BENDIXKing 700-00179-700 Installation Manual Download

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89000046-014

KSN 780/8XX/900 AeroNav AML STC Installation Manual for Helicopters

Rev 0

Page-4-3

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. The Circuit Breaker must be clearly identified and visible under all lighting

conditions. Circuit breaker size is identified in installation data shown in Appendix D: Electrical

Interface Drawings. Note that 14v aircraft may be required to replace the installed circuit breaker

and power wiring to accommodate the AeroNav XXX.

4.9 Power Distribution

Note: The references in the below images to the COM block are N/A for the AeroNav 880/780.
Aircraft installing one AeroNav XXX should connect the power and grounds as shown in Figure 3.

Avionics Bus

AeroNav 800/900

COM

Aircraft Ground

Single Avionics Bus

Figure 3 AeroNav XXX Power Distribution

Aircraft installing two should connect the power and grounds as shown in in Figure 4.

Avionics Bus 1

Avionics Bus 2

AeroNav 800/900

COM

AeroNav 800/900

COM

Aircraft Ground

Avionics Bus

AeroNav 800/900

COM

AeroNav 800/900

COM

Aircraft Ground

Preferred

Alternate

Figure 4 Dual AeroNav XXX Power Distribution

Summary of Contents for 700-00179-700

Page 1: ...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 an...

Page 2: ...Blank Page...

Page 3: ...are under continuous research and development Any information may therefore be changed without prior notice Honeywell reserves the right to make improvements or changes in the product described in th...

Page 4: ...ernational Inc Do not copy without express permission of Honeywell RECORD OF REVISIONS NOTE The revision level for every page of this document will be updated during the revision process A list of eff...

Page 5: ...00184 002 AeroNav 780 800 Install Kit Fixed Wing Tray Backplate 89000041 007 850 00184 003 AeroNav 780 800 Install Kit Helicopter Tray Backplate Connectors 89000041 009 850 00182 710 AeroNav 880 GPS...

Page 6: ...tions 1 7 1 6 3 Non TSO Functions 1 8 1 6 4 Partial TSO Functions 1 9 1 6 5 Open Problem Report 1 9 1 7 Software and Hardware Design Assurance Levels 1 9 1 8 Environmental Qualification Forms 1 10 1 9...

Page 7: ...terference 3 6 3 3 7 Ground Plane 3 6 3 3 8 Dual AeroNav XXX Installations 3 6 3 3 9 Anti Ice Protection 3 6 3 4 VHF Communication Antenna 3 6 3 4 1 Antenna Environmental Qualifications 3 6 3 4 2 VHF...

Page 8: ...New Installations 4 3 4 8 Circuit Protection 4 3 4 9 Power Distribution 4 3 4 10 Electrical Load Analysis 4 4 4 11 Low Power Behaviors 4 4 5 Mechanical Installation 5 1 5 1 Equipment Location New Ins...

Page 9: ...ndicator Electrical Characteristics 6 15 6 1 14 DME Tuning 6 15 6 2 Bezel Lighting 6 16 6 3 Traffic System 6 17 6 4 Lightning Detection System 6 17 6 5 Datalink Weather 6 18 6 6 Audio Panels 6 18 6 7...

Page 10: ...7 28 7 5 13 GDL Configuration Pages Page 11 7 29 7 5 14 Remote XPDR Configuration Page 12 7 30 7 5 15 WiFi Setup Page 13 7 30 7 5 16 Bluetooth Setup Page 14 7 37 7 5 17 RDR2000 Radar Configuration Pag...

Page 11: ...R Flight Checks 8 1 8 4 ILS Flight Checks 8 1 8 5 Sensors Verification 8 1 9 Glove Validation Procedures 9 1 10 Software and Database Update Procedures 10 1 10 1 Data Updates 10 1 10 2 Datalogs Downlo...

Page 12: ...he aircraft certification requirements must remain in compliance 2 An Electrical Load Analysis must be accomplished to determine that the electrical limits of the specific aircraft are not exceeded Th...

Page 13: ...00182 710 700 00182 711 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 00 510 00346 000 Rev 00 FPSM 530 00226 000 Rev 04...

Page 14: ...311 001 Rev 00 510 00312 005 Rev 00 510 00346 000 Rev 00 FPSM 530 00226 000 Rev 04 510 00294 000 Rev 04 510 00291 000 Rev 00 LIO App 530 00239 000 Rev 05 510 00328 000 Rev 00 510 00329 000 Rev 05 LIO...

Page 15: ...n History Modification Change Hardware PN Hardware Revision Software HW Release Date MOD 20 ADDS SHIELDING TO VHF CIRCUITS TO ELIMINATE SQUELCH BREAK 700 00179 700 03 03 10 1 or later 08 04 2019 Table...

Page 16: ...fications 1 4 1 2 AeroNav 880 900 Display Specifications Display Size 5 7 inches diagonal Active Area 4 53 inches w x 3 40 inches h Resolution 640x480 pixels Viewing Angle AeroNav 880 900 Designed and...

Page 17: ...receiver that complies with AC 20 138C Table 7 AeroNav 880 900 GPS Specifications 1 4 1 4 AeroNav 900 VHF Communication Transceiver Specification Audio Output 65 mW into 150 load Audio Response 6dB Va...

Page 18: ...Weights 1 4 1 6 AeroNav 900 VHF Navigation Specification Glideslope Receiver Selectivity 0 0091 ddm w test signal varied 17kHz 60dB for 132kHz offset Sensitivity flag 10uV max Spurious Response 60 dB...

Page 19: ...sity D Subminiature male P1002 25 position Standard D Subminiature female P1006 44 position High Density D Subminiature male Electrical Requirements Voltage 9 33 VDC Current AeroNav 780 4 4A main at 1...

Page 20: ...aximum below 60 000 ft TTFF Time to First Fix 150 seconds Reacquisition 20 seconds Position Update Interval 0 2 seconds 5 Hz PPS Signal Time Mark UTC Epoch 100ns 50ns over all conditions 1 sec 75ns be...

Page 21: ...Level 39dB S N N Frequency Stability 2 5 ppm Demodulation Audio Distortion 12 70 modulation Sidetone Fidelity 300 2500 Hz Demodulation Audio Response 6dB Variation from 300 to 2500 Hz Table 15 VHF Co...

Page 22: ...e 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 TSO articles must have separate a...

Page 23: ...ide Area Augmentation System WAAS Airborne Supplemental Navigation Equipment Using the Global Positioning System GPS Gamma 3 TSO C147a Traffic Advisory System TAS Airborne Equipment Class A Display Fu...

Page 24: ...ppropriate for rapid pilot recognition of exceedances 3 The fuel flow indicators are a digital readout instead of pointer and dial TSO C110a Airborne Passive Thunderstorm Detection Equipment 1 Environ...

Page 25: ...cal Depiction of Aircraft Position 1 De cluttering on chart page not provided 2 Location of traffic symbols in the absence of heading information TSO C169a VHF Radio Communications Transceiver Equipme...

Page 26: ...21 Partial Function TSOs 1 6 5 Open Problem Report At the time of this revision the AeroNav XXX does not have any open problems that affect safety or design assurance level of the unit 1 7 Software an...

Page 27: ...ing the USB port on the AeroNav Reference the AeroNav 800 780 Series Pilot s Guide or AeroNav 900 880 Series Pilot s Guide for updating the AeroNav XXX databases 1 10 Fault Detection and Exclusion FDE...

Page 28: ...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 airsp...

Page 29: ...itations stated in the STC and this manual Any deviations from the STC and or this manual must have a separate installation approval Installations in Part 23 25 29 aircraft or Part 27 helicopters not...

Page 30: ...mponent Ship Kit Black Bezel Ship Kit Black Bezel With Video AeroNav 900 Unit 89000039 003 89000039 004 AeroNav 880 Unit 89000041 009 89000041 010 Table 23 AeroNav 880 900 Ship Kit Component Ship Kit...

Page 31: ...a Kit Component Ship Kit ByteFlight Cable 20 ft 89000046 011 Table 29 ByteFlight Ship Kit 1 13 Materials Required but not Supplied The AeroNav XXX will require common installation supplies The followi...

Page 32: ...s as identified in Section 6 6 in order to supply AeroNav XXX terrain alerting audio Forward Looking Terrain Alerting FLTA functionality and TOD chime to the headsets For those installations that use...

Page 33: ...sets Forward Enables external command e g yoke mounted button to select frequencies forward in the com preset list to be loaded into the 1 Standby com slots Section 6 1 12 4 Com Presets Reverse Enable...

Page 34: ...y claims Category Vendor Model Air Data B D 2600 ADC B D 2601 ADC B D 2800 ADC B D 900004 003 ADC Bendix King KAD 280 480 ADC KDC 281 481 Shadin 8800T Alt Computer Shadin 9000T Alt Computer Shadin 920...

Page 35: ...GPSMAP 496 Garmin GPSMAP 695 Garmin GPSMAP 696 Garmin Aera 796 795 Argus 3000 Argus 5000 Argus 7000 Horizon DDMP Avidyne EX500 Avidyne EX600 Avidyne EX5000 Avidyne FlightMax Series Heading Bendix Kin...

Page 36: ...e Monitor JPI FS 450 ARNAV FC 10 ARNAV FT 10 EI FP 5L EI CGR 30P Insight GEM 3 Traffic L3 SKY497 SkyWatch L3 SKY899 SkyWatchHP Bendix King KTA 870 Bendix King KTA 970 Bendix King KMH980 Bendix King KM...

Page 37: ...e Adapter EGPWS Bendix King KGP560 DME Bendix King KN 61 Bendix King KN 62 62A Bendix King KN 63 Bendix King KN 64 Bendix King KN65 Bendix King KDI 572 Bendix King KDI 574 Bendix King KDM706 Collins D...

Page 38: ...ry RD444 Sperry RD 550A Sperry RD 650 RMI Bendix King KI 229 Bendix King KNI 582 Bendix King KDA 692 External GPS Annunciator Mid Continent MD41 Series Staco Switch 992561 Vivisun 95 40 Vivisun 95 45...

Page 39: ...ll function Table 31 AeroNav XXX Compatible Equipment 2 4 Minimum System Configuration for VFR 2 4 1 VFR Installation This section is intended for stand alone AeroNav XXX installations intended for VF...

Page 40: ...Can the AeroNav XXX helicopter tray be installed per the data in this manual If No additional installation approval is required Navigation s Antenna Installed N A for AeroNav 880 780 Section 3 5 Commu...

Page 41: ...13 1B Chapter 4 Also reference Appendix B STC Permissions in this manual The GPS antenna listed in Table 28 can be installed on unpressurized metal helicopters using the data below All other GPS Anten...

Page 42: ...and doubler thickness appropriate for the aircraft s skin thickness Fuselage Thickness Doubler Thickness Doubler Drawing 0 016 0 025 0 020 See Figure C 8 and C 9in Appendix C 0 032 0 050 0 032 Table 3...

Page 43: ...igure 1 defines a zone immediately aft of the nose of the helicopter where the GPS antenna should not be installed Helicopter locations aft of zone 1A 1B that are in a zone 2A or zone 3 are acceptable...

Page 44: ...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 Loc...

Page 45: ...l cable should be assembled per the connector manufacturer s assembly instructions 3 3 5 Approved GPS Antennas The AeroNav XXX can be interfaced to all TSO C190 antennas and the approved antennas list...

Page 46: ...is permitted to have a non WAAS system and a WAAS system installed however if the two antennas are not of the same type i e dual non WAAS or dual WAAS installation then FMS related data flight plans...

Page 47: ...cable should be made of RG 142B RG 400 or an equivalent 50 coaxial cable 3 5 3 Navigation Coaxial Cable Connector The connectors on the VHF navigation coaxial cable should be assembled per the connect...

Page 48: ...quipment should be installed with separation between redundant systems to prevent loss of navigation due to a single event 4 4 Shield Grounds All shield grounds should be grounded using the ground blo...

Page 49: ...9029 58 360 ORG BLU BLK M22520 02 01 M22520 2 09 M81969 1 04 M81969 1 04 P1050 Only on 880 780 M24308 4 268 M39029 58 360 ORG BLU BLK M22520 02 01 M22520 2 09 M81969 1 04 M81969 1 04 Ground Block 5838...

Page 50: ...lighting conditions Circuit breaker size is identified in installation data shown in Appendix D Electrical Interface Drawings Note that 14v aircraft may be required to replace the installed circuit br...

Page 51: ...for AeroNav XXX power requirements Also reference FAA AC 43 13 2B Paragraph 208 for more information on performing an aircraft electrical load analysis The purpose of the ELA is to show compliance to...

Page 52: ...the backside of the instrument panel The instrument panel requires either a 6 320 x 4 600 or 6 320 x 2 70 hole for the AeroNav 880 900 or AeroNav 780 800 respectively If the instrument panel in the ai...

Page 53: ...is inserted into the hole in the front bezel 5 5 Internal Cooling The AeroNav has several internal fans and heat sinks as part of its basic design There are exhaust vents on the left and right sides...

Page 54: ...milliohm 5 8 Weight and Balance After installing the AeroNav XXX the aircraft s weight and balance must be updated after installation is complete For those installations where an AeroNav 900 800 is re...

Page 55: ...iate Output 3 Waypoint Annunciate Output 4 Terminal Annunciate Output 5 Approach Annunciate Output 6 Message Annunciate Output 7 OBS Annunciate Output 8 Weight on Wheels WOW Output Output 9 Integrity...

Page 56: ...OBS Output 37 Audio 1 HI Alert audio Output 38 Audio 1 LO Alert audio Output 39 LTG Bus HI Input 40 LTG Bus LO GND Input 41 GPS RS232 Out 3 Output 42 GPS RS232 In 3 Input 43 Main OBI Clock Output 44...

Page 57: ...Select Input 74 COM Remote Recall Forward Input 75 COM Remote Recall Reverse Input 76 LTG BUS 2 HI Input 77 Aircraft GND 78 Aircraft GND Table 37 P1001 Pin Description 6 1 2 P1002 Communication Conne...

Page 58: ...C 2 5V Common Output 3 VOR LOC Flag Output 4 VOR LOC Flag VOR LOC 2 5V Common Output 5 VOR LOC Left Output 6 VOR LOC Right VOR LOC 2 5V Common Output 7 Com Monitor Audio HI Output 8 VOR LOC Composite...

Page 59: ...ut 41 Aircraft GND 42 Parallel DME 100KHz Output 43 Parallel DME 50KHz Output 44 Aircraft Power In Only used for Superflag Outputs Input Table 39 P1006 Pin Description 6 1 4 P1050 Additional I O Conne...

Page 60: ...y 6 1 5 Altitude Gray Code Altitude Gray code input is connected on the following pins Description Connector Pin Signal Type Altitude D4 P1001 70 Input Altitude A1 P1001 69 Input Altitude A2 P1001 68...

Page 61: ...GND P1002 25 Input Table 42 Synchro Heading Input 6 1 7 Main Course Deviation Indicator Output The main indicator displays both lateral and vertical deviations TO From and Flag indications from the N...

Page 62: ...flags The Navigation Superflags is on the following connector and pins Description Connector Pin Signal Type Main Lateral Super Flag P1001 17 Output Main Vertical Super Flag P1001 18 Output Table 46 M...

Page 63: ...iate P1001 9 Output LNAV GPS Select P1001 13 Output ILS GPS Approach P1001 14 Output Table 48 Annunciator Output All outputs sink up to 500 mA when activated 6 1 7 7 Switch Inputs Description Connecto...

Page 64: ...utput RS 232 Input 5 P1050 61 Input RS 232 Output 6 P1050 62 Output RS 232 Input 6 P1050 63 Input Table 51 RS 232 Input Output AeroNav 880 900 Only 6 1 9 ARINC 429 Description Connector Pin Signal Typ...

Page 65: ...Parameter Name 1 2 3 4 5 6 7 001 Distance to Go 002 Time to Go 012 Ground Speed 074 Data Record Header 075 Active Waypoint From To Data 100 Selected Course 1 113 Message Checksum 114 Desired Track 115...

Page 66: ...nation 352 Estimated Time to Destination 371 Specific Equipment ID 377 Equipment Hex ID Code 6 1 9 2 VHF ARINC Output Applies To AeroNav 800 900 Only 6 1 9 3 Onboard Radar ARINC Output When configured...

Page 67: ...136 VFOM 140 UTC Time of Fix Fine 150 UTC Time of Fix From GPS 165 Vertical Velocity 166 North South Velocity 174 East West Velocity 203 Pressure Altitude 247 Horizontal Figure of Merit HFOM 260 Date...

Page 68: ...pedance supply 9V via 620 6 1 12 3 Com Audio VOR ILS Audio Description Connector Pin Signal Type Com Audio HI P1002 7 Output Com Audio LO P1002 19 Output VOR ILS Audio HI P1006 16 Output VOR ILS Audio...

Page 69: ...e 60 Navigation Superflag Output The output supplies not less than 500 mA on a 28 volt system and 250 mA on a 14 volt system with the output voltage at Aircraft voltage 3VDC when the flag is to be out...

Page 70: ...V DME Common must be pulled low for the AeroNav XXX to channel the DME DME is active if the voltage to ground is 1 9 V or the resistance to ground is 375 Outputs is not more than 1 0V while sinking 20...

Page 71: ...rax100 formerly MLB100 Navworx 200 0011 RS232 or ARINC 429 RS 232 preferred Avidyne Corporation Skytrax100B RS232 or ARINC 429 RS 232 preferred L3 Communications SKY497 SKY899 ARINC 429 Bendix King KT...

Page 72: ...32 AeroNav with s w 10 2 3 1 or later Garmin GDL69 69A P N 011 00986 00 or 011 00987 00 only Pre Software 10 2 3 1 With Software 10 2 3 1 or later P N 011 03177 X0 will also work RS232 Garmin Software...

Page 73: ...tes Aspen EFD1000 ARINC 429 Low Speed Avidyne Entegra PFD ARINC 429 Low Speed Garmin G500 600 ARINC 429 Low Speed B D 90004 003 ARINC 429 Low Speed Honeywell Bendix King KDC281 481 ARINC 429 Low Speed...

Page 74: ...o the AeroNav XXX the AeroNav XXX will use the heading sources in this order highest first 1 ARINC 429 INS IRU 2 ARINC 429 EFIS 3 ARINC 429 from GAD42 4 ARINC 429 from EHSI 5 ARINC 429 from GTX 33 330...

Page 75: ...ansponder UAT Output The AeroNav XXX will transmit ADS B GPS position data to the following compatible ADS B capable transponders UAT Manufacturer Model Notes Avidyne Trig AXP340 TT31 ADS B output req...

Page 76: ...installer prior to returning the aircraft to 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 us...

Page 77: ...r Set the transponder to accept an active low when performing that squat switch setup The AeroNav XXX retransmits the Altitude data received from external altitude devices to GTX3X5 This is a non TSO...

Page 78: ...X 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...

Page 79: ...R94 interconnect The TDR94 part number needs to be a 500 or higher for ADS B OUT to be approved AERONAV XXX must have software 10 2 3 1 or later Table 72 ADS B Output 6 12 Video Input The AeroNav 880...

Page 80: ...sult in damage to the AeroNav XXX or to the equipment connected to the AeroNav XXX 7 2 Mounting Check Verify the AeroNav XXX tray is securely installed to the airframe 7 3 Chassis ID Setting For dual...

Page 81: ...or GNS 430 W use Appendix F Configuration Setup of this manual to first record the configuration of the GNS530 W or GNS430 W that is being replaced by the AeroNav XXX and then using that recorded data...

Page 82: ...Port will have a Speed selection and Data selection Figure 7 AeroNav 880 900 ARINC 429 Configuration Page The Speed Selection will have the following options Selection Description Low Standard low sp...

Page 83: ...from the following Flight Control systems Bendix King KFC400 Garmin GAD 42 Selected course heading and true airspeed data from Garmin GAD 42 Garmin GDL 88 Traffic Garmin GDL 88 Traffic from the GDL 8...

Page 84: ...Selected course and heading information from the following EHSI systems Sandel SN 3308 Sandel SN 3500 Avidyne EXP5000 Traffic Advisory Traffic information from the following traffic advisory systems...

Page 85: ...ndix King EFS 40 50 without update SW15 01 GPS vertical guidance provided on EFIS GAMA 429 Graphics ARINC 429 data as defined by the GAMA General Aviation Subset 2nd Edition including GAMA Graphics Pr...

Page 86: ...tes all 429 outputs with SDI 0 LNAV 1 Number 1 Pilot long range navigator RX Accepts 429 inputs with SDI 0 or 1 TX Generates all 429 outputs with SDI 1 LNAV 2 Number 2 Copilot long range navigator RX...

Page 87: ...the following ADS B Avi ADSB ADS B G GDL 88 Aviation Avtn no alt HW EGWS MapMX The following selections can be made on the RS 232 Input Channel Inputs Selection Description Off No device s connected t...

Page 88: ...3rd party compatible ADS B traffic devices transmitting at 38400 baud Capstone Trfc Wx1 2 Garmin GTX 345 and other 3rd party compatible ADS B traffic and weather devices transmitting at 38400 baud Ca...

Page 89: ...can display on the AeroNav and the lower priority weather data can be streamed out of the AeroNav via WiFi for display on a compatible tablet wireless device application The current display priority...

Page 90: ...100 or Freeflight FDL 978 RX Capstone Trfc2 Garmin GTX 335 345 and other 3rd party compatible ADS B traffic devices Capstone Trfc Wx1 2 Garmin GTX 345 and other 3rd party compatible ADS B traffic and...

Page 91: ...B avi HW EGPWS and MapMx 7 5 4 Main System Configuration This is a general page for miscellaneous configurations Figure 9 Main System Configuration Page The Main System Configuration Page Page 3 of 1...

Page 92: ...the GPS VLOC Capture option on the User Options part of the Setup tab on the AUX page Table 85 GPS Sequencing Airframe Selections Selection Description Fixed Wing For Fixed Wing installations Helicop...

Page 93: ...nabled Select Disable Not applicable for helicopter installation Disabled Default setting Table 91 Joystick Input Note It is imperative that only one source of terrain cautions and warnings be enabled...

Page 94: ...used for verifying electrical interfaces during installation and troubleshooting Field Description OAT Outside Air Temperature SAT Static Air Temperature TAT Total Air Temperature IAS Indicated Airspe...

Page 95: ...Lighting Configuration Page Photo Response Time Sets the speed at which the brightness changes when photocell is selected as the lighting source Both the Bezel and Display fields have a range of 1 to...

Page 96: ...nd then suddenly jumps to bright dimBus Slope The dimBus Slope sets the sensitivity of the display bezel to the aircraft dimmer Both the Bezel and Display fields have a range of 15 to 100 and the fact...

Page 97: ...on Manual for Helicopters Rev 0 Page 7 18 Honeywell International Inc Do not copy without express permission of Honeywell The AviCurve tracks the aircraft dimming bus as follows Figure 11 Lighting Cur...

Page 98: ...on Dimming Bus Calibration The section will calibrate the AeroNav XXX to the aircraft avionics lighting bus Selection Description dimBus Type DC select this option if the dimming bus is a DC bus AC se...

Page 99: ...ed Table 95 External Switch State Selection Verify That APR The APR annunciator is on or off as selected on this page GPS The GPS source select annunciator is on or off as selected on this page INTEG...

Page 100: ...nd therefore this is for bench testing purposes only TER CAUT The TER CAUT annunciator is on or off as selected on this page TER INHB The TER INHB annunciator is on or off as selected on this page TER...

Page 101: ...vertical flag on the external indicator is in view Table 98 Main CDI Flag Test Page TO FROM Selection Description FROM The FROM flag on the external indicator is in view Hidden The TO FROM flag on the...

Page 102: ...ce The VLOC annunciator will also be active GPS Only N A for AeroNav 880 780 The VLOC selection on the AeroNav XXX Nav Source knob has been disabled Therefore GPS and OBS are the only two available ch...

Page 103: ...s and does not support the testing of super flags CDI LAT VERT Selection Description Max Left The external CDI will be off scale full deflection to the left up Full Left The external CDI will be defle...

Page 104: ...urse is displayed on the AeroNav 880 900 and press the ENTR button on the AeroNav XXX 3 After calibrating verify 30 increments on the CDI HSI are properly displayed on the AeroNav XXX 2 In order to do...

Page 105: ...NC 429 Table 109 VOR LOC GS ARINC 429 Speed Configuration Format Selection RX TX Description OFF RX No data will be processed from an external device Proline VHF RX Processes VOR LOC G S and frequency...

Page 106: ...e 111 VOR LOC GS SDI Selection DME Mode Selection Description Directed Freq 1 If the AeroNav XXX is connected to a single channel or multi channel ARINC429 DME Direct Freq 1 will channel Receiver 1 Di...

Page 107: ...tenna 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 co...

Page 108: ...guration Page GDL Selection Page This page selects the attenuation and the type of GDL receiver connected to the AeroNav XXX Selection Description Attenuation This parameter sets the attenuation GDL 6...

Page 109: ...required for automatically selecting the transponder air or ground mode of operation For aircraft without a squat switch connect the squat switch input of the transponder to P1001 pin 8 of one of the...

Page 110: ...ntenance mode In order to modify one or both of these settings proceed as follows To configure the WiFi Mode 1 Boot the AeroNav to Maintenance mode 2 Select the Config tab 3 Turn the right knob until...

Page 111: ...the selection rectangle until the current Local SSID field is selected as shown Figure 23 WiFi Configuration Page 6 Press the right knob 7 The inner knob can now be used to advance through the availa...

Page 112: ...ork 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 Configur...

Page 113: ...5 15 1 2 Configuring the AeroNav as a Client to an External WAP In some cases an aircraft may have an existing WAP in use For example some aircraft may be accustomed to connecting 3rd party iPad appli...

Page 114: ...layed as shown in the image below Figure 27 WiFi Configuration Page 4 Press the lower right knob 5 Using the outer right knob advance the selection rectangle until the Remote SSID field is selected as...

Page 115: ...d 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...

Page 116: ...he Bluetooth Interface 1 Boot the AeroNav to Maintenance mode 2 Select the Config tab 3 Turn the right knob until the Bluetooth Setup Page is displayed as shown in the image below Figure 31 Bluetooth...

Page 117: ...between 26 5 and 28 0 in the Gain Pot field This will initiate the antenna clearance scan The antenna will move to each of the extreme positions to determine that there is no interference with the an...

Page 118: ...ode Config Tab when one set of the RS232 ports has been configured as WX 500 and at least one power cycle has been executed since configuration Stormscope Test page contains the following LSKs Change...

Page 119: ...no dedicated GAD42 configuration page in the AeroNav XXX 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 conf...

Page 120: ...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 Figure 33 Software Version Page Figure 3...

Page 121: ...and AeroNav 800 780 Series Pilot s Guides or Section 10 1 for update procedures 7 6 2 Airplane Flight Supplement Check Complete and install the Airplane Flight Manual Supplement in the aircraft s Fli...

Page 122: ...S position Verify no interference from other aircraft equipment is observed e g TCAS SATCOM etc 7 6 7 VHF COM Checkout Note This section is not applicable for AeroNav 880 780 7 6 7 1 VHF COM Interfere...

Page 123: ...1547 7 6 11 AeroNav XXX Bezel and Display Lighting Verify the Bezel and Display Lighting for the AeroNav XXX can be set to an appropriate level for Day and Night flight conditions Likewise verify any...

Page 124: ...ft deviation TO indication flag stowed Glideslope Vertical Deviation Half scale up deviation flag stowed Annunciators All on Bearing to Waypoint RMI 135 Selected Course OBS 150 when interfaced to an H...

Page 125: ...n external source This can be verified on the Main Input Page in maintenance mode reference Section 7 5 5 If power is removed from the external heading source the Main Input Page will display dashed l...

Page 126: ...on the flight instruments PFD HSI CDI is correct Verify annunciation is correct and in the Pilot s field of view 8 2 VHF COM Flight Check Note This section is not applicable for AeroNav 880 780 Verif...

Page 127: ...arked as a Pass then the glove pilot combination is considered to be a qualified pair Pilot Name Description of Glove Verification Step Circle one Touch the standby frequency window and verify a virtu...

Page 128: ...Displayed on map and used for TA and FLTA functions The AeroNav is shipped from the factory with this database already loaded and updates are anticipated to be a rare occurrence Table 117 Database Upd...

Page 129: ...ou 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 Confir...

Page 130: ...tralian Nav Data 1 5 MB 30 sec Worldwide Nav Data 15 MB 7 Min For multiple AeroNav installations the database uploads must be performed individually for each AeroNav to be updated Due to some of the u...

Page 131: ...re are five types of datalogs employed in the AeroNav s System Log This log provides an in depth record of the navigation state From this log you can re create many aspects of the FMS output and AeroN...

Page 132: ...LSK to deselect all logs and then use the bottom right AeroNav knob to highlight the desired log and push in to generated a green check mark The Logs LSK on that Maintenance Mode page provides two opt...

Page 133: ...tions 3 It is the responsibility of maintenance personnel to ensure the identified part is recorded in the necessary maintenance logs 4 It is the maintenance personnel s responsibility to ensure that...

Page 134: ...XX 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 E...

Page 135: ...apply the cleaning solution directly on the cloth Never spray cleaner directly on the screen In general isopropyl alcohol is a safe and effective cleaner Methanol and most acidic solutions can be tox...

Page 136: ...sceptibility 11 Category X no test performed Sand and Dust 12 Category X no test performed Fungus Resistance 13 Category X no test performed Salt Spray 14 Category X no test performed Magnetic Effects...

Page 137: ...alified to Category S Curves B and M Explosive Atmosphere 9 Category X no test performed Waterproofness 10 Category X no test performed Fluids Susceptibility 11 Category X no test performed Sand and D...

Page 138: ...stall 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 the MyAerospace Honeywell com website Technical Publi...

Page 139: ...stallation 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 Ins...

Page 140: ...14 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 Figure C 2 AeroNav 780 800 Tray In...

Page 141: ...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 Figure C 3 AeroNav 880 900 Instrument...

Page 142: ...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 Figure C 4 AeroNav 780 800 Instrument...

Page 143: ...roNav AML STC Installation Manual for Helicopters Rev 0 Page C 5 Honeywell International Inc Do not copy without express permission of Honeywell Figure C 5 Typical GPS Antenna Installation Figure C 6...

Page 144: ...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 Figure C 7 AV 801 GPS Antenna Hol...

Page 145: ...016 0 025 Protruding Head Rivets 0 020 MS20470AD3 MS20426AD3 Double Dimple 0 032 0 050 Countersunk Skin Countersunk Rivets 0 032 NAS1097AD4 Countersunk NAS1097AD4 Countersunk 0 032 0 050 Protruding H...

Page 146: ...6 014 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 Figure C 9 Typical GPS Antenna...

Page 147: ...19 Figure D 14 VOR ILS Indicator Interconnect 21 Figure D 15 Main Indicator Interconnect 22 Figure D 16 Main Indicator KI209 Interconnect 23 Figure D 17 Main Indicator KI208 Interconnect 24 Figure D...

Page 148: ...Interconnect 49 Figure D 41 Avidyne AXP322 Trig TT22 Interconnect 50 Figure D 42 Avidyne Dual AXP322 Trig TT22 Interconnect 51 Figure D 43 FreeFlight FDL 978RX Interconnect 52 Figure D 44 GDL 88 Inte...

Page 149: ...0 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 Figure D 1 Lighting Power and Antenna Inter...

Page 150: ...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 2 of 3...

Page 151: ...TION CONFIGURATION PROCEDURE 5 MAXIMUM ALLOWABLE WIRE GAUGE INTO P1002 PINS IS 20 AWG 6 THE AIRCRAFT POWER INPUT P1006 44 PROVIDES POWER FOR THE VOR LOC SUPERFLAG P1006 15 AND GLIDESLOPE SUPERFLAG P10...

Page 152: ...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 Figure D 2 Blind Altitude Encoders I...

Page 153: ...N 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 Figure D 3 RS 232 Serial Data Interconn...

Page 154: ...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 2 of 2...

Page 155: ...3 0 INCHES CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL 3 IF THE GPS ARINC 429 IN 1 PORT P1001 48 AND 49 IS ALREADY USED FOR ANOTHER PURPOSE THE GPS ARINC 42...

Page 156: ...NAV 1 RECEIVER A LRN LNAV 1 RECEIVER B LRN LNAV 2 RECEIVER A LRN LNAV 2 RECEIVER B NAV 1 RECEIVER A NAV 1 RECEIVER B NAV 2 RECEIVER A NAV 2 RECEIVER B ARINC 429 EFIS DISPLAY 2 LNAV TRANSMITTER A LNAV...

Page 157: ...v AML STC Installation Manual for Helicopters Rev 0 Page D 9 Honeywell International Inc Do not copy without express permission of Honeywell Figure D 6 EHSI ARINC 429 Interconnect Dual AeroNav XXX San...

Page 158: ...SERIAL RELAY SENSE NAV 2 P2 33 COURSE OBS LEG GPS 1 OFF DEVIATION ANALOG IN GPS 2 OFF OBS ROT NORMAL CDI SRC SEL P2 3 OBS CAL 000 0 RCVR 1 2 P2 12 NAV 1 2 MUST TEMPORARILY BE SET TO ANALOG AND ILS MU...

Page 159: ...900 AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D 11 Honeywell International Inc Do not copy without express permission of Honeywell Figure D 7 ARINC 429 RS 232 Air Data IRU AHRS I...

Page 160: ...ROUNDS TO BACK PLATE THE SHIELD LEADS MUST BE LESS THAN 3 0 INCHES CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL 3 IF THE GPS ARINC 429 IN 1 PORT P1001 48 AND...

Page 161: ...S ARINC 429 IN B GPS ARINC 429 OUT A GPS ARINC 429 OUT B NAV ARINC 429 IN A NAV ARINC 429 IN B NOTES 1 ALL WIRES TO BE 22 AWG OR GREATER UNLESS OTHERWISE NOTED 2 AT AERONAV UNIT TERMINATE SHIELD GROUN...

Page 162: ...PR STB POWER SWITCH HI POWER SWITCH LO 429 TX 1A 429 TX 1B DISPLAY GROUND SOFT KEY 1 TEST ALT SOFT KET 4 OPR STB POWER SWITCH HI POWER SWITCH LO RS 232 RX 2 RS 232 TX 2 RS 232 GROUND 2 REMOTE MUTE TRA...

Page 163: ...UIRED NEAR THE AERONAV UNIT INDICATING THAT A TRAFFIC ADVISORY SYSTEM IS INSTALLED AND ITS DATA MAY BE DISPLAYED ON THE AERONAV UNIT 6 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INT...

Page 164: ...046 014 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 Figure D 10 GTX 330 Intercon...

Page 165: ...4 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 Figure D 11 Terrain and Weather In...

Page 166: ...046 014 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 Figure D 12 Weather Intercon...

Page 167: ...30 10 14 17 19 18 20 NA NA 7 12 8 13 26 32 27 33 8 13 6 14 25 34 NA NA 9 13 10 14 11 15 12 30 GND LUG 17 19 18 20 NA NA 9 10 GND LUG P H R V GND LUG 12 13 GND LUG NA NA 9 10 GND LUG P H R V GND LUG 12...

Page 168: ...HER INTERCOM SYSTEM IN THE AIRCRAFT 6 INTERCOM WIRING OPTION 7 THE COM REMOTE TRANSFER INPUT P1002 15 MAY BE USED FOR EMERGENCY OPERATION OF THE COM TRANSMITTER IF THE REMOTE TRANSFER SWITCH IS ACTIVE...

Page 169: ...28 25 24 Navigation Indicator LEFT RIGHT TO FROM NAV FLAG NAV FLAG NAV SUPERFLAG NAV SUPERFLAG LO VOR LOC COMPOSITE ILS ENERGIZE UP DOWN GLIDESLOPE FLAG GLIDESLOPE FLAG GLIDESLOPE SUPERFLAG GLIDESLOP...

Page 170: ...REATER UNLESS OTHERWISE NOTED FACTURER S DOCUMENTATION FOR COMPLETE PINOUT AND INTERCONNECT INFORMATION PINOUTS OF OTHER UNITS FERENCE ONLY IT TERMINATE SHIELD GROUNDS TO THE CONNECTOR BACKSHELL OR US...

Page 171: ...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 LNAV OBS EXCITATION I...

Page 172: ...20 21 43 42 48 3 9 50 2 15 14 Navigation Indicator 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 LN...

Page 173: ...NUNCIATOR VLOC ANNUNCIATOR UP DOWN GLIDESLOPE FLAG GLIDESLOPE FLAG RESOLVER H RESOLVER C RESOLVER D RESOLVER E RESOLVER F RESOLVER G THERWISE NOTED AL DEVIATION INDICATOR DO NOT USE FOR IFR R COMPLETE...

Page 174: ...CK OBI DATA OBI SYNC KI 229 KNI 582 Pointer 1 KNI 582 Pointer 2 KDA 692 P2291 P5821 P5821 P6921 Bendix King Radio Magnetic Indicator 12 19 11 8 17 33 7 16 24 11 L M OBI CLOCK OBI DATA OBI SYNC ED BUTT...

Page 175: ...2MHZ P1006 19 18 20 22 21 AERONAV XXX 2 SERIAL DME DATA SERIAL DME CLOCK SER DME CHAN REQ PAR DME 4MHZ DME COMMON SER DME RNAV MODE PAR DME 2MHZ P1006 19 18 20 22 21 KN 62 62A KN 64 P621 P62A1 P641 B...

Page 176: ...0 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 Figure D 21 King Serial DME Tuning Interco...

Page 177: ...4 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 Figure D 22 Parallel DME Tuning In...

Page 178: ...LLEL DME 1MHZ PARALLEL DME 800KHZ PARALLEL DME 400KHZ PARALLEL DME 200KHZ PARALLEL DME 100KHZ PARALLEL DME 50KHZ DME COMMON P1006 14 20 21 33 37 39 40 42 43 22 KN 61 KN 65 P611 P651 Bendix King Parall...

Page 179: ...46 014 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 Figure D 24 Autopilot Interco...

Page 180: ...roNav AML STC Installation Manual for Helicopters Rev 0 Page D 32 Honeywell International Inc Do not copy without express permission of Honeywell Figure D 25 External Navigation Source and GPS Annunci...

Page 181: ...ECT CDI SOURCE SELECT 7 8 2 4 6 3 1 8 3 9 10 24 20 12 2 1 8 3 9 10 24 20 12 2 1 8 3 9 10 24 20 12 4 EATER UNLESS OTHERWISE NOTED S REQUIRED INDICATORS ON THIS PAGE ARE SUITABLE TO IREMENT N IS VLOC GP...

Page 182: ...0046 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 Figure D 26 Switch Intercon...

Page 183: ...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 Figure D 27 Garmin GAD 42 Inter...

Page 184: ...6 014 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 Figure D 28 Garmin G600 Interc...

Page 185: ...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 Figure D 29 Avidyne EX500 600 5000...

Page 186: ...SN 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 Figure D 30 Aspen EFD1000 Interconnec...

Page 187: ...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 Figure D 31 Aspen EFD1000 Interconn...

Page 188: ...6 014 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 Figure D 32 Transponder Interc...

Page 189: ...00046 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 Figure D 33 ELT Interconne...

Page 190: ...CTOR BACKSHELL OR USE CARD EDGE CONNECTOR TO TERMINATE SHIELD GROUNDS TO BACK PLATE 3 WIRE HARNESS OVERBRAID IS NOT SHOWN BUT MAY BE REQUIRED 4 REFER TO MANUFACTURER S DOCUMENTATION FOR COMPLETE PINOU...

Page 191: ...046 014 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 Figure D 35 RDR2000 Intercon...

Page 192: ...046 014 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 Figure D 36 GTX 335 Intercon...

Page 193: ...N 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 Figure D 37 GTX 345 Interconnect see b...

Page 194: ...AV 780 800 UNITS DO NOT DRIVE AUDIO INHIBIT IN AERONAV 780 800 UNITS SIMULTAINEOUS TIS B AND FLTA AURAL ANNUNCIATIONS ARE POSSIBLE ADDRESSED IN AFMS 5 AERONAV SERIAL PORTS RS232 AND ARINC 429 OTHER TH...

Page 195: ...46 014 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 Figure D 38 GTX 330ES Interco...

Page 196: ...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 Figure D 39 Robinson Analog Inte...

Page 197: ...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 Figure D 40 Robinson Aspen EFD100 I...

Page 198: ...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 Figure D 41 Avidyne AXP322 Trig TT22...

Page 199: ...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 Figure D 42 Avidyne Dual AXP322 Trig TT...

Page 200: ...4 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 Figure D 43 FreeFlight FDL 978RX I...

Page 201: ...0046 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 Figure D 44 GDL 88 Intercon...

Page 202: ...AeroNav AML STC Installation Manual for Helicopters Rev 0 Page D 54 Honeywell International Inc Do not copy without express permission of Honeywell Figure D 45 Avidyne AXP340 Trig TT31 Interconnect Fi...

Page 203: ...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 Figure D 47 Single GDU700 1060 PFD...

Page 204: ...4 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 Figure D 48 Dual GDU700 1060 PFD I...

Page 205: ...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 Figure D 49 Garmin G5 EHSI Inte...

Page 206: ...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 Figure D 50 Garmin G5 EADI Inte...

Page 207: ...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 Figure D 51 Garmin G5 EFIS Inte...

Page 208: ...046 014 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 Figure D 52 NGT9000R Interco...

Page 209: ...0046 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 Figure D 53 KT 74 Interconn...

Page 210: ...enna is mounted on top of the aircraft Verify antenna is clear of hangars buildings etc Interference Verify another piece of aircraft equipment is not interfering with the GPS system VHF Com is not tr...

Page 211: ...Chassis ID per section 7 3 Unit starts up in Maintenance Mode USB fob installed at power up AeroNav last shut down in Maintenance Mode Ensure fob is not in the USB slot and reapply power to the AeroN...

Page 212: ...0 W or GNS 430 W being replaced WAAS Enabled 530W or 430W with approved antenna Yes No 2nd unit Yes No N A 530 W or 430 W Hardware Part Number and Revision Number back of unit or aircraft logs _______...

Page 213: ...n of Devices Connected to the GNS 530 W or GNS 430 W 1st GNS 530 W or GNS 430 W 2nd GNS 530 W or GNS 430 W if applicable Traffic Datalink Lightning Sensor Autopilot Fuel Flow System Display s CDI s RM...

Page 214: ...oftware and then pressing the Download Logs LSK followed by the Confirm LSK These tables contain all the data that can be entered at time of installation to ensure the AeroNav XXX is properly configur...

Page 215: ...XXX Main ARINC 429 Config Page 1 12 Speed Data In 1 In 2 Out SDI VNAV For new AeroNav 880 900 installations see Section 7 5 2 for selections and descriptions AeroNav XXX Main RS232 Config Page 2 12 I...

Page 216: ...if present CONFIGURE Discretes GPS SELECT COM PRESETS Note Com Presets are always enabled on the AeroNav XXX GNS 530 W or 430 W MAIN SYSTEM CONFIG Page Airframe if present CONFIGURE Airframe AIRFRAME...

Page 217: ...L FF TAS CDI R FF W SPD T FF T FOB JOYSTICK WPT GNS 530 W or 430 W INSTRUMENT PANEL SELF TEST For reference only CDI FUEL CAPACITY FLG VCDI FUEL ON BOARD VFLG TO FRM FUEL FLOW ANNUN RMI Set Fuel Flow...

Page 218: ...SOURCE RESP TIME MIN SLOPE OFFSET PHOTO TRANS if applicable PHOTO SLP OFST if applicable AeroNav XXX MAIN LIGHTING Page 5 12 Bezel Display Photo Response Time Photo Slope Photo Minimum Photo Maximum d...

Page 219: ...DE EXTERNAL SWITCH STATE RMT CDI OBS DISCRETE TOGGLE APR OBS ILS GPS APR GPS TERM INTEG VLOC MSG WPT Note Check off the squares as required to match the solid squares on the GNS 530 430 unit these che...

Page 220: ...Page 7 12 CDI NAV FLAG TO FROM LAT VERT SELECTED COURSE Ignore SEL CRS for GPS Ignore SEL CRS for VLOC CDI OBI SOURCE V FLAG STATE For new AeroNav XXX installations see Section 7 5 8 for selections a...

Page 221: ...NEL MODE For new AeroNav XXX installations see Section 7 5 9 for selections and descriptions GNS 530 W or 430 W VOR LOC GS ARINC 429 CONFIG Page GNS 530W 430W Only RX TX SPEED SDI DME MODE AeroNav XXX...

Page 222: ...YNC REF HDG VALID Note Squares should all be green if no issues GNS 530 W or 430 W STORMSCOPE TEST Page if configured for Stormscope MODE STATUS TRIGGER COUNT HDG AeroNav XXX STORMSCOPE CONFIG Page So...

Page 223: ...IM A if 429 interface LIM B if 429 interface HDG if 429 interface BARO ALT if 429 interface RAD ALT if 429 interface TEST MODE if 429 interface AeroNav XXX STORMSCOPE DATA Page Software version 10 2 o...

Page 224: ...GNS 530 W or 430 W GAD 42 Config Page if configured for an ARINC 429 input from GAD 42 MAIN RMI OBI ROLL STEERING NAV RMI OBI REMOTE CRS SEL SEL CRS DRIVE TAS INPUT DIST SERIAL GPS NAV 429 L H HEADING...

Page 225: ...WS CONFIG VOICE GENDER VOLUME PLAY AUDIO MSG GNS 530 W or 430 W TAWS Audio Config Page 2 if installed ALERT Reduced Terrain Clearance CAUT WARN ALERT Reduced Obstacle Clearance CAUT WARN ALERT Imminen...

Page 226: ...ission of Honeywell GNS 530 W or 430 W GDL Config Page if installed ATTENUATION MODEL if displayed GNS 530 W or 430 W DATALINK DIAGNOSTICS Page if installed QOS TERR SAT 1 SAT 2 TUNER AeroNav XXX GDL...

Page 227: ...N 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...

Page 228: ...Honeywell International Inc Do not copy without express permission of Honeywell...

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