main Discrete I/O (Page 6) ..................7-20 7.5.8 Main CDI/OBS Config Page (Page 7) ................
  • Page 11 7.6.14 Self-test Page ......................7-45 7.6.15 Dual AeroNav XXX Configuration ................7-46 7.6.16 Heading Interface Check ..................7-46 7.6.17 ADS-B Output ......................7-46 8. Flight Checks ................8-1 GPS Verification ......................... 8-1 VHF COM Flight Check ....................... 8-1 VOR Flight Checks ......................8-1 ILS Flight Checks ........................
  • Page 12 Notes to Installers: The following important issues regarding the BendixKing 780/8XX/900 AeroNav GPS/NAV/COM System installation should be noted during the planning stages. 1. These installation instructions assume that the GPS/NAV/COM transceiver can be installed in a structurally sound manner in accordance with the installation manual and AC 43.13-( ).

  • Page 13: General Information

    1. General Information 1.1 Introduction This manual contains information about the physical, mechanical, and electrical characteristics of the BendixKing 780/8XX/900 AeroNav GPS/Navigation/Communication, and provides installation instructions for its components. 1.2 Applicability This manual applies to the following part numbers in Table 1 and Table 2...
  • Page 14 Model Number Hardware Part Software Part Number Number (or later approved revision) ACR: 530-00240-001 Rev. 00 • 510-00340-000 Rev. 00 • 510-00341-000 Rev. 00 • 510-00310-000 Rev. 00 • 510-00311-001 Rev. 00 • 510-00312-005 Rev. 00 AeroNav 780 (Black Bezel) 700-00179-710 •...

  • Page 15: Unit Modifications

    1.3 Unit Modifications The following tables list the hardware modifications since initial release of the AeroNav 900 and AeroNav 800. The AeroNav 880 and AeroNav 780 do not have any unit modifications at the time of this revision. Modification Change Hardware PN Hardware Software...
  • Page 16 Electrical Requirements Voltage 9-33 VDC AeroNav 880: Current 4.4A main at 14VDC 3.0A main at 28VDC AeroNav 900: 4.4A main, 6.5A COM, 0.5A NAV at 14VDC 3.0A main, 1.0A NAV at 28VDC 3.6A @ 10W, 4.1A @ 16W COM at 28VDC Dimming Bus 28VDC/14VDC/5VDC/5VAC Cooling Requirements...
  • Page 17 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 (SIL 0 – “per hour” SUPP Navigation Accuracy Category Velocity (NAC Category 3 [< 1 m/s] ADS-B installations should use a NACv of 1 unless GPS tests support a higher category.
  • Page 18 1.4.1.5 AeroNav 880/900 Installed Unit Weight in Pounds Installed Weight Without Installed Weight with Backshells Unit Unit Weight Backshells (Less Wiring) (Less Wiring) AeroNav 5.65 8.17 8.64 AeroNav 6.75 9.51 10.32 Table 9 AeroNav Installed Weights 1.4.1.6 AeroNav 900 VHF Navigation Specification Glideslope Receiver 0 +/-.0091 ddm w/ test signal varied +/-17kHz.

  • Page 19: Aeronav 780/800 Specifications

    1.4.2 AeroNav 780/800 Specifications The AeroNav 780/800 unit has the following characteristics: 1.4.2.1 AeroNav 780/800 Physical and Electrical Specifications Physical Specifications Bezel Height 2.66 inches (67 mm) Bezel Width 6.25 inches (159 mm) Depth (w/Connectors) 11.00 inches (279 mm) Weight Table 12 AeroNav Installed Weights Connectors (Aircraft Mating Connector) P1001 - 78-position High Density D-Subminiature...
  • Page 20 1.4.2.3 AeroNav 780/800 Display Specifications Display Size 4.8 inches diagonal Active Area 4.53 inches (w) x 1.70 inches (h) Resolution 640x480 pixels Viewing Angle AeroNav 780/800 Designed and Tested Limits: Left/Right: 45° 35° Down: 35° LCD Specification: Left/Right: 80° 80° Down: 60°...
  • Page 21 1.4.2.5 AeroNav 800 VHF Communication Transceiver Specifications Audio Output 65 mW into 150Ω load Audio Response <6dB Variation from 350 to 2500 Hz, 4kHz -18dB AGC Characteristics <6dB Variation from 10uV to 10mV Sensitivity 4uV (6dB (S+N)/N 30% mod @ 1KHz) 10mV spurious signal produces no more output than a desired Spurious Response signal at 6dB (S+N)/N...

  • Page 22: Power Requirements

    1.5 Power Requirements The AeroNav XXX is capable of operating from 9-33 VDC. The following table shows the maximum current requirements for 14VDC and 28VDC aircraft electrical systems. Voltage 14VDC 28VDC Main Power AeroNav 4.4A 3.0A 900/880/800/780 COM Power 10W* 6.5A 3.6A COM Power 16W*...
  • Page 23 Title Type/Categories Number Traffic Alert and Collision Avoidance System TSO-C118a (TCAS) Airborne Equipment, TCAS I Devices that Prevent Blocked Channels Used TSO-C128a* in Two-Way Radio Communications Due to Unintentional Transmissions Stand-Alone Airborne Navigation Equipment Using the Global Positioning System (GPS) Augmented by the Wide Area Augmentation TSO-C146d System (WAAS).Airborne Supplemental...

  • Page 24: Tso Deviations

    1.6.2 TSO Deviations Deviation(s) 1. Environmental qualification performed TSO-C34e - ILS Glideslope Receiving Equipment in accordance with DO-160G rather than DO-160B. 1. Environmental qualification performed TSO-C36e - Airborne ILS Localizer Receiving in accordance with DO-160G rather than Equipment DO-160B. 1. Environmental qualification performed TSO-C40c - VOR Receiving Equipment in accordance with DO-160G rather than DO-160B.

  • Page 25: Non-Tso Functions

    Deviation(s) 1. The AeroNav XXX map does not place a TSO-C147a – Traffic Advisory System (TAS) range ring at 2 NM from the own aircraft Airborne Equipment symbol when a display range of 10 NM or less is selected; 1. Smoothing and scaling algorithms at TSO-C157a –...

  • Page 26: Partial Tso Functions

    1.6.4 Partial TSO Functions The following AeroNav XXX TSOs are partial function: Description Comment Fuel Flowmeters Display Only TSO-C44c Airborne Passive Thunderstorm Detection Display Only TSO-C110a Equipment Traffic Alert and Collision Avoidance System Display Only TSO-C118a (TCAS) Airborne Equipment, TCAS I Traffic Advisory System (TAS) Airborne Display Only TSO-C147a...

  • Page 27: Environmental Qualification Forms

    Component Function DO-178B Design Assurance Level GPS Navigation Checklist Fuel Display Charts (N/A for AeroNav 880/905/780) Timers/Schedulers Calculators Maintenance Mode Airborne Weather Radar Display of External Video Data to ADS-B Out Table 22 DO-178B Software Design Assurance Levels 1.8 Environmental Qualification Forms The environmental Qualification for the AeroNav XXX is listed in Appendix A: Environmental Qualification Form.
  • Page 28 TSO-C146d compliant antenna equipped aircraft that experience a WAAS • failure or when operating outside of SBAS coverage areas; • Non-TSO-C146d compliant antenna equipped aircraft (e.g. TSO-C129a only compliant systems) when operating in Oceanic and Remote airspace, Enroute and Terminal airspace, or during any LNAV/VNAV, LP, or LPV approach.

  • Page 29: Part 27 Helicopter Stc Approved Model List

    1.11 Part 27 Helicopter STC Approved Model List The aircraft listed on the Part 27 Helicopter Approved Model List STC are eligible to install the AeroNav XXX. However, the installer must determine if the installation is in compliance with the limitations stated in the STC and this manual.

  • Page 30: Bendixking Supplied Material

    1.12 BendixKing Supplied Material The following Helicopter Ship Kits are available for ordering from BendixKing. The Part 23 fixed wing ship kits are listed in the KSN 780/8XX/900 AeroNav AML STC Installation Manual 89000046-013. Note: Ship Kit content and/or Part numbers may change without notice, verify before ordering.

  • Page 31: Materials Required But Not Supplied

    Component Ship Kit GPS Antenna 89000046-010 Table 28 GPS Antenna Kit Component Ship Kit ByteFlight Cable, 89000046-011 20 ft. Table 29 ByteFlight Ship Kit 1.13 Materials Required but not Supplied The AeroNav XXX will require common installation supplies. The following items may be required for installation, but not supplied: •...

  • Page 32: Installation Considerations

    Note: If the unit being replaced was an HTAWS-enabled device used for 91/135 HTAWS compliance, the AeroNav XXX cannot be installed without a separately installed HTAWS unit. BendixKing TA/FLTA is not an approved TSO-C194 HTAWS unit. All installations must verify the aircraft complies with Section 2.4.1 after completing the AeroNav XXX installation.

  • Page 33: Optional Installation Features

    2.2 Optional Installation Features This section summarizes optional features that may require extra wiring. Feature Description Reference Section for Installation Details Audio Panel Aurals Allows AeroNav XXX produced aural alerts (e.g. FLTA Section 6.6 terrain alerts, Top of Descent alerts, 500’ callouts, etc) to be heard in the headsets.

  • Page 34: Aeronav Xxx Interfaces

    The AeroNav XXX can interface with a host of other avionics equipment. The following list represents the proven interfaces. There may be other devices that can be configured the same as one on the below list but BendixKing has not tested it and can therefore not make any compatibility claims. Category...
  • Page 35 Category Vendor Model Displays Garmin MX20 Garmin GMX200 Garmin GPSMAP 195 Garmin GPSMAP 295 Garmin GPS III Pilot Garmin GPSMAP 196 Garmin GPSMAP 296 Garmin GPSMAP 396 Garmin GPSMAP 496 Garmin GPSMAP 695 Garmin GPSMAP 696 Garmin Aera 796/795 Argus 3000 Argus 5000...
  • Page 36 Category Vendor Model Shadin 91204XT(38)D and 91204XT-D “Miniflo-L” Digital Fuel Mgmt Systems Shadin 91802-() “DigiData” Fuel/Airdata EDM-700 Engine Monitor EDM-760 Engine Monitor FS-450 ARNAV FC-10 ARNAV FT-10 FP-5L CGR-30P Insight GEM 3 Traffic SKY497 SkyWatch SKY899 SkyWatchHP Bendix King KTA-870 Bendix King KTA-970 Bendix King...
  • Page 37 Category Vendor Model Avidyne TWX670 (“Native” format) Datalink Garmin GDL-69/69A*** Avidyne MLB700/100 AV-300/350 Heads-up Technologies XMD076 Miscellaneous Garmin GAD42 Interface Adapter EGPWS Bendix King KGP560 Bendix King KN 61 Bendix King KN 62/62A Bendix King KN 63 Bendix King KN 64 Bendix King KN65 Bendix King...
  • Page 38 Category Vendor Model Century NSD 360A Century NSD 1000 Collins 331A-6P Collins 331A-9G Collins PN-101 Mid Continent MD 222-402/-406 Mid Continent MD 200-20X/-30X STec ST 180 Sperry RD444 Sperry RD 550A Sperry RD 650 Bendix King KI 229 Bendix King KNI 582 Bendix King KDA 692...

  • Page 39: Minimum System Configuration For Vfr

    Category Vendor Model Narco Not specified Pointer 3000 Kannad Not specified Radar Bendix King RDR 2000 * Avidyne Skytrax100 (formerly MLB100) Avidyne SkyTrax100B* Freeflight Systems FDL-978-RX** Garmin GDL 88** * AeroNav Software version 10.2 or higher ** AeroNav Software version 10.2.1 or higher *** Compatibility with P/N 011-00986-00 or 011-00987-00 only pre software 10.2.3.1.

  • Page 40: Pre-Installation Checklist

    2.5 Pre-Installation Checklist Prior to beginning installation of the AeroNav XXX, complete the following pre-installation checklist. This checklist will help in determining installation requirements. If the Installation Items below are not complete, additional installation approval may be required. Installation Item Reference AeroNav AeroNav...

  • Page 41: Antenna Installation

    3. Antenna Installation This section describes the installation of the GPS, NAV, and Glideslope antennas on unpressurized, metallic fuselage helicopters. The installer is responsible to ensure the structural aspects of the installation meet all regulatory requirements and are adequate for the aircraft type. Antenna installations on helicopters are beyond the scope of this manual and a separate installation approval is required.

  • Page 42: Gps Antenna Location

    Doubler Fabrication: Doubler material is to be 2024-T3 clad aluminum per AMS QQ-A- • 250/5 Form the doubler to match the fuselage curvature • Etch, alodine, and prime the doubler per the guidance provided in • AC43.13-1B Drill holes and install rivets per AC43.13-1B •...
  • Page 43 3.3.1.1 Aircraft Lightning Zone If installing an Avidyne GPS Antenna (Avidyne Part Number 200-00282-000), the GPS antenna is qualified to be installed in an aircraft lightning zone 2A or 3 as defined by SAE ARP5414A and RTCA DO-160G. The GPS antenna can be installed anywhere in a zone 2A or zone 3 area. The forward nose zone 1A or 1B the No Installation Area can be determined using Figure 1 Distance to Aircraft Lightning Zone 2A.
  • Page 44 Example: For example, if a helicopter shown in Figure 2 has a V of 175 KIAS, the No Installation Area will be 7.2 feet. This is shown on Figure 1 Distance to Aircraft Lightning Zone 2A. with a dotted line and Figure 2 with d1 and d2 areas. Figure 2 Helicopter Lightning Zone Note: Locating the GPS antenna in the correct aircraft lightning zone is the responsibility of the installing agency.

  • Page 45: Gps Antenna Bonding

    3.3.2 GPS Antenna Bonding The GPS Antenna should have ≤ 2.5 milliohm resistance to the helicopter fuselage. 3.3.3 GPS Antenna Cable The GPS Antenna Cable must be RG-142B, RG-400, or an equivalent 50Ω 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.

  • Page 46: Gps Interference

    must be selected as “Non-WAAS”. This will result in the FMS functionality of the AeroNav XXX inhibiting selection of any WAAS (SBAS) approach in the database. Installing a new GPS antenna listed in Table 34 requires additional structural approval beyond the scope of this manual.

  • Page 47: Voltage Standing Wave Ratio

    3.4.4 Voltage Standing Wave Ratio The VSWR should not exceed 2:1 over the VHF communication radio frequency range. A VSWR over 2:1 may result in loss in transmitting power up to 50%. 3.4.5 VHF Antenna The VHF Communication Antenna should meet one of the following Technical Standard Orders (TSO): TSO-C37( ), TSO-C38( ), TSO-C169( ).

  • Page 48: Electrical Installation

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

  • Page 49: Copper Overbraid Installation

    The Approved Model List for the STC will indicate if an aircraft is required to install wire harness overbraid on the AeroNav XXX wiring. Note: Overbraid is not required on VFR only installations as defined in Section 2.4.1. 4.5.3 Copper Overbraid Installation The copper overbraid, if required, must be a minimum 90% optical coverage per ASTM-B-33.

  • Page 50: Databus Wiring - New Installations

    4.7.2 Databus Wiring – New Installations For all new installations of dual AeroNavs (not replacing pre-existing GNS4xx/5xx systems), the recommended wiring for the RS-485 data protocol is shielded twisted- pair cable with an approximate characteristic impedance of 100-120 Ohms. The wire material must meet 14 CFR 27.1359 (c). 4.8 Circuit Protection Circuit Breakers must be installed in a location easily accessible to the pilot and must be resettable trip free devices.

  • Page 51: Electrical Load Analysis

    If installing a 3rd party NAV and/or COM and AeroNav XXX, connect the AeroNav XXX as shown in Figure 5. Preferred Alternate Avionics Bus 1 Avionics Bus 2 Main Bus Avionics Bus AeroNav 800/900 Other COM/NAV AeroNav 800/900 Other COM/NAV Aircraft Ground Aircraft Ground Aircraft Ground...

  • Page 52: Mechanical Installation

    AC 43.13-2B, Chapter 11, Paragraph 1104(a). 5.1.3 Requirements for Tray Installation The BendixKing Tray must be installed in the aircraft as described below in order to satisfy the structural requirements for the STC. Deviations to these requirements will require separate approval.

  • Page 53: Equipment Location - Replacement Unit

    b. If new forward support brackets are fabricated, the fabrication methods must follow the requirements of either Figure C - 1 or Figure C - 2, FAA Advisory Circular 43.13-1B, Chapter 4 for general airframe fabrication criteria, including hole tolerances, edge distances, rivet spacing, and corrosion protection, and Advisory Circular 43.13-2B, Chapters 2 and 11 for structural adequacy.

  • Page 54: Electrical Bonding

    Note the hottest source(s) on that page and supply that information to BendixKing Technical Support to include both the source and the associated temperature for follow-on guidance. The metal bezel of the AeroNav XXX is intentionally designed to radiate heat away from the internal components and out of the unit.

  • Page 55: System Installation

    6. System Installation The following section will describe interfacing the AeroNav XXX to various other avionics and aircraft equipment. 6.1 Pin Function List The following Section Lists the Pin function for each connector. 6.1.1 P1001 Main Connector Description Signal Type VLOC Annunciate Output GPS Annunciate...
  • Page 56 Description Signal Type Main +Down Output Main Vertical +Flag Output Main Vertical -Flag (GND) Main OBS Rotor C Output Main OBS Rotor H(GND) Main OBS Stator D Input Main OBS Stator E (2.5V Common OBS) Output Main OBS Stator F Input Main OBS Stator G (2.5V Common OBS) Output...

  • Page 57: P1002 Communication Connector

    Description Signal Type Altitude C2 Input Altitude C1 Input Altitude B4 Input Altitude B2 Input Altitude B1 Input Altitude A4 Input Altitude A2 Input Altitude A1 Input Altitude D4 / Weight on Wheels (WOW) Input Input OBS Mode Select Input Aircraft Power 2 Input CDI Source Select...

  • Page 58: P1006 Navigation Connector

    Pins Description Signal Type Intercom Microphone Audio LO Input COM Microphone Audio LO Input COM Audio LO Output Reserved Aircraft GND Aircraft GND Synchro Y Input Synchro Z Input Synchro Reference Signal - Input Table 38 P1002 Pin Description 6.1.3 P1006 Navigation Connector Note: This connector is not used in the AeroNav 880/905/780.

  • Page 59: P1050 Additional I/O Connector

    Pins Description Signal ILS Energize Output Glideslope +Flag Output Glideslope +Down/-Flag (Glideslope 2.5V Common) Output Glideslope +Up Output Parallel DME - 1MHz Output Com Monitor Audio LO Output VOR/ILS Arinc-429 In B Input VOR/ILS Arinc-429 In A Input Parallel DME - 800KHz Output Glideslope Superflag Output...

  • Page 60: Altitude Gray Code

    Pins Description Signal GPS ARINC-429 Out 2B Output VOR/ILS ARINC 429 OUT 3A** Output VOR/ILS ARINC 429 OUT 3B** Output 46-59 NO CONNECT RS232 Out 5 Output RS232 IN 5 Input RS232 Out 6 Output RS232 IN 6 Input Ground 65-76 NO CONNECT RS170 Video IN...

  • Page 61: Heading Input

    6.1.6 Heading Input Note: This section is N/A for the AeroNav 880/780. The AeroNav XXX can accept a 3-wire ARINC 407 Synchro heading input on the following connectors and pins: Description Connector Signal Type Synchro X P1002 Input Synchro Reference Signal + (26VAC P1002 Input 400 Hz)
  • Page 62 6.1.7.3 Navigation Flags The Navigation Flags is on the following connector and pins: Description Connector Signal Type Main Lateral +Flag P1001 Output Main Lateral -Flag P1001 Output Main Vertical +Flag P1001 Output Main Vertical -Flag P1001 Output Table 45 Main Navigation Flag Output 6.1.7.4 Navigation Superflags The Navigation Superflags is on the following connector and pins: Description...
  • Page 63 6.1.7.6 Annunciators Electrical Output Description Connector Signal Type VLOC Annunciate P1001 Output GPS Annunciate P1001 Output Waypoint Annunciate P1001 Output Terminal Annunciate P1001 Output Approach Annunciate P1001 Output Message Annunciate P1001 Output OBS Annunciate P1001 Output Integrity Annunciate P1001 Output LNAV GPS Select P1001 Output...

  • Page 64: Serial Data

    6.1.8 Serial Data 6.1.8.1 RS-232 Description Connector Signal Type RS-232 Output 1 P1001 Output RS-232 Input 1 P1001 Input RS-232 Output 2 P1001 Output RS-232 Input 2 P1001 Input RS-232 Output 3 P1001 Output RS-232 Input 3 P1001 Input RS-232 Output 4 P1001 Output RS-232 Input 4...

  • Page 65: Arinc 453

    6.1.9.1 GPS ARINC Output The data output on the GPS ARINC out port depends on the configuration of the unit. Below is a list of configurations and label outputs for each: 1. ARINC 429 2. GAMA 429 3. GAMA 429 Graphics 4.
  • Page 66 Label Number Parameter Name Lateral Scale Factor • • • • • • Vertical Scale Factor • • • • • Conic Arc Inbound Course • • Conic Arc Radius • • Conic Arc Course Change Angle • • Airport Runway Azimuth •...

  • Page 67: Rs170 Video

    6.1.9.4 ARINC 743A Output Label Number Parameter Name MSL Altitude Track Angle Latitude Longitude Ground Speed Latitude, Fine Longitude, Fine Greenwich Mean Time VFOM UTC Time of Fix Fine UTC Time of Fix From GPS Vertical Velocity North-South Velocity East-West Velocity Pressure Altitude Horizontal Figure of Merit (HFOM) Date...

  • Page 68: Com/Vor/Ils Audio Electrical Characteristics

    6.1.12 Com/VOR/ILS Audio Electrical Characteristics Note: This section is N/A for AeroNav 880/780. 6.1.12.1 Com Microphone Key Description Connector Signal Type P1002 COM MIC Key Input Table 55 VHF Communication Microphone Key This input is active if either the voltage to ground <1.9V or the resistance to ground is <375Ω. This input is considered inactive if the voltage to ground is 11-33 VDC.

  • Page 69: Vor/Ils Indicator Electrical Characteristics

    6.1.12.5 Standby Com Monitor Description Connector Signal Type Com Monitor Audio HI P1006 Output Com Monitor Audio LO P1006 Output Table 59 Standby Communication Output This optional signal use can be used with audio panels that have a means of selecting the #1 standby com audio (e.g.

  • Page 70: Bezel Lighting

    6.1.14.1 Serial/Parallel Tuning Description Connector Signal Type NAV PAR DME – 8MHz P1006 Output SER DME – CHAN REQ/PAR DME – 4MHz P1006 Output* SER DME – RNAV MODE/PAR DME – 2MHz P1006 Output* NAV PAR DME – 1MHz P1006 Output NAV PAR DME –...

  • Page 71: Traffic System

    6.3 Traffic System The AeroNav XXX can be connected to Traffic Systems either by RS232 or ARINC 429. The AeroNav XXX supprts the following Traffic Systems: Manufacturer Model Data Notes Format RS232 or Avidyne Corporation TSA6XX, TAS6XXA, 9900BX RS-232 preferred ARINC 429 Skytrax100 RS232 or...

  • Page 72: Datalink Weather

    6.5 Datalink Weather The AeroNav XXX can be connected to Datalink Weather Systems via RS232. The AeroNav XXX supports the following Datalink Weather Systems: Manufacturer Model Data Notes Format MLB700 RS232 Avidyne Corporation SkyTrax100 RS232 AeroNav with s/w (formerly MLB100) [Navworx 200-0011-()-()] 10.1.0 or later Skytrax 100B...

  • Page 73: Gad 42

    6.7 GAD 42 The AeroNav XXX can be connected to the Garmin GAD42 Interface Adapter. If the AeroNav XXX is replacing a GNS530/W or GNS430/W that had previously been connected to a GAD42, then no action is required since the configuration is already saved in the GAD42. If this is a new installation of an AeroNav XXX (i.e.

  • Page 74: Heading System Sources

    Collins AHS-85E ARINC 429 High Speed Table 70 IRU/AHRS Systems The BendixKing AeroNav XXX can accept heading information via ARINC 429 from other IRU/AHRS sources if the following labels are provided: 314 - True Heading • • 320 - Magnetic Heading IRU/AHRS not listed in the table above can still be approved if the following conditions are met: •...

  • Page 75: Multifunction Displays

    6.10 Multifunction Displays The AeroNav XXX can be connected to Multifunction Display Systems via RS232 or ARINC 429. The AeroNav XXX supports the following Multifunction Display Systems: Manufacturer Model Data Format Notes • Aviation No Alt format for MX20 version 5.5 and earlier Garmin MX20...
  • Page 76 installation, the transponder system must be tested per 14 CFR 91.411 to verify the airdata retransmitted by AeroNav XXX is operating correctly prior to return to service. The Hardware and Software Design Assurance for the Altitude Retransmission is Level B and C respectively. The AeroNav XXX has a maximum internal latency of 340 mS for retransmission the altitude data.
  • Page 77 service. The AeroNav XXX will use the airdata source with the highest priority, reference Section 6.8.1.1. Installers must ensure the airdata source being used for transponder Mode C transmissions complies with 14 CFR 91.217. After installation, the transponder system must be tested per 14 CFR 91.411 to verify the airdata retransmitted by AeroNav XXX is operating correctly prior to return to service.
  • Page 78 accept an active low on ground when performing that squat switch setup. • The NGT9000XX needs a pressure altitude input • The NGT9000XX has its own internal GPS receiver See Figure D-66 for NGT9000 interconnect • AeroNav XXX must have software 10.2.3.1 or later for the •...

  • Page 79: Video Input

    service. The AERONAV XXX will use the airdata source with the highest priority, reference Section 6.8.1.1. Installers must ensure the airdata source being used for transponder Mode C transmissions complies with 14 CFR 91.217. After installation, the transponder system must be tested per 14 CFR 91.411 to verify the airdata retransmitted by AERONAV XXX is operating correctly prior to return to service.

  • Page 80: Configuration And Checkout

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

  • Page 81: Unit Installation

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

  • Page 82: Arinc 429 Port Configuration

    7.5.2 ARINC 429 Port Configuration The ARINC 429 can be selected individually for each ARINC 429 Transmit and Receive Port. Each Transmit and Receive Port will have a “Speed” selection and “Data” selection. Figure 7 AeroNav 880/900 ARINC 429 Configuration Page Note: Shown is the AeroNav 780/800 ARINC 429 Config Page.
  • Page 83 The “Data” will have the following INPUT options: Selection Description No device connected to this ARINC 429 input Airdata Altitude, temperature, and speed information from the following Air Data Systems: B&D 2600, 2601, 2800, 90004-003, Bendix/King KAD 280/480, Shadin ADC 2000 Airdata/AHRS Heading, altitude, temperature, and speed information from an Air Data/AHRS system.
  • Page 84 Aspen EFD1000 (If connected to an ACU1, set the ARINC 429 speed to low speed. If connected to an ACU2 and using ADF, RADALT or Remote OAT data set the ARINC 429 speed to high speed, otherwise low speed.) Honeywell Primus 1000 Avidyne EXP5000* INS/IRU Heading information from the following Inertial systems:...
  • Page 85 The “Data” will have the following OUTPUT options: Selection Description No device(s) connected to ARINC 429 output ARINC 429 Standard ARINC 429 output (non-GAMA) GAMA 429 ARINC data as define by the General Aviation Manufacturers’ Association (GAMA) General Aviation Subset, 2 Edition.
  • Page 86 Selection Description GAMA 429 Non- ARINC 429 data that is not necessarily conforming to the GAMA General standard Aviation Subset, 2 Edition. ARINC 743A ARINC 429 - 743A labels Onboard Radar Honeywell RDR2000 Table 79 ARINC 429 Output Selection Note: It is important in dual AeroNav installations that the corresponding SDI selection be made properly.

  • Page 87: Port Configuration

    7.5.3 RS-232 Port Configuration The RS-232 Configuration Page allows the configuration Inputs and Outputs to match that of the equipment installed in the aircraft. Figure 8 RS-232 AeroNav 880/900 Configuration Page Note: Shown is an AeroNav 880/900 Main RS232 Config Page. The AeroNav 780/800 only has 4 inputs and outputs Note: If you configure Skytrax WX, Capstone Wx, MLB Wx, or WX500 on any input channel, the same numbered output channel cannot be configured with any of the following;...
  • Page 88 Selection Description GDL 69 Serial data input for in-flight access to weather and messaging from the following units: Garmin GDL69/69A P/N 011-00986-00 or 011-00987-00 only (Garmin software version 4.01 or later) pre Avidyne software 10.2.3.1. With software 10.2.3.1 and later P/N 011- 03177-X0 will also work MLB700 Serial weather data information from the Avidyne MLB700 XMD076...
  • Page 89 Selection Description Shadin-Fuel Serial fuel flow information from the following units: Shadin 91053XP and 91053XT-D “Digiflo-L” Digital Fuel Management Systems Shadin 91204XX(38)D and 91204XT-D “Miniflo-L” Digital Fuel Management Systems 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 JPI for the Garmin GNS series.
  • Page 90 Selection Description Serial position, velocity, and navigation data to the following units: Aviation no Alt Garmin MX20 (V5.5 or earlier) Horizon DDMP Insight TAS 1000 Air Data Computer AXP322 Select for Avidyne AXP322 Remote Transponder CrossSync Serial transfer of flights plans and user waypoints and cross-side data (e.g.

  • Page 91: Main System Configuration

    These Traffic receiving devices are mutually exclusive. Multiple devices should not be installed/configured on a single unit. The following RS232 Output protocols may be configured on two or more RS232 ports: Aviation, Aviation No Altitude, ADS-B (avi), HW EGPWS, and MapMx. 7.5.4 Main System Configuration This is a general page for miscellaneous configurations.
  • Page 92 GPS Select Selections: Selection Description Auto In GPS mode on the AeroNav XXX, the GPS Select discrete will not be active (open) in a GPS approach, and no messages will annunciate on the AeroNav XXX and no pilot action is required. This setting allows the pilot to use the GPS ...
  • Page 93 Checklist Selection Description Enabled Select Enabled to allow the user editable checklists to be displayed/accessible. Disabled Default setting Table 89 Checklist Setting TIS-B Annunciation Selection Description Enabled Select Enabled for installations in U.S. Disabled Outside US airspace Table 90 TIS-B Annunciations Joystick Selection Description...

  • Page 94: Main Input Configuration

    7.5.5 Main Input Configuration (Page 4) The Main Input Page displays information received from ARINC 429, RS-232, and other electrical inputs. This page is helpful during troubleshooting of the AeroNav XXX system. This is used for verifying electrical interfaces during installation and troubleshooting. Field Description Outside Air Temperature...

  • Page 95: Main Lighting Configuration

    7.5.6 Main Lighting Configuration The source of the lighting for the AeroNav XXX can be the bezel photocell sensor or the dimming bus. 28VDC, 14VDC, 5VDC and 5VAC dimming buses are all supported and are automatically detected by the AeroNav XXX. Figure 10 Main Lighting Configuration Page Photo Response Time Sets the speed at which the brightness changes when photocell is selected as the lighting source.
  • Page 96 Photo Maximum The Photo Maximum sets the maximum brightness when the dimming source is the photocell. Both the Bezel and Display fields have a range of 50 to 100, and the factory default is 100. dimBus Transition % The dimBus Transition % sets the threshold where the aircraft dimming bus takes over from the photocell.
  • Page 97 The AviCurve tracks the aircraft dimming bus as follows: Figure 11 Lighting Curve - AviCurve Figure 12 Lighting Curve - Proportional Curve 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page 7-18 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 98 Field Selection Bezel Value displayed represents the current % brightness of the bezel backlighting Display Value displayed represents the current % brightness of the display backlighting Mx Input Photocell – Maintenance Mode will use this method if selected. This is the default setting. This setting uses the Photocell on the AeroNav XXX bezel or display.

  • Page 99: Main Discrete I/O

    7.5.7 Main Discrete I/O This page will test the Main Discrete outputs on the AeroNav XXX. Figure 13 Main CDI/OBS Configuration Page Selection Verify That RMT CDI On is displayed when a remote CDI source select switch is pressed. RMT OBS On is displayed when a remote OBS switch is pressed.

  • Page 100: Main Cdi/Obs Config Page

    Selection Verify That The GPS SELECT output is on or off as selected on this page (NOTE: This output is GPS SELECT connected to the autopilot GPS SELECT input, not to an annunciation, and therefore this is for bench testing purposes only). TER CAUT The TER CAUT annunciator is on or off as selected on this page.
  • Page 101 The following parameters can be tested: CDI (LAT/VERT) Selection Description Max Left The remote CDI will be off-scale full deflection to the left/up Full Left The remote CDI will be deflected to the left/up Center The remote CDI will be centered Full Right The remote CDI will be deflected to the right/down Max Right...
  • Page 102 Ignore Options Selection Description Ignore SEL CRS for 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 Yes/No –...

  • Page 103: Vor/Loc/Gs Cdi

    7.5.9 VOR/LOC/GS CDI Note: This page is not applicable for the AeroNav 880/780. This will test the operation of the VOR/LOC/GS output from the AeroNav XXX on the P1006 connector to an external CDI/HSI display. Figure 15 CDI Test Page Note: This page currently will only test low level flags and does not support the testing of super flags CDI (LAT/VERT)
  • Page 104 SPR Flag (LAT/VRT Super Flag) Selection Description Hidden The lateral and vertical flag on the external indicator is hidden In view The lateral and vertical flag on the external indicator is in view Table 106 NAV Superflag Test Page TO-FROM Selection Description FROM...

  • Page 105: Vor/Loc/Gs Arinc 429 Configuration

    7.5.10 VOR/LOC/GS ARINC 429 Configuration Note: This page is not applicable for the AeroNav 880/780. This page will configure the ARINC 429 for the VOR/LOC/GS output. Figure 16 VOR/LOC ARINC 429 Configuration Page The following parameters can be configured. Speed: Selection Description Standard Low-speed ARINC 429...

  • Page 106: Gps Vertical Offset

    SDI: Selection Description Common RX: Accepts all 429 inputs TX: Generates all 429 outputs with SDI =0 VOR/ILS 1 Number 1 (Pilot) VOR/ILS Receiver RX: Accepts 429 inputs with SDI = 0 or 1 TX: Generates all 429 outputs with SDI = 1 VOR/ILS 2 Number 2 (Copilot) VOR/ILS Receiver RX: Accepts 429 inputs with SDI = 0 or 2...

  • Page 107: Main Arinc 429 Port 3 Configuration

    Figure 18 GPS Antenna Height 7.5.12 Main ARINC 429 Port 3 Configuration This page will configure a GLAS enabled IFD to transmit a pseudo VOR/ILS output to the flight displays and autopilot on ARINC 429 port 3. Only configure this setting if high speed VOR/ILS ARINC out is specified on the drawing.

  • Page 108: Gdl Configuration

    7.5.13 GDL Configuration Pages This page allows the configuration of the Garmin GDL 69/69A. This page is always displayed in Maintenance Mode. The GDL 69/69A must be activated prior to configuring the AeroNav XXX, reference the GDL installation manual for setup and configuration information. Figure 20 GDL Configuration Page GDL Selection Page This page selects the attenuation and the type of GDL receiver connected to the AeroNav XXX.

  • Page 109: Remote Xpdr Configuration

    7.5.14 Remote XPDR Configuration This page will configure the Avidyne AXP322 Remote transponder. Reference the AXP322 installation manual as needed. The transponder must be configured to operate. Please note; it may take up to 3 minutes to update the transponder configuration after changing a parameter below.
  • Page 110 7.5.15.1.1 Configuring the AeroNav as a WAP The factory default setting for the AeroNav, presents the AeroNav as WAP with SSID (i.e. the name of the provided network) set to "LIO_WIFI". Additionally, the default PSK (i.e. the password needed to access the Wi-Fi access point) is set to "abcdef1234".
  • Page 111 Figure 22 WiFi Configuration Page 4. Press the lower right knob 5. Using the outer right knob, advance the selection rectangle until the current Local SSID field is selected as shown: Figure 23 WiFi Configuration Page 6. Press the right knob 7.
  • Page 112 To configure the network password (PSK) 1. Boot the AeroNav to Maintenance mode. 2. Select the "Config" tab. 3. Turn the right knob until the "Wifi Configuration" Page is displayed as shown in the image below. Figure 24 WiFi Configuration Page 4.
  • Page 113 7. The inner knob can now be used to advance through the available characters. The outer knob will advance to the next character in the PSK. NOTE: One of the possible character selections is a space character. Spaces at the end of the PSK will not be contained in the final PSK.
  • Page 114 Designate the Network to Connect To: 1. Boot the AeroNav to Maintenance mode. 2. Select the "Config" tab. 3. Turn the right knob until the "Network Configuration" Page is displayed as shown in the image below. Figure 27 WiFi Configuration Page 4.
  • Page 115 To configure the network password (PSK) NOTE: This value will be supplied by the device with which you are attempting to connect. 1. Boot the AeroNav to Maintenance mode. 2. Select the "Config" tab. 3. Turn the right knob until the "Wifi Configuration" Page is displayed as shown in the image below.

  • Page 116: Bluetooth Setup

    Bluetooth devices in range of the AeroNav. NOTE: You will likely need to put the BendixKing Bluetooth keyboard into discoverable mode by pressing the button on the rear of the keyboard.

  • Page 117: Rdr2000 Radar Configuration

    7.5.17 RDR2000 Radar Configuration 7.5.17.1 Configuration Module Setup 7.5.17.2 Primary Radar Setup 1. Power on the primary AeroNav in Maintenance Mode and select the Config/Radar Calibration page. 2. Press the “Radar” LSK, then place the radar into “Test” 3. Press the Diagnostics LSK to display the diagnostics page. 4.

  • Page 118: Stormscope Test Page

    b. To increment the value of the “Roll Angle” use the left inner knob to select a “Tilt Setting” between 5 and 10. When the “Tilt Setting” is between 5 and 10, the value of the “Roll Angle” field will slowly increase. To decrement the value of the “Roll Angle”...

  • Page 119: Gad 42 Configuration

    SW Version - displays the WX-500 Main SW Version / Main Boot SW Version / DSP SW • Version Config - displays the WX-500 configuration settings (Serial Jumpers, Hdg Valid Flag, Flag • Sense, Hdg Value, Inhibit Line and Antenna Mount). Environment - displays the WX-500 environmental parameters (voltages and processor •...
  • Page 120 Figure 33 Software Version Page Figure 34 Fan Status Page 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page 7-41 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 121: Checkout

    Figure 35 AeroNav Temperature Status Page The pages on the “Diag” tab are for BendixKing Technical Support diagnostics purposes and are not described in this manual. 7.6 Checkout After configuring the AeroNav XXX, the following post-installation tasks should be performed.

  • Page 122: Electrical Load Analysis

    Since a full featured AeroNav XXX is within 5% of the weight of the removed GNS530/430 (less than 1 pound difference), no new weight and balance must actually be performed according to AC 43.13-1B Change 1 Acceptable Methods, Techniques, and Practices Aircraft Inspection and Repair (Chapter 10) and AC 120-27E Aircraft Weight and Balance Control.

  • Page 123: Vor/Loc/ Gs Checkout

    7.6.7.3 Receiver/Transmitter Operation Test VHF Com’s ability to receive and transmit to another VHF Com station. Verify using a low/middle/high frequency. 7.6.8 VOR/LOC/ GS Checkout Note: This section is not applicable for AeroNav 880/780. If installed, test the VOR/LOC/GS system using a local frequency or test set. Verify the OBS (selected course) is functioning, CDI/HSI/PFD is indicting correctly, and NAV audio is received.

  • Page 124: Self-Test Page

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

  • Page 125: Dual Aeronav Xxx Configuration

    7.6.15 Dual AeroNav XXX Configuration If installing two AeroNav XXX units, verify duplex communication between the two units. Reference Section 3.3.8 and 7.3 for limitations and configuration. 7.6.16 Heading Interface Check Verify the AeroNav XXX is receiving heading information from an external source. This can be verified on the Main Input Page in maintenance mode, reference Section 7.5.5.

  • Page 126: Flight Checks

    8. Flight Checks The AeroNav XXX must be flight tested to verify the installation is operating properly. The following items should be tested in flight to verify the AeroNav XXX function. 8.1 GPS Verification Verify the following in flight: • Verify the GPS reception during all phases of flight.

  • Page 127: Glove Validation Procedures

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

  • Page 128: Software And Database Update Procedures

    Use one of the formatted fobs supplied by BendixKing (marked by the BendixKing logo printed on one side). In the event one of those fobs are not available, either call BendixKing for a replacement fob (a nominal fee will be charged) or purchase a replacement through other means. Acceptable alternative USB drives are FAT32 format, between 1-16 GB, and manufactured by WINTEC filemate.
  • Page 129 You will be prompted to “Confirm” or “Cancel”. Assuming you selected “Confirm”, you should see a dialog box presented in the middle of the screen and all uploadable files on that fob will be individually listed and check marks may be visible next to each file name. Figure 37 Confirm and Cancel LSK Use the “Select All”, “Un-select All”...
  • Page 130 For multiple AeroNav installations, the database uploads must be performed individually for each AeroNav to be updated. Due to some of the upload durations, BendixKing recommends creating a fob for each AeroNav to be updated so that the updates can happen in parallel and not stacked serially, thereby extending the overall time to accomplish a full update.

  • Page 131: Datalogs Download

    Event Log – This log contains miscellaneous data such as all alerts, • keystrokes, system status and error messages, etc. It is designed to be diagnostics log for BendixKing Technical Support technicians and not expected to be used by owners/operators. It logs at an on-condition rate;...
  • Page 132 Download Configuration Info - This log contains the system • configuration for the unit. GPS Log - This log contains detailed internal state data for the GPS. • The “Download Logs” LSK is presented when “Software” is selected on the SYS tab and the system is not in-air.

  • Page 133: Software Update

    10.3 Software Update The following procedures should be followed when performing optional or mandatory software change to the AeroNav 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.

  • Page 134: Periodic Maintenance

    11. Periodic Maintenance The AeroNav XXX does not require any periodic or preventative maintenance. Maintenance on the AeroNav XXX is on condition. 11.1 Equipment Calibration The AeroNav XXX 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. (N/A for AeroNav 880/780) 11.3 Cleaning The front display and bezel may require cleaning periodically, reference Section 12...

  • Page 135: Bezel And Display Cleaning

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

  • Page 136: Appendix A: Environmental Qualification Form

    BendixKing requires the following for helicopter installations: Plug & Play Installations – Installer has option to use existing tray; New Installations – Installer must use BendixKing's Helicopter Tray, reference Table 26 or Table 27; Table 118 Environmental Qualification Form – AeroNav 900/880/800/780...
  • Page 137 AeroNav905, AeroNav910 (Low Temp and Vibration Categories Differ From Table 118) RTCA/DO-160G Environmental Tests Test Category Section Temperature and Altitude Equipment qualified to Category X (non-standard category) Equipment tested to C1 with Ground Survival Low limited to -40C Low Temp 4.5.2 High Temp 4.5.3 &...

  • Page 138: Appendix B: Stc Permissions

    Appendix B: STC Permissions Avidyne Corporation hereby grants to all National Aviation Authorities (FAA, CAA, JAA, etc) approved installers the use of data from STC SA00387BO to install the AeroNav XXX System. This also includes any international validations of the STC (e.g. EASA, ANAC, etc). Copies of the STC data are available on MyAerospace.Honeywell.com website Technical Publications page or upon request.

  • Page 139: Appendix C: Mechanical Drawings

    Appendix C: Mechanical Drawings Figure C - 1 AeroNav 880/900 Tray Installation....................1 Figure C - 2 AeroNav 780/800 Tray Installation....................2 Figure C - 3 AeroNav 880/900 Instrument Panel Cutout ................3 Figure C - 4 AeroNav 780/800 Instrument Panel Cutout ................4 Figure C - 5 Typical GPS Antenna Installation ....................
  • Page 140 Figure C - 2 AeroNav 780/800 Tray Installation 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page C-2 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 141 Figure C - 3 AeroNav 880/900 Instrument Panel Cutout 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page C-3 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 142 Figure C - 4 AeroNav 780/800 Instrument Panel Cutout 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page C-4 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 143 Figure C - 5 Typical GPS Antenna Installation Figure C - 6 AT-575 GPS Antenna Hole Pattern 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page C-5 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 144 Figure C - 7 AV-801 GPS Antenna Hole Pattern 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page C-6 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 145 Figure C - 8 Typical GPS Antenna Doubler Installation ‡ Fuselage Skin Adjacent Structure Doubler Thickness Outer Rivet Row in Inner Four Rivet in Thickness Rivet Type Doubler Doubler 0.016" - 0.025" Dimpled skin / 0.020" MS20426AD3 (Double MS20426AD3 (Double Countersunk Rivets Dimple) Dimple)
  • Page 146 Figure C - 9 Typical GPS Antenna Doubler 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page C-8 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 147: Appendix D: Electrical Interface Drawings

    Appendix D: Electrical Interface Drawings Figure D - 1: Lighting, Power, and Antenna Interconnect ................1 Figure D - 2: Blind Altitude Encoders Interconnect ..................4 Figure D - 3: RS-232 Serial Data Interconnect ....................5 Figure D - 4: EFIS Interconnect ........................7 Figure D - 5: Generic EFIS Interconnect ......................
  • Page 148 Figure D - 35: RDR2000 Interconnect ......................43 Figure D - 36: GTX 335 Interconnect ......................44 Figure D - 37: GTX 345 Interconnect ......................45 Figure D - 38: GTX 330ES Interconnect ......................47 Figure D - 39: Robinson Analog Interconnect ....................48 Figure D - 40: Robinson Aspen EFD100 Interconnect ...................
  • Page 149 Figure D - 1: Lighting, Power, and Antenna Interconnect Page 1 of 3 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-1 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 150 Page 2 of 3 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-2 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 151 NOTES: ALL WIRES TO BE 22 AWG OR GREATER UNLESS OTHERWISE NOTED. IF AIRCRAFT HAS MULTIPLE POWER BUSSES, IT IS RECOMENDED THAT AERONAV XXX POWER CONNECTIONS BE CONNECTED AS DESCRIBED IN SECTION 4. AIRCRAFT POWER INPUT TO THE AERONAV XXX MAY BE 9-33 VDC. THE AERONAV XXX SHOULD BE CONFIGURED FOR THE CORRECT LIGHTING BUS VOLTAGE POST-INSTALLATION.
  • Page 152 Figure D - 2: Blind Altitude Encoders Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-4 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 153 Figure D - 3: RS-232 Serial Data Interconnect Page 1 of 2 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-5 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 154 Page 2 of 2 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-6 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 155 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT AERONAV UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE – THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
  • Page 156 ARINC 429 EFIS DISPLAY #1 AERONAV XXX #1 P1001 LNAV TRANSMITTER A GPS ARINC 429 IN 1 A LNAV TRANSMITTER B GPS ARINC 429 IN 1 B GPS ARINC 429 OUT A LRN/LNAV 1 RECEIVER A LRN/LNAV 1 RECEIVER B GPS ARINC 429 OUT B LRN/LNAV 2 RECEIVER A P1006...
  • Page 157 Figure D - 6: EHSI ARINC 429 Interconnect, Dual AeroNav XXX, Sandel SN3308 Interconnect Page 1 of 2 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-9 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 158 NOTES: ALL WIRES TO BE 24 AWG OR GREATER UNLESS OTHERWISE NOTED. AT AERONAV UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE. AERONAV XXX #1 SETUP MAIN ARINC 429 CONFIG: IN 1: LOW, SANDEL EHSI OUT:...
  • Page 159 Figure D - 7: ARINC 429/RS-232 Air Data/IRU/AHRS Interconnect Page 1 of 2 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-11 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 160 NOTES: ALL WIRES TO BE 22 AWG OR GREATER UNLESS OTHERWISE NOTED. AT AERONAV UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE. THE SHIELD LEADS MUST BE LESS THAN 3.0 INCHES. CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
  • Page 161 AERONAV XXX SANDEL SN3500 P1001 31/(2) GPS ARINC 429 OUT A GPS ARINC 429 IN A GPS ARINC 429 OUT B 17/(32) GPS ARINC 429 IN B GPS ARINC 429 IN 1A GPS ARINC 429 OUT A GPS ARINC 429 IN 1B GPS ARINC 429 OUT B P1006 VOR/ILS 429 OUT A...
  • Page 162 Bendix/King KTA 870/KMH 880 KTA 970/KMH 980 P1001 AERONAV XXX GPS ARINC 429 IN 1 A CDU 429 A TX GPS ARINC 429 IN 1 B CDU 429 B TX ANNUNCIATE D TAS TEST IN ANNUNCIATE E TAS STBY L3 Communications SKY 497 AERONAV XXX P1001...
  • Page 163 CONTROL/DISPLAY UNIT IS NOT IN THE INSTALLATION, A DEDICATED SWITCH MAY BE REQUIRED TO TURN THE SKYWATCH PROCESSOR UNIT ON OR OFF. THE BENDIXKING/RYAN TAS PROCESSOR SWITCH PIN (P1-16) SHOULD BE GROUNDED TO TURN THE PROCESSOR UNIT ON, AND OPEN TO TURN THIS UNIT OFF. IF A RYAN TCAD DISPLAY UNIT IS NOT IN THE INSTALLATION, A DEDICATED SWITCH MAY BE REQUIRED TO TURN THE TAS PROCESSOR UNIT ON AND OFF.
  • Page 164 Figure D - 10: GTX 330 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-16 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 165 Figure D - 11: Terrain and Weather Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-17 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 166 Figure D - 12: Weather Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-18 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 167 AUDIO PANEL GARMIN AVIDYNE PS ENGINEERING Bendix/King SL 10 SERIES PMA 6000 KMA 24H GMA 340 GMA 347 AMX240 PMA 8000(B/BT) KMA 24 KMA 26 KMA 28 SL 15 SERIES PMA 7000 -70/-71 BOTTOM J3471 J1 (BOTTOM) BOTTOM P241 P261 J1 (BOTTOM) P241 9/(10)
  • Page 168 NOTES: ALL WIRES TO BE 22 AWG OR GREATER UNLESS OTHERWISE NOTED. CONNECTING TWO MICROPHONES TO MIC AUDIO HI/LO OR INTERCOM MIC HI/LO AT THE SAME TIME MAY RESULT IN WEAK OR DISTORTED AUDIO. MIC ISOLATION RELAYS ARE RECOMMENDED SO THAT ONLY ONE MIC IS ACTIVE AT A TIME.
  • Page 169 Navigation GARMIN Bendix/King Indicator GI 102/A GI 106/A KI 202 KI 206 KI203 KI204 KI 208 KI 209 KI 208A KI 209A P2021 P2061 P2031 P2041 P2081 P2091 P208A1 P209A1 +LEFT +RIGHT +FROM NAV +FLAG NAV -FLAG NAV SUPERFLAG NAV SUPERFLAG LO VOR/LOC COMPOSITE ILS ENERGIZE +DOWN...
  • Page 170 GARMIN S-TEC BENDIX KING CENTURY COLLINS SPERRY CONTINENT KPI 552/B NSD360A KI 525A 331A-9G RD 444 RD550A RD650 GI 102 (X) GI106 GI106A ST 180 KI 206 331A-6P PN-101 KPI 553/A/B NSD1000 Navigation Indicator P2061 P101 CD132 +LEFT +RIGHT +FROM NAV +FLAG NAV -FLAG NAV SUPERFLAG...
  • Page 171 Navigation Bendix/King Indicator KI 209A P209A1 LNAV LATERAL DEV +LT IN LNAV LATERAL DEV +RT IN LNAV +TO IN LNAV +FROM IN LNAV LATERAL +FLAG IN LNAV LATERAL -FLAG IN LNAV VERTICAL +UP IN LNAV VERTICAL +DOWN IN LNAV VERTICAL +FLAG IN LNAV VERTICAL -FLAG IN LNAV FCS LOC ENGAGE IN OBS RETURN...
  • Page 172 Navigation Bendix/King Indicator KI 208A P208A1 LNAV LATERAL DEV +LT IN LNAV LATERAL DEV +RT IN LNAV +TO IN LNAV +FROM IN LNAV LATERAL +FLAG IN LNAV LATERAL -FLAG IN LNAV FCS LOC ENGAGE IN OBS RETURN LNAV OBS EXCITATION IN LNAV OBS SIN OUT LNAV OBS COS OUT RELAY ENGAGE...
  • Page 173 Navigation Mid-Contient Indicator 200-202/ 200-203/ 200-206/ 200-207/ -302 -303 -306 -307 +LEFT +RI GHT +FRO M NAV +FLAG NAV -FLAG GPS ANNUNCI ATOR VLOC ANNUNCIATOR +DO WN GLIDESLOPE +FLAG GLIDESLOPE -FLAG RESO LVER H RESO LVER C RESO LVER D RESO LVER E RESO LVER F RESO LVER G...
  • Page 174 Radio Magnetic Bendix/King Indicator KNI 582 KNI 582 KI 229 KDA 692 Pointer #1 Pointer #2 P2291 P5821 P5821 P6921 OBI CLOCK OBI DATA OBI SYNC Radio Magnetic Bendix/King Indicator KNI 582 KNI 582 KI 229 KDA 692 Pointer #1 Pointer #2 P2291 P5821...
  • Page 175 Bendix/King KN 62/62A KN 64 AERONAV XXX #1 P1006 P621/P62A1 P641 SERIAL DME DATA DATA BUS SERIAL DME CLOCK CLOCK BUS SER DME-CHAN REQ/PAR DME-4MHZ RNAV/CHANNEL REQUEST DME COMMON DME COMMON SER DME-RNAV MODE/PAR DME-2MHZ AERONAV XXX #2 P1006 SERIAL DME DATA SERIAL DME CLOCK SER DME-CHAN REQ/PAR DME-4MHZ DME COMMON...
  • Page 176 Figure D - 21: King Serial DME Tuning Interconnect, Remote Mount 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-28 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 177 Figure D - 22: Parallel DME Tuning Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 178 Parallel Slip Code Bendix/King Tuned DME KN 61 KN 65 AERONAV XXX P1006 P611 P651 PARALLEL DME-8MHZ SER DME-CHAN REQ/PAR DME-4MHZ SER DME-RNAV MODE/PAR DME-2MHZ PARALLEL DME-1MHZ PARALLEL DME-800KHZ PARALLEL DME-400KHZ PARALLEL DME-200KHZ PARALLEL DME-100KHZ PARALLEL DME-50KHZ DME COMMON DME COMMON S OTHERWISE NOTED.
  • Page 179 Figure D - 24: Autopilot Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-31 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 180 Figure D - 25: External Navigation Source and GPS Annunciators Interconnect Page 1 of 2 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-32 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 181 MD41-14xx MID-CONTINENT MD41-xxxx GPS ACU 1484W 1404A/1408A 1464A/1474A 1470 AERONAV XXX P1001 1488W 1414A/1418A 1468A/1478A VLOC ANNUNCIATE VLOC ANN GPS ANNUNCIATE GPS ANN WAYPOINT ANNUNCIATE WPT ANN TERMINAL ANNUNCIATE TERM ANN APPROACH ANNUNCIATE APR ANN MESSAGE ANNUNCIATE MSG ANN OBS ANNUNCIATE OBS ANN INTEGRITY ANNUNCIATE INTG ANN...
  • Page 182 Figure D - 26: Switch Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-34 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 183 Figure D - 27: Garmin GAD 42 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-35 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 184 Figure D - 28: Garmin G600 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-36 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 185 Figure D - 29: Avidyne EX500/600/5000 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-37 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 186 Figure D - 30: Aspen EFD1000 Interconnect (without ACU) 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-38 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 187 Figure D - 31: Aspen EFD1000 Interconnect (with ACU) 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-39 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 188 Figure D - 32: Transponder Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-40 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 189 Figure D - 33: ELT Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-41 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 190 AVIDYNE SKYTRAX 100 AERONAV XXX P1001 ARINC 429 IN A TIS 429 TX 1A ARINC 429 IN B TIS 429 TX 1B RS232 TX 2 RS232 GPS RX RS232 TX 1 FIS DISPLAY RX RS232 RX 1 FIS DISPLAY TX DISPLAY GND NOTES: ALL WIRES TO BE 22 AWG OR GREATER UNLESS OTHERWISE NOTED.
  • Page 191 Figure D - 35: RDR2000 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-43 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 192 Figure D - 36: GTX 335 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-44 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 193 Figure D - 37: GTX 345 Interconnect (see below for notes) 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-45 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 194 NOTES: 1. ALL WIRES TO BE 24 AWG MINIMUM UNLESS OTHERWISE SPECIFIED. 2. ALL GROUND CONNECTIONS SHOWN FOR THE GTX345 ARE TO BE CONNECTED TO SHIELD BLOCK GROUND. 3. AT AERONAV UNIT, TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR USE CARD-EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE –...
  • Page 195 Figure D - 38: GTX 330ES Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-47 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 196 Figure D - 39: Robinson Analog Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-48 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 197 Figure D - 40: Robinson Aspen EFD100 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-49 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 198 Figure D - 41: Avidyne AXP322/Trig TT22 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-50 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 199 Figure D - 42: Avidyne Dual AXP322/Trig TT22 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-51 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 200 Figure D - 43: FreeFlight FDL 978RX Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-52 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 201 Figure D - 44: GDL 88 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-53 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 202 Figure D - 45: Avidyne AXP340/Trig TT31 Interconnect Figure D - 46: XMD076 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-54 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 203 Figure D - 47: Single GDU700/1060 PFD Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-55 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 204 Figure D - 48: Dual GDU700/1060 PFD Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-56 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 205 Figure D - 49: Garmin G5 EHSI Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-57 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 206 Figure D - 50: Garmin G5 EADI Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-58 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 207 Figure D - 51: Garmin G5 EFIS Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-59 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 208 Figure D - 52: NGT9000R Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-60 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 209 Figure D - 53: KT-74 Interconnect 89000046-014 KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D-61 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 210 Appendix E: Troubleshooting Guide Component Trouble Probable Cause Solution AeroNav XXX The unit is not getting power to The unit is not getting power. Check Circuit Breaker the main connector Check wiring and unit seating in tray The AeroNav XXX is not Wiring Check Coaxial Cables computing a position...
  • Page 211 Lighting page for proper setting CMOS Battery Dead CAS The 10-year life expectancy of Return the AeroNav to Message the CMOS battery has been BendixKing for battery reached. This may result in replacement longer GPS satellite acquisition times. VHF Radio Slots displaying Red-...
  • Page 212 Appendix F: Configuration Setup In order to support the requirements of some validations of the AML STC, this section should be easily removable and inserted into the aircraft logs. For those installations where an AeroNav XXX is replacing a GNS-530/W or GNS-430, please record the following parameters from the GNS-530/W or GNS-430/W setup pages before removing the unit (Note: this will need to be conducted for each GNS-530/W or GNS-430/W being replaced): WAAS Enabled (530W or 430W with approved antenna)? Yes...
  • Page 213 Please list the other avionics that are installed in the aircraft (please be as specific as possible with make and models of the gear) and connected to the GNS-530/W or GNS-430/W. Enter “None” or “Don’t Know” as required. The GNS-530/W or GNS-430/W Setup pages will be captured on subsequent pages.
  • Page 214 Air Data IRU/INS Other Other Other GNS-530/W or GNS-430/W Maintenance Mode Entry: GNS-530 configuration data is accessed from the GNS-530/W Maintenance Mode settings which is entered via holding ENTR button on 530/W bezel during power application. GNS-530/W or GNS-430/W Page Navigation: Use the inner right knob on the GNS-530/W to scroll through the maintenance mode pages.
  • Page 215 AeroNav XXX - Main ARINC 429 Config Page (1/12) Garmin 530/W or 430/W - MAIN ARINC 429 CONFIG page Speed Data Speed Data In 1 IN 1 In 2 IN 2 VNAV VNAV For new AeroNav 880/900 installations, see (if present) Section 7.5.2 for selections and descriptions AeroNav XXX - Main RS232 Config Page (2/12) Input...
  • Page 216 AeroNav XXX – Main System Config page (3/12) GNS-530/W or 430/W – MAIN SYSTEM CONFIG Page (Fuel) Fuel Type CONFIGURE Fuel GPS Select FUEL TYPE Airframe Tail Number GNS-530/W or 430/W – MAIN SYSTEM CONFIG Page External TAWS (Terrain) [if present] CONFIGURE Terrain WOW Input (Helo)
  • Page 217 GNS-530/W or 430/W – MAIN INPUTS Page AeroNav XXX – MAIN INPUTS Page (4/12) B ALT B ALT W DIR D ALT W DIR D ALT GPS SC P ALT P ALT VLC SC L FF L FF R FF R FF W SPD T FF...
  • Page 218 GNS-530/W or 430/W– MAIN LIGHTING Page AeroNav XXX – MAIN LIGHTING Page (5/12) Display Bezel Display Photo LIGHTING Response Time SOURCE Photo Slope RESP TIME / Photo Minimum SLOPE / OFFSET Photo Maximum PHOTO TRANS % dimBus Transition applicable) dimBus PHOTO SLP / Slope OFST (if...
  • Page 219 GNS-530/W or 430/W – DATE / TIME SETUP Page (No Need to Fill In – For Reference Only) UTC DATE UTC TIME No AeroNav XXX Equivalent AeroNav XXX – MAIN DISCRETE I/O Page (6/12) GNS-530/W or 430/W – MAIN DISCRETE I/O Page GRAY CODE DECODED ALTITUDE GRAY...
  • Page 220 GNS-530/W or 430/W – MAIN CDI / OBS CONFIG AeroNav XXX – MAIN CDI / OBS CONFIG Page Page (7/12) FLAG FROM FLAG FROM VERT VERT SELECTED COURSE SELECTED COURSE V-FLAG Ignore SEL SOURCE STATE CRS for Ignore SEL CRS for VLOC V-FLAG SOURCE...
  • Page 221 GNS-530/W or 430/W – VOR/LOC/GS CDI Page AeroNav XXX – VOR/LOC/GS CDI Page (8/12) FLAG FLAG FROM FLAG FLAG FROM VERT VERT SELECTED COURSE SELECTED COURSE CHANNEL CHANNEL MODE MODE GNS-530W or GNS-430W Only For new AeroNav XXX installations, see Section 7.5.9 for selections and descriptions.
  • Page 222 GNS-530/W or 430/W– STORMSCOPE CONFIG Page (if configured for Stormscope) STATUS: MODE: AeroNav XXX STORMSCOPE CONFIG Page (Software version 10.2 or higher) Accessible via the TEST page, select GET DATA, scroll to Config, and record the SW VERSION: ANT MOUNT: jumpers installed and grounded HEADING J3-1...
  • Page 223 AeroNav XXX – STORMSCOPE DATA Page (Software version 10.2 or higher) GNS-530/W or 430/W– STORMSCOPE DATA DOWNLOAD Page (if configured for Stormscope) SOFTWARE VERSIONS: SOFTWARE VERSIONS: Model Model Main SW Ver Main SW Ver Main Boot SW Ver Main Boot SW Ver DSP SW Ver DSP SW Ver GNS-530/W or 430/W –...
  • Page 224 GNS-530/W or 430/W– RYAN TCAD CONFIG Page (if configured for Ryan TCAD] MODE APPROACH MODE HEIGHT RANGE GND/FLD ELEVATION No AeroNav XXX Equivalent Page Note: Use the presence of the traffic VOLUME thumbnail and the Audio Volume Control page to control these parameters in the MUTE DURATION AeroNav XXX.
  • Page 225 GNS-530/W or 430/W– TAWS Audio Config Page 1 (if installed) No AeroNav XXX Equivalent Page TAWS CONFIG (Use the User Options LSK and Volume Control VOICE GENDER LSK of the Audio Tab instead) VOLUME PLAY AUDIO MSG GNS-530/W or 430/W – TAWS Audio Config Page 2 (if installed) ALERT Reduced Terrain Clearance...
  • Page 226 GNS-530/W or 430/W – GDL Config Page AeroNav XXX – GDL Config Page (if installed) (if installed) (11/12) ATTENUATION ATTENUATION MODEL (if displayed) MODEL GNS-530/W or 430/W – DATALINK DIAGNOSTICS Page (if installed) TERR No AeroNav XXX Equivalent Page Note: Use the Datalink Status page on the AUX- SYS tab for datalink status data.
  • Page 227 Notice: SOFTWARE LICENSE: AVIDYNE CORPORATION (“AVIDYNE”) IS WILLING 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.
  • Page 228 © Honeywell International Inc. Do not copy without express permission of Honeywell.

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