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Garmin GNC 420AW, Installation Manual

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Garmin GNC 420AW Installation Manual Download Page 95

 

400W Series Installation Manual 

 

Page 5-11 

190-00356-02  

Rev. G 

5.3.6 

INSTRUMENT PANEL SELF-TEST Page 

Select the INSTRUMENT PANEL SELF-TEST Page (see 
Figure 5-8).  This page allows verification that the 400W 
Series unit is communicating properly with other 
instruments.  Compare on-screen indications with the 
information depicted on connected instruments, such as the 
CDI, HSI, RMI and/or external annunciators.  It also 
displays fuel capacity, amount on-board, and flow. 

 

 

5.3.7 

MAIN LIGHTING Page 

Select the MAIN LIGHTING Page (see Figure 5-9).  This 
page allows you to set display parameters that affect the 
display backlight and key lighting brightness.  The 
DISPLAY and KEY lighting characteristics are adjusted 
separately, each with the following fields: 

 

LIGHTING 

Shows the current level of display backlighting, based on 
the lighting input source (lighting bus voltage, or the ambient light if the source is 

PHOTO

) and the 

settings on this configuration page.  This field has a range of 0 (zero) to 9999. 

SOURCE 

Selection Description 

PHOTO 

Backlight level is determined by the ambient light level as measured 
by the photocell on the 400W Series unit. 

14V DC 

Backlight level tracks a 14 volt DC aircraft lighting bus. 

28V DC 

Backlight level tracks a 28 volt DC aircraft lighting bus. 

5V DC 

Backlight level tracks a 5 volt DC aircraft lighting bus. 

5V AC 

Backlight level tracks a 5 volt AC aircraft lighting bus. 

 

RESP TIME - 

(Response Time)  

Sets the speed with which the brightness responds to the input level (bus voltage or ambient light) 
changes.  The higher the number the slower the display responds.  This field has a range of 3 to 7, and is 
set to 4 at the factory. 

MIN - 

(Minimum)  

Sets the minimum brightness of the display.  The higher the number, the brighter the minimum 
brightness.  Display minimum brightness has a range of 35 to 999, and is set to 80 at the factory.  Key 
minimum brightness has a range of 20 to 99, and is set to 40 at the factory.  It is prudent to verify that 
display and key lighting characteristics match those of other equipment in the panel under night lighting 
conditions. 

 

Figure 5-8.  INSTRUMENT PANEL 

SELF-TEST Page 

 

Figure 5-9.  MAIN LIGHTING Page 

Summary of Contents for GNC 420AW

Page 1: ...v G 400W SERIES INSTALLATION MANUAL GPS 400W GNC TM 420W 420AW and GNS TM 430W 430AW GNC and GNS are trademarks of Garmin Ltd or its subsidiaries and may not be used without the express permission of Garmin Garmin International Inc ...

Page 2: ...400W Series Installation Manual 190 00356 02 Rev G ...

Page 3: ...Address www garmin com Garmin Europe Ltd Liberty House Bull Copse Road Hounsdown Business Park Southampton SO40 9RB UK Telephone 44 0 8708501243 RECORD OF REVISIONS Revision Revision Date Description A 11 2 06 Production Release B 11 28 06 Added GA 35 antenna information and corrected wire gauge for main connector power C 4 5 07 Incorporated customer feedback D 10 1 07 Incorporated main software v...

Page 4: ...ed to be taken to display an alternate traffic color 5 41 Checkout Log Added V Flag State to Main CDI OBS Configuration section 6 6 6 2 Added check GPS Antenna to the Alert Text GPS is not responding in Table 6 2 H 51 Appendix H Updated Figure H 32 to include note that the ILS GPS approach discrete is required by some CDIs HSIs that are used with the M4C D Autopilots G H 55 Appendix H Updated Figu...

Page 5: ...er Section 2410 of the Export Administration Act of 1979 Include this notice with any reproduced portion of this document WARNING This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This Notice is being provided in accordance with California s Proposition 65 If you have any questions or would like addit...

Page 6: ...ts 1 11 1 6 Regulatory Compliance 1 12 1 6 1 TSO Authorization and Advisory Circular Reference 1 12 1 6 2 TSO Deviations 1 14 1 6 3 ETSO Authorization 1 15 1 6 4 ETSO Deviations 1 16 1 6 5 FCC Grant of Equipment Authorization 1 16 1 7 Database Options and Updates 1 17 1 7 1 Aviation Database 1 17 1 7 2 Terrain Database 1 17 1 8 Fault Detection and Exclusion FDE 1 17 1 9 Limited Warranty 1 18 2 INS...

Page 7: ...mputer Interface Approval 2 12 2 9 3 Audio Panel Interface Approval 2 13 3 INSTALLATION PROCEDURES 3 1 3 1 Unit and Accessories 3 1 3 2 Optional Accessories 3 2 3 2 1 GPS Antenna Options 3 2 3 2 2 GPS Antenna Doubler 3 3 3 2 3 Other Accessories 3 3 3 3 Database Options 3 3 3 4 Miscellaneous Options 3 3 3 5 Optional Reference Material 3 3 3 6 Installation Materials Required but Not Provided 3 4 3 6...

Page 8: ...cteristics 4 7 4 4 3 Main Indicator Configuration 4 8 4 4 4 Main Indicator Calibration and Checkout 4 8 4 4 5 Main Indicator Interconnect 4 8 4 5 Annunciators Switches 4 9 4 5 1 Annunciators Switches Function 4 9 4 5 2 Annunciators Switches Electrical Characteristics 4 11 4 5 3 Annunciators Switches Configuration 4 11 4 5 4 Annunciators Switches Calibration and Checkout 4 11 4 5 5 Annunciators Swi...

Page 9: ...Electrical Characteristics 4 21 4 10 3 DME Tuning Configuration 4 22 4 10 4 DME Tuning Calibration and Checkout 4 22 4 10 5 DME Tuning Interconnect References 4 22 5 POST INSTALLATION CONFIGURATION CHECKOUT PROCEDURES 5 1 5 1 Mounting and Wiring Check 5 1 5 2 Connector Engagement Check 5 1 5 3 Configuration Mode Operations 5 1 5 3 1 MAIN ARINC 429 CONFIG Page 5 2 5 3 2 MAIN RS 232 CONFIG Page 5 5 ...

Page 10: ... Sensor and Fuel Air Data Computer 5 26 5 4 5 Altitude Encoder Gray Code Connection 5 26 5 4 6 AHRS IRU Interface Check 5 27 5 4 7 GAD 42 Interface Check 5 27 5 4 8 Lighting Bus Interface Check 5 27 5 5 Ground Checks Normal Mode 5 28 5 5 1 Display of Self Test Data 5 28 5 5 2 Signal Acquisition Check 5 29 5 5 3 VHF COM Interference Check 5 29 5 5 4 VHF NAV Checkout GNS 430W 5 31 5 5 5 VHF COM Chec...

Page 11: ... 8 1 Equipment Calibration 8 1 8 2 VOR Checks 8 1 8 3 Cleaning 8 1 8 4 Battery Replacement 8 1 APPENDIX A ENVIRONMENTAL QUALIFICATION FORM A 1 APPENDIX B STC DATA B 1 B 1 STC Information B 1 B 2 Permission to use STC B 1 B 3 Continued Airworthiness Instructions B 1 B 4 STC Approved Model List B 1 APPENDIX C RESERVED C 1 APPENDIX D 400W SERIES RS 232 AVIATION DATA FORMAT D 1 D 1 Electrical Interfac...

Page 12: ... Autopilots G 3 G 5 Encoding Altimeter or Blind Encoder Gray Code G 4 G 6 EFIS Displays G 4 G 7 EHSI G 4 G 8 IRU AHRS G 5 G 9 NAV Indicator G 5 G 10 Weather Traffic and Terrain G 5 G 11 DME G 6 G 12 CDI HSI Source Selection Annunciators G 6 G 13 Multifunction Displays G 7 G 14 Interface Adapters G 7 APPENDIX H STC APPROVED INSTALLATION DIAGRAMS H 1 H 1 Introduction H 1 H 2 Drawing List H 1 ...

Page 13: ...ement of GPS Vertical Offset 5 20 Figure 5 20 GPS Vertical Offset Page 5 20 Figure 5 21 STORMSCOPE CONFIG Page 5 21 Figure 5 22 STORMSCOPE TEST Page 5 21 Figure 5 23 STORMSCOPE DOWNLOAD DATA Page 5 21 Figure 5 24 TRAFFIC Page SkyWatch 5 22 Figure 5 25 TRAFFIC Page TCAD 5 22 Figure 5 26 RYAN TCAD CONFIG Page 5 23 Figure 5 27 GAD 42 CONFIG Page 5 23 Figure 5 28 GDL CONFIG Page 5 23 Figure 5 29 Data ...

Page 14: ...5 Figure H 29 External Navigation Source and GPS Annunciators H 47 Figure H 30 Parallel Slip Code DME Tuning Interconnect H 49 Figure H 31 Cessna Autopilot Interconnect H 50 Figure H 32 Bendix Autopilot Interconnect H 51 Figure H 33 Switches Interconnect H 52 Figure H 34 ARINC 429 Avidyne PFD MFD Interconnect H 53 Figure H 35 Collins Autopilot Interconnect H 55 Figure H 36 Garmin GAD 42 Interconne...

Page 15: ...tin date and the purpose of the modification The table is current at the time of publication of this manual see date on front cover and is subject to change without notice Authorized Garmin Sales and Service Centers are encouraged to access the most up to date bulletin and advisory information on the Garmin Dealer Resource web site at www garmin com using their Garmin provided user name and passwo...

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Page 17: ...re specifically noted references made to the GNC 420W will apply equally to GNC 420AW Table 1 1 400W Series Units MODEL PART NUMBER COLOR NOTES GPS 400W 011 01057 00 BLACK 011 01057 10 GRAY 011 01057 40 BLACK NOTE 1 011 01057 50 GRAY NOTE 1 GNC 420W 011 01058 00 BLACK 011 01058 10 GRAY 011 01058 40 BLACK NOTE 1 011 01058 45 BLACK 28 VDC UPGRADE UNIT 011 01058 50 GRAY NOTE 1 GNC 420AW 011 01059 00 ...

Page 18: ...ems GPS or GPS with Wide Area Augmentation Systems GPS WAAS Referred to as Global Navigation Satellite Systems GNSS Equipment as revised Regardless of applicability of the AML STC or alternative field approval application for installation and operational approval prior to completing the installation and before returning the airplane to service the installer or other appropriately certificated pers...

Page 19: ...r telephones installed in or carried aboard aircraft Ground based cellular telephones must not be operated while aircraft are off the ground When any aircraft leaves the ground all ground based cellular telephones on board that aircraft must be turned off Ground based cell phones that are on even in a monitoring state can disrupt GPS performance 1 4 Technical Specifications 1 4 1 Physical Characte...

Page 20: ...um GNC 420W GNC 420AW Main Connector 1 2 A 28 VDC maximum 2 5 A 14 VDC maximum GNS 430W GNS 430AW Main Connector 1 2 A 28 VDC maximum 2 5 A 14 VDC maximum GNC 420W GNS 430W COM Connector 15 mA 28 VDC receive 3 0 A 28 VDC transmit 15 mA 14 VDC receive 6 0 A 14 VDC transmit GNC 420AW GNS 430AW COM Connector 15 mA 28 VDC receive 3 0 A 28 VDC transmit Superflag Power Requirements 500 mA maximum per su...

Page 21: ...ition Accuracy 1 25 meter RMS horizontal 2 meter vertical with WAAS Velocity 1000 knots maximum above 60 000 ft TTFF Time To First Fix 1 45 min typical with current almanac position and time Reacquisition 10 seconds typical Position Update Interval 0 2 sec 5 Hz 1 PPS Pulse Per Second 275 Nsec of UTC second Datum WGS 84 SATCOM Compatibility SATCOM compatibility is dependent upon antenna selection S...

Page 22: ...7 37 kHz for 8 33 kHz channeling Spurious Response Greater than 85 dB Modulation AM Double sided Emission Designator 6K00A3E Frequency Band 118 00 to 136 99 MHz 25 kHz and 8 33 kHz channel spacing Transmitting Power GNS 420W GNS 430W 10 watts minimum 15 watts maximum GNS 420AW GNS 430W 16 watts minimum 20 watts maximum Transmitter Duty Cycle Recommended 10 maximum Modulation Capability The modulat...

Page 23: ...S N N shall not be less than 6 dB Course Deviation Sensitivity 103 5 dBm or less for 60 of standard deflection Flag The LOC Course Deviation Flag must be flagged a in the absence of an RF signal b When either the 90 or 150 Hz modulating signals is removed and the other is maintained at its normal 20 c In the absence of both 90 and 150 Hz modulation d When the level of a standard localizer deviatio...

Page 24: ...ncies displaced by 132 kHz or greater the input signal is at least 60 dB down Standard deflection a With a standard deflection FLY DOWN condition 90 Hz dominant the output shall be 78 mV 7 8 mV b With a standard deflection FLY UP condition 150 Hz dominant the output shall be 78 mV 7 8 mV Flag The unit Flags a When the level of a standard deviation test signal produces 50 or less of standard deflec...

Page 25: ... 00 GA 35 GPS WAAS Screw mount Teardrop footprint 1 TNC Aero Antenna AT575 93GW TNCF 000 RG 27 NM 013 00235 00 Garmin 013 00244 00 013 00244 00 GA 36 GPS WAAS Screw mount ARINC 743 TNC Aero Antenna AT575 126GW TNCF 000 RG 27 NM 013 00244 00 Garmin 013 00245 00 013 00245 00 GA 37 GPS WAAS XM Screw mount ARINC 743 TNC TNC Aero Antenna AT2300 126GW TNCF 000 RG 27 NM 013 00245 00 Comant GPS WAAS VHF 3...

Page 26: ...op Footprint 1 BNC Garmin 011 01111 00 010 10561 01 GA 57 GPS WAAS and FIS Antenna 3 Screw Mount ARINC 743 Footprint BNC TNC 4 Garmin 011 01032 00 010 10604 00 Garmin AT 590 1104 N A A33 GPS WAAS Antenna Screw Mount TNC Aero Antenna AT575 9UW TNCF 000 05 26 NM N A Garmin AT 590 1112 013 00113 00 A34 GPS WAAS Antenna Screw Mount Teardrop Footprint 2 TNC Aero Antenna AT575 93W TNCF 000 05 26 NM 013 ...

Page 27: ...tion for a license on FCC form 404 Application for Aircraft Radio Station License The FCC also has a fax on demand service to provide forms by fax Outside the US contact the responsible telecommunication authority The GNC 420W GNC 420AW GNS 430W and GNS 430AW owner accepts all responsibility for obtaining the proper licensing before using the transceiver The maximum transmitting power modulation i...

Page 28: ...W 500W Series STC SA01933LA the TSO design approval has been determined to be adequate by the STC which constitutes the separate installation design approval Table 1 4 TSO Authorization Models Function TSO Minimum Performance Standard GPS 400W GNC 420W GNC 420AW GNS 430W GNS 430AW ILS Glideslope TSO C34e RTCA DO 192 ILS Localizer TSO C36e RTCA DO 195 VHF COM Transmitter 100nm range TSO C37d RTCA D...

Page 29: ...errain D NOTE Unauthorized changes or modifications to any 400W Series product may void the compliance to required regulations and authorization for continued equipment usage All 400W Series unit functions are design approved under the TSO Airworthiness approval for installation and operational use is recognized under AML STC SA01933LA If additional information drawing lists and software documenta...

Page 30: ...ad of RTCA DO 160B as the standard for Environmental Conditions and Test Procedures for Airborne Equipment 1 Garmin was granted a deviation from TSO C113 section 2 1 2 4 to use RTCA DO 178B instead of RTCA DO 178A to demonstrate compliance for the verification and validation of the computer software TSO C113 2 Garmin was granted a deviation from TSO C113 section 2 1 2 3 to use RTCA DO 160D instead...

Page 31: ...itation e The ability to use 128 dBmic as the minimum SBAS satellite signal in space for the purpose of assessing the operational limitation NOTE 1 C146a cont d 8 Garmin was granted a deviation from TSO C146a paragraph 2 1 1 9 to use 20 seconds instead of 10 seconds to reacquire a dropped satellite under the conditions described in the paragraph The 20 second period is the time period specified by...

Page 32: ...ssed approach with manual action It shall be possible to take this action before crossing the MAWP Missed Approach Waypoint in which case the equipment shall automatically initiate the missed approach procedure at the MAWP 5 Garmin was granted a deviation from RTCA DO 229C not to implement paragraph 2 2 4 2 3 which states If the aircraft is past the FPAP length offset and the pilot has not already...

Page 33: ... Garmin Terrain database updates can be accomplished by replacing or reprogramming the database card and inserting the updated card in the right card slot on the unit front panel The Terrain database can be downloaded via the internet and the card programmed using a USB programmer available from Garmin Contact Garmin at 800 800 1020 or www garmin com for more information or instructions 1 8 Fault ...

Page 34: ... misuse accident or unauthorized alteration or repairs SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE STATUTORY OR OTHERWISE THIS WARRA...

Page 35: ...re closing the work area in case problems occur 2 2 Minimum System Configuration 2 2 1 VFR Installation The minimum 400W Series unit installation requires the following items for a VFR Installation GNS 400W Series unit installed in the aircraft manufacturer approved location for 6 25 inch wide avionics equipment GPS antenna is required for GPS navigation functions An external CDI is required for i...

Page 36: ...e is not required by the 400W Series unit to meet the requirements of TSO C146a 2 3 1 Multiple Uncorrected Pressure Altitude Sources The 400W Series can accept altitude from a Gray code or RS 232 altitude encoder fuel air data computer FADC ARINC 429 air data computer ADC ARINC 429 EFIS and ARINC 429 traffic advisory system If multiple sources of altitude data are supplied to the 400W Series unit ...

Page 37: ...ries unit STC For mounting the GPS WAAS antenna refer to Garmin GA Antenna AML STC SA01695SE or other FAA approved data For mounting the COM NAV and Glideslope antennas refer to the aircraft manufacturer s data 2 4 1 GPS Antenna Location The GPS antenna is a key element in the overall system performance and integrity for a GPS WAAS navigation system The mounting location geometry and surroundings ...

Page 38: ...PS antenna or XM antenna 4 To maintain a constant gain pattern and limit degradation by the windscreen avoid mounting the antenna closer than 3 inches from the windscreen 5 For multiple GPS installations the antennas should not be mounted in a straight line from the front to the rear of the fuselage Also varying the mounting location will help minimize any aircraft shading by the wings or tail sec...

Page 39: ...400W Series Installation Manual Page 2 5 190 00356 02 Rev G Figure 2 1 GPS Antenna Installation Considerations ...

Page 40: ...he GNC 420W or GNS 430W COM antenna ELT antenna and DF receiver antenna is critical Use the following guidelines in addition to others in this document when locating the 400W Series unit and its antennas GPS Antenna Locate as far as possible from all COM antennas and all COM transceivers including the 400W Series COM ELT antennas and DF receiver antennas The GPS antenna is less susceptible to harm...

Page 41: ...on annunciation requirement In addition any required GPS navigation annunciations must be within 16 805 inches of the pilot view centerline If the 400W Series unit display is within this area then no external GPS navigation annunciations are required The 400W Series unit as a redundant or secondary TSO C146a certified navigation device may be installed outside the acceptable view parameters if the...

Page 42: ...be within the acceptable field of view if the following criteria are met The left edge of the 400W Series unit is within 11 8 inches of the primary view centerline and the top edge of the 400W Series unit is no lower than the bottom edge of the primary flight instruments or the unit is line abreast with the affected CDI 4 If the 400W Series unit is mounted to the left of the primary instruments th...

Page 43: ... are met The left edge of the 400W Series unit is within 13 4 inches of the primary view centerline and the top edge of the 400W Series unit is no lower than the bottom edge of the primary flight instruments or the unit is line abreast with the affected CDI 4 If the 400W Series unit is mounted to the left of the primary instruments the internal display of annunciation within the 400W Series unit i...

Page 44: ...NOTE The entire annunciator unit must be within the acceptable field of view The external GPS Navigation annunciator unit must contain at a minimum the following annunciations INTEG INTG or LOI TERM APR MSG WPT Figure 2 3 GPS Navigation Annunciation Field of View ...

Page 45: ... as appropriate Use 22 to 24 AWG wire for all connections except for power Use 20 AWG for power and ground Avoid sharp bends 2 7 Air Circulation and Cooling The 400W Series units meet all TSO requirements without external cooling However as with all electronic equipment lower operating temperatures extend equipment life On the average reducing the operating temperature by 15 to 20 C 27 to 36 F dou...

Page 46: ...ng only LNAV If these conditions are met the interface can be approved under AML STC SA01933LA These autopilots are limited to those operations for which they were previously FAA approved when interfaced with the other TC d or STC d navigation units e g if the previous unit was installed and approved for coupled VOR ILS LOC BC and GPS LNAV approaches this upgraded installation will also be approve...

Page 47: ...io panels not listed in Appendix G can still be approved under 400W 500W Series AML STC SA01933LA if all of the following conditions are met The installation of the audio panel was previously FAA approved The VHF COM audio and VHF NAV audio if applicable must be verified as described in sections 5 5 4 and 5 5 5 If these conditions are met the interface can be approved under AML STC SA01933LA ...

Page 48: ...Page 2 14 400W Series Installation Manual Rev G 190 00356 02 This page intentionally left blank ...

Page 49: ...411 40 010 00411 41 011 01059 40 BLK 16W 28 X 010 00411 50 010 00411 51 011 01059 50 GRY 16W 28 X GNS 430W 010 00412 00 010 00412 01 011 01060 00 BLK 10W X 14 28 010 00412 10 010 00412 11 011 01060 10 GRY 10W X 14 28 010 00412 40 010 00412 41 011 01060 40 BLK 10W X 14 28 X 010 00412 45 010 00412 46 011 01060 45 BLK 16W X 28 X 010 00412 50 010 00412 51 011 01060 50 GRY 10W X 14 28 X GNS 430AW 010 0...

Page 50: ... the doubler To connect the GPS antenna coaxial cable to the antenna a TNC plug is required GA 36 Antenna GA 36 Antenna Garmin P N 013 00244 00 contains the following items ITEM PART NUMBER QTY 013 00244 00 Garmin GA 36 GPS WAAS Antenna 1 AT575 126G Aero Antenna 1 1 Antenna includes 8 32 UNC 2A x 1 00 SS 303 mounting screws qty 4 and O ring qty 1 An antenna doubler may also be required Refer to Se...

Page 51: ... Options ITEM GARMIN P N Data Card World Wide 010 10546 00 Data Card Americas 010 10546 01 Data Card International 010 10546 02 Data Card Taws Terrain 128 MB Note 1 010 10201 20 Data Card Taws Terrain 256 MB Note 1 010 10201 21 Note 1 Data cards 010 10201 20 and 010 10201 21 are functionally equivalent 3 4 Miscellaneous Options ITEM GARMIN P N Connector BNC Male Clamp 330 00087 00 GPS 1 57542 GHz ...

Page 52: ... splitter used with the VOR LOC antenna GNS 430W Only Headphones 500Ω nominal impedance GNC 420W and GNS 430W Only Microphone Low impedance carbon or dynamic with transistorized pre amp GNC 420W and GNS 430W Only For a list of optional accessories and source selection annunciators refer to Appendix G 3 6 2 Materials Required But Not Supplied New Installations Only The 400W Series unit is intended ...

Page 53: ...r Insertion Extraction Tool Positioner Insertion Extraction Tool Positioner Insertion Extraction Tool Military P N M22520 2 01 M22520 2 09 M81969 1 04 N A M81969 1 02 M22520 2 08 M81969 1 02 Positronic 9507 9502 3 M81969 1 04 9502 11 M81969 1 02 9502 5 M81969 1 02 ITT Cannon 995 0001 584 995 0001 739 N A N A N A 995 0001 604 980 2000 426 AMP 601966 1 601966 6 91067 1 N A N A 601966 5 91067 2 Danie...

Page 54: ...3 1 If the connector is provided by the installer follow the connector manufacturer s instructions for cable preparation Figure 3 1 Coaxial Cable Installation The card edge connector may be used to terminate shield grounds to the 400W Series back plate Feed wires through the connector backshells before insertion into the 25 44 and 78 pin connectors Contacts for the 25 44 and 78 pin connectors must...

Page 55: ...n the installation kit the installer may use contacts made by ITT Cannon under P N 031 1007 001 These contacts require the use of a different crimp tool positioner than shown in the table with the part numbers as follows Daniels P N K250 Astro P N 616245 or ITT Cannon P N 980 0005 722 3 For the card edge connector pin contacts use AMP part number 90272 1 or equivalent crimping tool To prevent a po...

Page 56: ...ll the rack in the aircraft panel using six 6 32 flat head screws and six self locking nuts The screws are inserted from the inside through the holes in the sides of the rack 4 If the back plate was previously removed see Step 1 replace the back plate by positioning the tabs on the back plate in the slots of the left side of the rack viewing it from the cockpit and attaching it by replacing the tw...

Page 57: ... loss to the cable and should be considered when computing the cable loss A typical loss of 0 2 dB can be used for each connection To maintain integrity of the WAAS signal the GPS antenna coaxial cable must have a minimum of two shields e g RG 400 or RG 142B NOTE If RG 142B or RG 400 is used 1 5 dB equates to a length of approximately 6 5 feet of cable with a connector on each end RG 142B or RG 40...

Page 58: ...na the glideslope may be a separate antenna in some aircraft that receives VOR frequencies between 108 and 117 95 MHz and localizer frequencies between 108 and 112 MHz and glideslope information between 328 6 and 335 4 MHz Follow the antenna manufacturer s installation instructions for mounting antennas It is recommended that the installer use RG 142B RG 400 or equivalent 50Ω coax for the NAV ante...

Page 59: ...ax GPS 400W Main power P4001 760mA 1 4A 410mA 700mA GNC 420W Main power P4001 1 12A 2 5A 560mA 1 2A COM power P4002 RX 4mA 15mA 8mA 15mA TX 3 25A 6 0A 1 6A 3 0A GNC 420AW Main power P4001 1 12A 2 5A 560mA 1 2A COM power P4002 RX N A N A 3mA 15mA TX N A N A 1 6A 3 0A GNS 430W Main power P4001 1 60A 2 5A 800mA 1 2A COM power P4002 RX 4mA 15mA 8mA 15mA TX 3 25A 6 0A 1 60A 3 0A GNS 430AW Main power P4...

Page 60: ...III IV X X a 3 21 X ii a 4 31 41 X X ii a 3 2000 X X ii a 3 Century Triden X X ii a 3 System 20 30 40 50 X i a 4 System 55 X X i a 3 System 55X X X X a 2 ARINC 429 roll steering System 60 1 X i a 4 System 60 2 65 X X i a 3 S TEC System 60 PSS X a 3 Cessna 300B 400B 800B X X a 3 Bendix M4C M4D X X a 3 Collins APS 65 X X a 3 i Roll steering may be provided through the ST 901 GPSS converter ii Roll s...

Page 61: ...ver the AFMS provided with the AML STC should still be used with the appropriate limitations specified as described below AFMS Section 2 8 Autopilot Coupling Limitations This section of the AFMS contains two possible limitations a No limitations for autopilot coupling b Lateral GPS coupling LNAV only For 430W 530W units The GS of an ILS VLOC may be coupled to the autopilot without any limitations ...

Page 62: ...itation 2 is checked for any installation that meets all of the following criteria The GPS SELECT discrete output is configured for Auto on the Main System Config Page refer to section 5 3 3 in the appropriate installation manual ARINC 429 GPSS provided directly to the autopilot computer or through a roll steering converter The 400W 500W interface to the autopilot provides vertical deviation infor...

Page 63: ...TEGRITY ANNUNCIATE Out 10 ANNUNCIATE D Out 11 ANNUNCIATE E Out 12 ALTITUDE ALARM ANNUNCIATE Out 13 GPS SELECT Out 14 ILS GPS APPROACH Out 15 AIRCRAFT POWER 2 In 16 TIME MARK OUT Out 17 MAIN LATERAL SUPERFLAG Out 18 MAIN VERTICAL SUPERFLAG Out 19 AIRCRAFT POWER 1 In 20 AIRCRAFT POWER 1 In 21 MAIN LEFT Out 22 MAIN RIGHT Out 23 MAIN LATERAL FLAG Out 24 MAIN LATERAL FLAG GROUND Out 25 MAIN TO Out 26 M...

Page 64: ...4 GPS RS 232 OUT 4 Out 55 GPS RS 232 IN 4 In 56 GPS RS 232 OUT 1 Out 57 GPS RS 232 IN 1 In 58 GPS RS 232 OUT 2 Out 59 GPS RS 232 IN 2 In 60 ALTITUDE COMMON GROUND Out 61 ALTITUDE C4 In 62 ALTITUDE C2 In 63 ALTITUDE C1 In 64 ALTITUDE B4 In 65 ALTITUDE B2 In 66 ALTITUDE B1 In 67 ALTITUDE A4 In 68 ALTITUDE A2 In 69 ALTITUDE A1 In 70 ALTITUDE D4 In 71 OBS MODE SELECT In 72 AIRCRAFT POWER 2 In 73 CDI S...

Page 65: ...C HI In 6 COM MIC AUDIO HI In 7 500Ω COM AUDIO HI Out 8 RESERVED 9 RESERVED 10 RESERVED 11 AIRCRAFT POWER In 12 AIRCRAFT POWER In 13 RESERVED 14 TRANSMIT INTERLOCK In 15 COM REMOTE TRANSFER In 16 SPARE 17 INTERCOM MIC LO In 18 COM MIC AUDIO LO In 19 500Ω COM AUDIO LO Out 20 RESERVED 21 AIRCRAFT GROUND 22 AIRCRAFT GROUND 23 RESERVED 24 RESERVED 25 RESERVED 13 12 11 10 9 8 7 6 5 4 3 2 1 25 24 23 22 ...

Page 66: ... 14 PARALLEL DME 8MHZ Out 15 VOR LOC SUPERFLAG Out 16 500Ω VOR ILS AUDIO HI Out 17 500Ω VOR ILS AUDIO LO Out 18 SERIAL DME CLOCK Out 19 SERIAL DME DATA Out 20 SER DME CHAN REQ PAR DME 4MHZ I O 21 SER DME RNAV MODE PAR DME 2MHZ I O 22 DME COMMON In 23 VOR ILS ARINC 429 OUT B Out 24 VOR ILS ARINC 429 OUT A Out 25 VOR OBI CLOCK Out 26 VOR OBI SYNC Out 27 VOR OBI DATA Out 28 VLOC REMOTE TRANSFER In 29...

Page 67: ...age converter should include a single short circuit protection device on its output such as a circuit breaker The output should be connected to the COM power input P4002 11 and P4002 12 for the COM transmitter The other power input pins P4001 19 20 15 72 and P4006 44 accept 11 to 33 VDC Refer to Figure H 5 A power connection on P4006 44 is only required if NAV SUPERFLAG and or G S SUPERFLAG is uti...

Page 68: ...tance to ground is 375 Ω These inputs are considered inactive if the voltage to ground is 11 33 VDC NOTE Some transponders and other altitude encoder receivers do not have internal isolation diodes to prevent the unit from pulling the encoder lines to ground when the unit is off These units require a diode added to the installation harness for each encoder line The anode should be connected on the...

Page 69: ...n Indicator Electrical Characteristics 4 4 2 1 Deviation Pin Name Connector Pin I O MAIN LEFT P4001 21 Out MAIN RIGHT 1 65V COMMON P4001 22 Out MAIN UP 1 65V COMMON P4001 27 Out MAIN DOWN P4001 28 Out The deviation output is capable of driving up to three 1000 Ω meter loads with 150 mVDC 10 for full scale deflection The drive circuit provides for more than full scale deflection with a maximum cour...

Page 70: ...R E 2 5V COMMON OBS P4001 34 Out MAIN OBS STATOR F P4001 35 In MAIN OBS STATOR G 2 5V COMMON OBS P4001 36 Out MAIN OBS ROTOR C and H are a buffered output that is intended to drive the OBS rotors MAIN OBS STATOR D and MAIN OBS STATOR F are each phase and amplitude shifted version of the MAIN ROTOR C output Each pair is intended to read one of the two windings of the indicator s OBS stator 4 4 3 Ma...

Page 71: ...the arrival waypoint the waypoint annunciator flashes 4 5 1 3 CDI SOURCE SELECT GNS 430W Only This discrete input may be used to toggle between display of GPS and VOR LOC Glideslope information on the MAIN external CDI HSI A momentary low on this pin performs the same function as pressing the CDI key on the GNS 430W bezel 4 5 1 4 VLOC ANNUNCIATE GNS 430W Only This annunciator output is driven when...

Page 72: ... to select Demo Mode on the 400W Series unit A low on this pin at time of unit power up invokes the Demo Mode Demo Mode allows the 400W Series unit to simulate reception of GPS satellite signals CAUTION Do not connect DEMO MODE SELECT in an aircraft installation 4 5 1 13 GPS SELECT The GPS Select Output is driven low when GPS data is being displayed on the CDI HSI and the ILS GPS Approach Output i...

Page 73: ...LECT P4001 73 In COM REMOTE RECALL 1 P4001 74 In DEMO MODE SELECT P4001 75 In 1 Main software version 3 00 or later These inputs are considered active if either the voltage to ground is 1 9 V or the resistance to ground is 375 Ω These inputs are considered inactive if the voltage to ground is 11 33 VDC 4 5 2 3 TIME MARK OUT Pin Name Connector Pin I O TIME MARK OUT P4001 16 Out TIME MARK OUT output...

Page 74: ...magnetic variation NOTE Aviation RS 232 data may be transmitted with or without the current GPS altitude in feet Refer to Section 5 3 2 The 400W Series unit can receive pressure altitude air data and fuel data from certain systems on the GPS RS 232 IN 1 port The 400W Series unit can communicate with a Ryan TCAD 9900B system using the GPS RS 232 OUT 2 and GPS RS 232 IN 2 lines to display traffic in...

Page 75: ...Data Record Header 075G Active Wpt From To Data 100 Selected Course 1 100P Selected Course 1 113G Message Checksum 114 Desired Track True 115 Waypoint Bearing True 116 Cross Track Distance 116G 2 Cross Track Distance 117G 1 Vertical Deviation 117P 1 Vertical Deviation 121 Horizontal Command to Autopilot 125 Greenwich Mean Time BCD 147G Magnetic Variation 251 Distance to Go 251G Distance to Go 252 ...

Page 76: ...figuration setting that can be used to enable the transmission of these labels for the indicated ARINC 429 output types Refer to Section 5 3 1 for additional details 2 Label 116G and 326G utilize the optional resolution extension bits bits 11 13 The following labels are output on the VOR ILS ARINC 429 OUT port Label Parameter Name 034G VOR ILS Frequency BCD 035G DME Frequency BCD 100G Selected Cou...

Page 77: ...A P4001 46 Out GPS ARINC 429 OUT B P4001 47 Out GPS ARINC 429 IN 1 A P4001 48 In GPS ARINC 429 IN 1 B P4001 49 In GPS ARINC 429 IN 2 A P4001 50 In GPS ARINC 429 IN 2 B P4001 51 In VOR ILS ARINC 429 OUT A P4006 24 Out VOR ILS ARINC 429 OUT B P4006 23 Out VOR ILS ARINC 429 IN A P4006 36 In VOR ILS ARINC 429 IN B P4006 35 In The GPS and VOR ILS ARINC 429 outputs conform to ARINC 429 electrical specif...

Page 78: ...FER switch When TRANSMIT INTERLOCK is active the GNC 420W or GNS 430W COM receiver sensitivity is decreased This input is intended to reduce interference from other transmitters in the aircraft The TRANSMIT INTERLOCK input should be connected to the PTT input of other transmitters in the aircraft If connected to multiple PTT inputs these connections must include diode isolation or multiple radios ...

Page 79: ... audio and INTERCOM MIC audio 4 7 2 4 DISCRETE INPUTS Pin Name Connector Pin I O TRANSMIT INTERLOCK P4002 14 In COM REMOTE TRANSFER P4002 15 In VLOC REMOTE TRANSFER P4006 28 In These inputs are considered active if either the voltage to ground is 1 9 V or the resistance to ground is 375 Ω These inputs are considered inactive if the voltage to ground is 11 33 VDC COM REMOTE TRANSFER and VLOC REMOTE...

Page 80: ...LOC frequency is channeled to a localizer channel 4 8 2 VOR ILS Indicator Electrical Characteristics 4 8 2 1 Superflags Pin Name Connector Pin I O VOR LOC SUPERFLAG P4006 15 Out GLIDESLOPE SUPERFLAG P4006 38 Out The output supplies not less than 500 mA on a 28 volt system and 250 mA on a 14 volt system with the output voltage not less than AIRCRAFT POWER 3 VDC when the flag is to be OUT OF VIEW Th...

Page 81: ... rotors VOR OBS STATOR D and VOR OBS STATOR F are each phase and amplitude shifted version of the VOR ROTOR C output Each pair is intended to read one of the two windings of the indicator s OBS stator 4 8 2 6 VOR LOC COMPOSITE Pin Name Connector Pin I O VOR LOC COMPOSITE OUT P4006 8 Out With a Standard VOR Test Signal applied VOR LOC COMPOSITE OUT is 0 5 0 1 VRMS into a 10 kΩ load With a Standard ...

Page 82: ...a stream set to indicate that a localizer frequency is tuned which stows the needle or drives it to the 3 o clock position 4 9 2 RMI OBI Electrical Characteristics Pin Name Connector Pin I O MAIN OBI CLOCK P4001 43 Out MAIN OBI SYNC P4001 45 Out MAIN OBI DATA P4001 44 Out Pin Name Connector Pin I O VOR OBI CLOCK P4006 25 Out VOR OBI SYNC P4006 26 Out VOR OBI DATA P4006 27 Out The output driver is ...

Page 83: ... leakage current with respect to ground is less than 10 μA NAV DME COMMON must be pulled low to indicate to the NAV module that it is the device channeling the DME NAV DME COMMON is considered active if either the voltage to ground is 1 9 V or the resistance to ground is 375 Ω These inputs are considered inactive if the voltage to ground is 11 33 VDC 4 10 2 2 King Serial DME Tuning Pin Name Connec...

Page 84: ... configuration 4 10 4 DME Tuning Calibration and Checkout None 4 10 5 DME Tuning Interconnect References Refer to Appendix H for interconnect information NOTE For the GNS 430W to tune a Narco DME 890 or IDME 891 or an ARC Cessna RTA 476A using parallel 2 of 5 unique wiring and configuration are required Refer to 5 3 14 and Figure H 24 ...

Page 85: ...stallation If fewer than three turns are possible the mounting rack should be moved aft toward the pilot such that the aircraft panel does not obstruct the unit from engaging in the rack 5 3 Configuration Mode Operations With power applied to the aviation rack and the 400W Series unit turned off press and hold the ENT key and turn the unit on Release the ENT key when the display activates After th...

Page 86: ...each be configured independently for the desired function s SPEED Selection Description Low Standard low speed ARINC 429 nominally 12 5 kilobits per second High High speed ARINC 429 nominally 100 kilobits per second NOTE Interfacing systems listed in the following tables are provided for reference only Refer to Appendix G to determine if the interface to a particular system is approved under the 4...

Page 87: ...ystems Bendix King KFC 400 Garmin GAD 42 Selected course heading and true airspeed data from the Garmin GAD 42 Garmin GDU 1 Selected course heading altitude temperature and speed information from the following systems Garmin G600 Garmin GTX 330 Garmin and Garmin w TIS This is a Garmin data concentration format Only high speed ARINC 429 should be used Garmin GTX 330 Honeywell EFIS Selected course h...

Page 88: ... The output data includes navigation and flight plan information including graphical representation of flight plan procedures to the following EFIS systems Honeywell Primus 1000 GAMA 429 Graphics w Int ARINC 429 data as defined by the GAMA General Aviation Subset 2nd Edition including GAMA Graphics Protocol A The output data includes navigation and flight plan information including graphical repre...

Page 89: ... stream ARINC 429 vertical guidance labels are used by the following systems Sandel SN3500 Other systems may also use these labels 5 3 2 MAIN RS 232 CONFIG Page Select the MAIN RS 232 CONFIG Page see Figure 5 2 Change the selectable RS 232 inputs and or outputs to match that of the equipment installed in the aircraft NOTE Interfacing systems listed in the following tables are provided for referenc...

Page 90: ...X 327 Transponder Trans Cal Industries IA RS232 X SSD120 ACK Technologies A 30 Mod 8 and above Ryan TCAD Traffic information from a Ryan TCAD 9900B or 9900BX Series system Shadin adc Serial air data information from the following units Shadin ADC 200 200 2000 Shadin alt Serial altitude data from the following units Shadin 8800T 9000T 9200T Shadin fadc Serial air data and fuel flow information from...

Page 91: ... Garmin MX20 V5 5 or earlier Horizon DDMP INSIGHT TAS 1000 Air Data Computer Crossfill Serial transfer of flight plans and user waypoints between two 400W 500W Series units GDL 69 Serial communication to a Garmin GDL 69 69A HW EGPWS 3 Serial communication to a Bendix King Honeywell KGP 560 EGPWS MapMX 2 3 Serial position altitude velocity and navigation data to the following units Garmin MX20 V5 7...

Page 92: ... A The aircraft is using Jet A or Jet A 1 fuel 6 7 lbs gal Jet B The aircraft is using Jet B JP 4 fuel 6 5 lbs gal Terrain Select Terrain in the CONFIGURE field to select the TERRAIN TYPE NONE or TERRAIN To test the Terrain Data Card highlight the TEST CARD field and press the ENT key Verify that the TEST CARD field indicates PASS A FAIL condition indicates that the Terrain Data Card is unusable S...

Page 93: ...d message is displayed telling the pilot to enable the A P APR Outputs This setting will not allow the pilot to select automatic GPS to ILS CDI transitions on the AUX CDI ALARMS page only manual transitions are permitted For Honeywell Bendix King KFC 225 and KAP 140 autopilots NOTE The GPS SELECT setting affects autopilot mode transitions and must be reflected in the AFMS Refer to Section 5 8 for ...

Page 94: ...nd Speed HDG Heading True or Magnetic WDIR Wind Direction B ALT Barometric corrected Altitude D ALT Density Altitude P ALT Pressure Altitude 5 3 5 MAIN INPUTS 2 Page Select the MAIN INPUTS 2 Page Figure 5 7 This page is also used for verifying electrical interfaces during installation and troubleshooting Information that is not being received by the 400W Series unit is dashed out Field Description...

Page 95: ...of 0 zero to 9999 SOURCE Selection Description PHOTO Backlight level is determined by the ambient light level as measured by the photocell on the 400W Series unit 14V DC Backlight level tracks a 14 volt DC aircraft lighting bus 28V DC Backlight level tracks a 28 volt DC aircraft lighting bus 5V DC Backlight level tracks a 5 volt DC aircraft lighting bus 5V AC Backlight level tracks a 5 volt AC air...

Page 96: ... using additional parameters PHOTO TRANS and PHOTO SLP OFFST described below PHOTO TRANS Photocell Transition Percentage When a lighting bus is used to control the lighting of the display see Figure 5 10 this parameter sets the point on the lighting bus control below which the display brightness tracks the 400W Series unit s photocell This field has a range of 0 zero to 99 and is set to 25 at the ...

Page 97: ...tallation DISCRETE TOGGLE Selection Verify That APR The APR annunciator is active and inactive as selected on this page GPS The GPS source select annunciator is active and inactive as selected on this page INTEG The INTEG annunciator is active and inactive as selected on this page MSG The MSG annunciator is active and inactive as selected on this page OBS The OBS annunciator is active and inactive...

Page 98: ...ag is hidden TO The TO flag is in view SELECTED COURSE Select 150 on the CDI HSI that is connected to the 400W Series unit s MAIN OBS inputs The SELECTED COURSE field indicates near to 150 and a Calibrate to 150 field appears Selecting this field calibrates the 400W Series unit to match the input source Verify OBS operation by checking that the course displayed on the 400W Series unit is within 2 ...

Page 99: ... it is desired to switch a Bendix King KI 229 or KNI 582 RMI pointer independently from the GNS 430W CDI button Track CDI The MAIN King Serial OBI outputs are GPS or VOR and switchable by the GNS 430W CDI button This is useful if it is desired the Bendix King KI 229 or KNI 582 RMI pointer to display the same navigation source as the GNS 430W CDI outputs V FLAG STATE Main software version 3 20 or l...

Page 100: ...etting is reversed The higher the SQ 250 number the more signal is required to break squelch SQ 833 Sets the squelch threshold for 8 33 kHz channel spacing operation May be set to any value between 0 zero and 63 The higher the number the more signal is required to break squelch SIDE Sets the sidetone audio output level May be set to any value between 0 zero and 63 NOTE The sidetone audio output le...

Page 101: ...sing the controls on the GNS 430W front panel make the selections below and verify the interfaces as appropriate NOTE The LAT VERT and SELECTED COURSE configurations only apply to installations where a CDI HSI is connected to the VOR LOC GLIDESLOPE pins on connector P4006 CDI LAT VERT Selection Verify That Max left The CDI is pegged to the left up Full left The CDI is deflected full scale to the l...

Page 102: ...ries to match the input source Verify OBS operation by checking that the course displayed on the 400W Series is within 2 of the selected course Do this at 30 intervals around the OBS card DME CHNL MODE This configuration allows you to set the format for DME tuning data output Selection Description King serial King Serial DME tuning data Parallel 2x5 2 of 5 parallel DME tuning Parallel BCD Shifted ...

Page 103: ...s 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 TX Generates all 429 outputs with SDI 2 DME MODE Selection Description Directed freq 1 If the GNS 430W is connected to a multi channel ARINC 429 DME channel...

Page 104: ...n is used to enter the height above ground of the GPS antenna Prior to proceeding measure the GPS antenna vertical offset to the nearest foot as shown in Figure 5 19 Figure 5 19 Measurement of GPS Vertical Offset Use the large and small knobs to enter the offset value and press ENT to save Figure 5 20 GPS Vertical Offset Page ...

Page 105: ...e STORMSCOPE TEST Page see Figure 5 22 This page shows current strike activity WX 500 status and the heading supplied by the WX 500 The WX 500 mode may be changed to Demo Noise monitor Self test Strike test or Weather Verify that the WX 500 mode can be changed Refer to the WX 500 manual for specific installation test procedures for the WX 500 using this page to view strike data change the WX 500 m...

Page 106: ...andby mode verify that the SkyWatch may be placed in self test mode by highlighting Test Mode and pressing ENTER on the 400W Series unit Refer to the L3 Communications SkyWatch installation manual for system checkout For Ryan TCAD see Figure 5 25 this page shows the current shield mode and altitude Verify that the TCAD shield mode may be changed Ground GND Terminal TML Standard STD En Route ENR or...

Page 107: ...see Figure 5 27 This page allows remote configuration of a GAD 42 Interface Adapter Unit For details of this function please refer to Section 5 of the GAD 42 Installation Manual P N 190 00159 00 5 3 23 GDL CONFIG Page This page allows the user to set the attenuation and model of the GDL 69 It is only available if one of the RS 232 ports is configured for the GDL 69 69A The GDL 69A XM must be activ...

Page 108: ...r test word returned from the GDL 69 is displayed on the DATA LINK DIAGNOSTICS page for each of the following parameters Display Description QOS Quality of Service Test TERR Terrestrial Error Status SAT1 Satellite 1 Error Status SAT2 Satellite 2 Error Status TUNER Tuner Status Figure 5 29 Data Link Diagnostics ...

Page 109: ...lowing steps 1 Go to the VOR LOC GS CDI configuration page 2 Verify correct operation of the lateral deviation flag and TO FROM flag using the corresponding selections 3 Verify correct operation of the vertical deviation and flag using the corresponding selections 5 4 3 Discrete Inputs and Annunciator Outputs Checkout If the GNS 400W Series unit is connected to external annunciators systems or ext...

Page 110: ...h the active altitude source NOTE After applying power to an altitude source it may take several minutes to warm up During the warm up period the altitude display on the GNS 400W Series unit will be dashed out 4 If there are multiple altitude sources remove power from the currently active source and apply power to another source that has not been checked 5 Repeat steps 3 and 4 until all available ...

Page 111: ...ions to a different number 4 Verify that after pressing ENT the STATUS field will change to SENDING then change back to ACTIVE If the entry reverts to the previous number when ACTIVE is displayed then refer to the GAD 42 Installation Manual P N 190 00159 00 5 4 8 Lighting Bus Interface Check The display and key backlighting on the 400W Series unit can track an external lighting dimmer bus input an...

Page 112: ...displayed Parameter Self Test Value Course Deviation Half scale left deviation TO indication flag pulled Glideslope Vert Deviation Half scale up deviation flag pulled Annunciators All On Bearing to Waypoint RMI 135 Selected Course OBS 400W Series unit displays the OBS value 149 5 if interfaced to an HSI with driven course pointer Desired Track 149 5 Displayed as 150 Items below are not displayed o...

Page 113: ...ll IFR installations NOTE It is known that certain non aviation radios including marine transceivers can interfere with civil aviation navigation and surveillance equipment including the Garmin GNS 400W Series When installing GNS 400W Series equipment in accordance with the appropriate STC it is the responsibility of the installer to ensure that the GNS 400W Series unit modification is compatible ...

Page 114: ...75 MHz 121 225 MHz 131 300 MHz 121 250 MHz 131 325 MHz 131 200 MHz 131 350 MHz NOTE For VHF radios with 8 33 kHz channel spacing include the following frequencies in addition to those listed above 8 33 kHz COM Channel Spacing 121 185 MHz 130 285 MHz 121 190 MHz 131 290 MHz 7 Repeat steps 3 through 6 for all remaining COM transceivers installed in the aircraft 8 If aircraft is TCAS equipped turn on...

Page 115: ...ies unit must be verified 5 5 6 1 Honeywell Bendix King EFS40 50 Interface Check If a Honeywell EFS40 50 has been connected to GNS 400W Series unit the interface should be verified as described in this section 1 Cycle power to the first GNS 400W Series unit and acknowledge the prompts until it gets to the self test page see Section 5 5 1 2 Ensure that GPS1 data is displayed by pressing the 1 2 key...

Page 116: ...self test page verify that the SN3308 is displaying the following data from the GPS source Course Deviation Half scale left deviation TO indication flag pulled Vertical Deviation Half scale up deviation flag pulled Active Waypoint GARMN 4 On the GNS 400W Series unit verify that an OBS value is displayed and not dashed out 5 Acknowledge the self test on the GNS 400W series unit by pressing the ENT ...

Page 117: ...t the SN3308 is displaying the following data from GPS1 Course Deviation Half scale left deviation TO indication flag pulled Vertical Deviation Half scale up deviation flag pulled Active Waypoint GARMN 6 On the first GNS 400W Series unit verify that an OBS value is displayed and not dashed out 7 Acknowledge the self test on the first GNS 400W Series unit by pressing the ENT key 8 Select VLOC on th...

Page 118: ...out 5 Acknowledge the self test on the GNS 400W Series unit by pressing the ENT key 6 Select VLOC on the GNS 400W Series unit and verify that the SN3308 displays NAV 1 or NAV 2 depending on what navigation source the GNS 430W is 7 Ensure that the NAV1 or NAV2 indication does not have a red line through it 5 5 6 4 EHSI Deviation Scaling If HSI CDI Is Driven by the 400W Series Unit Via Serial Data I...

Page 119: ...mscope has been connected to the GNS 400W Series unit the Stormscope interface should be verified as described in this section 1 Go to the Lightning page on the GNS 400W Series unit in the NAV page group 2 Verify that LIGHTNING FAILED is not displayed in yellow on the center of the Lightning page 3 Using the Self Test selection under the Lightning Menu initiate a Stormscope self test 5 5 6 8 GMX 2...

Page 120: ...page group NOTE If the XM Satellite Radio audio subscription has not been activated audio is available only on Channel 1 If the audio subscription has been activated audio should be available on multiple channels 2 Ensure that the GDL 69A audio is not muted 3 Verify that audio can be heard over the headsets Adjustment of the volume may be required 5 5 6 10 Crossfill Check If Dual Units Installed W...

Page 121: ...OR OBI output from the GNS 430W is connected to an RMI navigation indicator verify the interface as follows 1 Apply power to the equipment 2 If installed set the RMI select switch to the VLOC position 3 Tune a local VOR station or use a simulated signal from an approved VOR Test System 4 Verify that the RMI needle swings and points towards the VOR station 5 5 6 12 DME Tuning Check GNS 430W Only If...

Page 122: ...display of flight plan data is consistent with the CDI indication deviation TO FROM in the pilot s primary field of view 5 6 2 VHF COM Flight Check GNC 420W and GNS 430W After the installation is complete a flight test is recommended to ensure satisfactory performance To check the communications transceiver maintain an appropriate altitude and contact a ground station facility at a range of at lea...

Page 123: ... Press the CDI key to select VLOC on the 430W Verify that the GPSS mode disengages 5 7 Database Check Check the aviation database to ensure it is current The database information is displayed during the unit display start up sequence To check the database 2 Turn off the 400W Series units and then turn it on The 400W Series unit will go through its normal start up sequence 3 Wait for the Aviation D...

Page 124: ...he AFMS corresponding to the type of GPS antenna that was installed 3 Fill in the appropriate checkbox in the Limitations section of the AFMS corresponding to the autopilot coupling limitations NOTE The GPS SELECT setting will determine if the transition into approach mode is automatic or requires pilot acknowledgement of a message prompt Refer to GPS SELECT in Section 4 5 1 13 for additional deta...

Page 125: ..._ Display Key In 2 High Low __________________ Source ___________ __________ Out High Low __________________ Resp Time Min ____ _____ ____ _____ Slope Offset ____ _____ ____ _____ SDI Common LNAV 1 LNAV 2 Photo Trans ___________ N A Photo Slp Ofst ____ _____ N A VNAV Disable Labels Enable Labels Main CDI OBS Config Main RS 232 Configuration RX TX OBI Source Always GPS Track CDI N A Chnl 1 ________...

Page 126: ...ach APR VDI down centered up N A GPS Indicator GPS TO FROM flag OFF TO FROM N A Integrity INTEG Valid flags N A Message MSG OBS Selected Course N A OBS Mode OBS N A Terminal Mode TERM VOR ILS INDICATOR N A N A VLOC Indicator VLOC CDI left centered right N A Waypoint WPT VDI down centered up N A ILS GPS Approach ILS GPS APR TO FROM flag OFF TO FROM N A GPS Select GPS SELECT Valid flags ALTITUDE ENC...

Page 127: ...T GNS 430W ONLY N A Garmin GDL 69 69A VOR reception checked N A Crossfill check Localizer reception checked N A External RMI Deviation needle and flag checked N A DME Tuning N A G600 System VHF COM CHECKOUT 420W and 430W MAGNETIC COMPASS CHECK Receiver Transmitter operation checked N A Compass swing performed Antenna checked VSWR __________ FLIGHT CHECKS GPS checked ILS checked 430W only COM check...

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Page 129: ... off then turn on each piece one at a time to isolate the source of the interference Route GPS cable and locate GPS antenna away from sources of interference Improper antenna installation or coax routing Check GPS antenna installation connections and cable routing The GPS antenna must be mounted on the top of the aircraft Antenna shaded from satellites Make sure the aircraft is clear of hangars bu...

Page 130: ...correct Check ARINC 429 output port speed setting for port that autopilot is connected to and verify that the speed is correct for autopilot Wiring connections are incorrect Check wiring Must be connected to main GPS 429 output Autopilot is not getting GPSS Roll Steering data from the 400W Series unit ARINC 429 Roll Steering used Certain autopilots require groundspeed for GPSS to be enabled Ensure...

Page 131: ...vice not compatible or improper connection Verify 400W Series unit RX is connected to remote device TX and 400W Series unit TX is connected to remote device Rx Multiple TX lines connected together Verify that there is only one TX source per RX port RS 232 device is not communicating with the 400W Series unit Wiring connections are incorrect Check wiring CDI scaling on EFS 40 50 is not correct On E...

Page 132: ...orrupted Contact Garmin technical support CDI key stuck The CDI key is stuck in the enabled or pressed state Try pressing the CDI key again to cycle its operation Contact Garmin technical support CDI key disabled Ignore CDI key has been selected on the MAIN CDI OBS CONFIG page Go to the MAIN CDI OBS CONFIG page and deselect Ignore CDI key Check unit cooling The 400W Series unit has detected excess...

Page 133: ...n information has been lost or corrupted Reconfigure the unit Data transfer cancelled crossfill is busy An attempt to transfer flight plan data during a unit to unit crossfill was cancelled The host unit is busy Wait until any previous crossfill operation is complete before reattempting the transfer Data transfer cancelled data invalid An attempt to transfer a single user waypoint during a unit to...

Page 134: ...d a failure in the GAD 42 interface adapter Any mechanical indicators connected to your unit are unusable Refer to section 5 2 3 of the GAD Installation Manual P N 190 00159 00 Check for proper configuration Check wiring GDL 69 is not responding No data is being received from the GDL 69 Contact Garmin technical support GPS antenna cable is shorted Verify that the center conductor is not shorted to...

Page 135: ... 232 Serializer Icarus Rosetta or Shadin or grey code inputs Refer to Table 6 1 RS 232 device is not communicating with the GPS 400W GNS430W No basemap data available The 400W series unit has detected a failure in the built in basemap land data memory Land data does not appear on the Map Page Other unit functions continue to work normally Contact Garmin technical support to reload the basemap data...

Page 136: ... changed since it was last turned on in normal mode Contact Garmin technical support Ensure that Terrain database is inserted in the right most card slot Reload the TERRAIN database TERRAIN has failed The unit has detected a failure in the terrain system Contact Garmin technical support Check for proper configuration Check for correct wiring Traffic device has failed The 400W Series unit cannot co...

Page 137: ... proper configuration Check the wiring WX 500 device has failed The WX 500 is reporting a system failure Refer to the WX 500 installation manual for additional troubleshooting information Check for proper configuration of WX 500 WX 500 heading has failed The WX 500 is reporting invalid heading data The failure may be within the WX 500 or other connected equipment 6 3 Contacting the Factory for Ass...

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Page 139: ...approved by the FAA authorization to conduct any GPS or WAAS operation under Instrument Flight Rules IFR requires that 1 Aircraft using the GPS or WAAS capability of the 400W Series navigation equipment under IFR must be equipped with an approved and operational alternate means of navigation appropriate to the flight with the exception of oceanic and remote operations 2 For flight planning purpose...

Page 140: ... 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 approval for installation in an aircraft The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements The 400W Series GPS WAAS receiver when installed with the appropriate antenna l...

Page 141: ...y AML STC SA01933LA however instructions and data provided in this manual may be used to perform the alteration and obtain other FAA approval The 400W Series unit TERRAIN functionality is not recommended for use in rotorcraft 7 4 Aircraft Radio Station License An aircraft radio station license is not required when operating in U S airspace but may be required when operating internationally ...

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Page 143: ...y replacement and removal must be performed by professional services The 400W Series unit includes an internal battery that will last 5 to 8 years The battery is used for internal time clock and GPS system information Regular planned replacement is not necessary The 400W Series unit will display a Low Battery and Unit Needs Service message when replacement is required Once the low battery message ...

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Page 145: ...vironmental Qualification Forms EQFs visit the Dealers Only page on http www garmin com The part numbers for each form are listed below Table A 1 Environmental Qualification Form Part Numbers Unit EQF Part Number GPS 400W 005 00221 08 GNC 420W 005 00221 47 GNC 420AW 005 00221 48 GNS 430W 005 00221 49 GNS 430AW 005 00221 50 ...

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Page 147: ...rs Only portion of the Garmin website at www garmin com B 3 Continued Airworthiness Instructions Refer to the 400W Series Instructions for Continued Airworthiness P N 190 00356 65 B 4 STC Approved Model List The 400W 500W Series STC SA01933LA Approved Model List AML includes airplanes that are type certificated only under CAR 3 or 14 CFR Part 23 The Garmin 400W Series unit equipment is approved fo...

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Page 149: ...400W Series Installation Manual Page C 1 190 00356 02 Rev G Appendix C RESERVED ...

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Page 151: ...cription ETX ASCII end of text character 03 hex D 3 Output Sentence Type 1 The Type 1 output sentences have the following general format id item designator single ASCII alphabetic character dddd item data 1 to 10 printable ASCII characters CR ASCII carriage return character 0D hex LF ASCII line feed character 0A hex Each Type 1 sentence is output by the 400W Series unit approximately once every se...

Page 152: ... knots E d d d d d Distance to waypoint in tenths of nautical miles G s n n n n Cross track error where s L left or R right of course nnnn error in hundredths of nautical miles I d d d d Desired track in tenths of degrees K c c c c c Destination waypoint identifier will be blank filled on right if less than 5 characters in identifier L d d d d Bearing to destination waypoint in tenths of degrees Q...

Page 153: ...I carriage return character 0D hex LF ASCII line feed character 0A hex Each waypoint in the route being navigated by the 400W Series unit has a Type 2 sentence output by the 400W Series unit approximately once every second If no route is being navigated by the 400W Series unit i e the active route is empty the following Type 2 sentence is output approximately once every second id item designator 3...

Page 154: ...sequence number of waypoint unsigned binary wpt 1 5 Destination waypoint identifier will be blank filled on right if less than 5 characters in identifier lat 1 2 3 s d d d d d d d x x m m m m m m x h h h h h h h s 0 north or 1 south ddddddd latitude degrees unsigned binary xx undefined mmmmmm latitude minutes unsigned binary x undefined hhhhhhh hundredths of latitude minutes unsigned binary lon 1 ...

Page 155: ...itude Encoders Altitude Serializers and Altitude Converters RMS sp 12345T 12ul CR Where RMS ASCII characters sp space 0x20 sign indicator 0x2b or 0x2d 12345 altitude in feet T ASCII character sign indicator 12 sensor temperature ul checksum of bytes 1 through 14 in hex ASCII i e FA CR carriage return 0x0d Note Checksum is calculated by adding each byte in the message 1 through 14 E 3 Icarus Altitu...

Page 156: ...0x03 Note Checksum is calculated by adding each byte in the message 2 through 51 such that carries are discarded to give a one byte result The ASCII coded decimal representation of that byte is given ranging from 0 0x30 0x30 0x30 to 255 0x32 0x35 0x35 E 5 ARNAV EI Fuel Flow Sentence The Garmin 400W Series units are capable of receiving the following 13 byte message from the ARNAV or Electronics In...

Page 157: ... represents rate of turn degrees per second ZK 901 CR LF ZK ASCII characters sign 901 represents vertical speed tens of ft minute ZL234 CR LF ZL ASCII characters 234 represents heading degrees from north ZM5678 CR LF ZM ASCII characters 5678 represents fuel flow right tenths gallons hour ZN90123 CR LF ZN ASCII characters 90123 represents fuel used right tenths gallons ZO4567 CR LF ZO ASCII charact...

Page 158: ...w right Twin only tenths gallons hour GN90123 CR LF GN ASCII characters 90123 represents fuel used right Twin only tenths gallons GO4567 CR LF GO ASCII characters 4567 represents fuel flow left or Single tenths gallons hour GP89012 CR LF GP ASCII characters 89012 represents fuel used left or Single tenths gallons GQ001 CR LF GQ ASCII characters 001 represents error log reason indicator 001 temp se...

Page 159: ...rror log reason indicator SR67890 CR LF SR ASCII characters 67890 represents fuel remaining tenths gallons SS123 CR LF SS ASCII character 123 represents ground speed knots ST456 CR LF ST ASCII character 456 represents track degrees SU789012 CR LF SU ASCII character 789012 represents distance to waypoint hundredths nautical miles SV E W 345 CR LF SV ASCII character E represents East W represents We...

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Page 161: ...List The following drawings are included in this section Figure F 1 400W Series Mounting Rack Dimensions Figure F 2 GNS 430W Mounting Rack Installation Figure F 3 GNC 420W Mounting Rack Installation Figure F 4 GPS 400W Mounting Rack Installation Figure F 5 400W Series Recommended Panel Cutout Dimensions ...

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Page 163: ...llation Manual Page F 3 190 00356 02 Rev G 3 05 77 5 B A DIMENSIONS MODEL C 4 9 124 4 8 122 3 05 77 5 GNS 430W GNC 420W 1 4 35 6 1 3 33 1 2 30 5 2 85 72 4 4 6 117 GPS 400W Figure F 1 400W Series Mounting Rack Dimensions ...

Page 164: ...Page F 4 400W Series Installation Manual Rev G 190 00356 02 Figure F 2 GNS 430W Mounting Rack Installation ...

Page 165: ...400W Series Installation Manual Page F 5 190 00356 02 Rev G Figure F 3 GNC 420W Mounting Rack Installation ...

Page 166: ...Page F 6 400W Series Installation Manual Rev G 190 00356 02 Figure F 4 GPS 400W Mounting Rack Installation ...

Page 167: ...400W Series Installation Manual Page F 7 190 00356 02 Rev G Figure F 5 400W Series Recommended Panel Cutout Dimensions ...

Page 168: ...Page F 8 400W Series Installation Manual Rev G 190 00356 02 This page intentionally left blank ...

Page 169: ...previously FAA approved The VHF COM audio and VHF NAV audio if applicable must be verified as described in sections 5 5 4 and 5 5 5 Manufacturer Model Data Format Notes Honeywell Bendix King KMA 24 KMA 24H 70 71 KMA 26 KMA 28 Garmin GMA 340 GMA 347 Garmin AT SL15 SL15M SL10S SL10MS SL10 SL10M PS Engineering PMA 6000 PMA 7000 Series PMA 8000 Series G 2 Air Data Computer Air Data Computers not liste...

Page 170: ...ously FAA approved The interface check for the altitude serializer encoder described in section 5 4 4 serial interface or 5 4 5 parallel gray code interface must be successfully completed Manufacturer Model Data Format Notes ARNAV FC 10 FT 10 Electronics International FP 5L Icarus Instruments 3000 JP Instruments EDM 700 Sandia SAE 5 35 Shadin 8800T 9000T 9200T F ADC 200 F ADC 2000 91204XT 38 D Min...

Page 171: ...nit was installed and approved for coupled VOR ILS LOC BC and GPS LNAV approaches this upgraded installation will also be approved for these operations however GPS and RNAV approaches with GPS WAAS based vertical guidance LNAV V L VNAV and LPV modes on the 400W series unit are not authorized when coupled to the autopilot NOTE Contact Garmin to remove VNAV limitations Mfr Model Data Format Notes KA...

Page 172: ...A 346 Parallel Gray Code Sandia SAE 35 Parallel Gray Code Terra AT 3000 Parallel Gray Code Trans Cal Industries IA RS 232 X SSD120 Parallel Gray Code Parallel Gray Code G 6 EFIS Displays Manufacturer Model Data Format Notes Garmin G600 GDU 620 ARINC 429 RS 232 400W 500W Series software version 3 10 or later is required Honeywell Bendix King EFS 40 50 SG 465 ARINC 429 400W 500W series software vers...

Page 173: ... B KPI 553 A B Century NSD 360A NSD 1000 Collins 331A 6P 331A 9G PN101 331A 3F 3G Garmin GI 102 A GI 106 A S TEC ST 180 Sperry RD 444 RD 550A RD 650 Mid Continent MD222 402 MD222 406 G 10 Weather Traffic and Terrain Manufacturer Model Data Format Notes Garmin GDL 69 GTX 330 RS 232 ARINC 429 High Speed Honeywell Bendix King KGP 560 KTA 870 KTA 810 KMH 880 KMH 820 KTA 970 KTA 910 1 KMH 980 KMH 920 1...

Page 174: ...witch 992561 1241762200 Indicator 14VDC Indicator Staco Switch 992561 1241862200 Indicator 28VDC Indicator Vivisun 95 40 17 B6 AW724 Indicator 28VDC Indicator can be converted to 14VDC operation by replacing qty 4 28VDC lamps with 14VDC lamps P N 14 113 Vivisun 95 45 11 B6 AW724 Indicator Switch 28VDC Indicator with momentary switch can be converted to 14VDC operation by replacing qty 4 28VDC lamp...

Page 175: ...altitude even though it is part of Aviation format MapMX format for MX20 version 5 6 or later 1 Garmin GMX 200 RS 232 Aviation format MapMX format preferred 1 EX500 P N 700 00007 ARINC 429 MFD software P N 530 00193 or later is required Avidyne EX5000 P N 700 00004 or P N 700 00030 ARINC 429 MFD software P N 530 00195 or later is required 1 Main software version 3 10 or later G 14 Interface Adapte...

Page 176: ...Page G 8 400W Series Installation Manual Rev G 190 00356 02 This page intentionally left blank ...

Page 177: ...3308 Figure H 14 ARINC 429 Sandel EHSI Interconnect Two GNS 430W Two Sandel SN3308 Figure H 15 ARINC 429 RS 232 Air Data IRU AHRS Interconnect Figure H 16 Traffic Advisory System Interconnect Figure H 17 GTX 330 Interconnect Figure H 18 Weather and Terrain Interconnect Figure H 19 Audio Panel Interconnect Figure H 20 VOR ILS Indicator Interconnect Figure H 21 RMI OBI Interconnect Figure H 22 King ...

Page 178: ...Page H 2 400W Series Installation Manual Rev G 190 00356 02 This page intentionally left blank ...

Page 179: ...400W Series Installation Manual Page H 3 190 00356 02 Rev G Figure H 1 400W Series System Interface Diagram ...

Page 180: ...Page H 4 400W Series Installation Manual Rev G 190 00356 02 Figure H 2 GNS 430W Typical Installation Sheet 1 of 2 ...

Page 181: ...400W Series Installation Manual Page H 5 190 00356 02 Rev G Figure H 2 GNS 430W Typical Installation Sheet 2 of 2 ...

Page 182: ...Page H 6 400W Series Installation Manual Rev G 190 00356 02 Figure H 3 GNC 420W Typical Installation Sheet 1 of 2 ...

Page 183: ...400W Series Installation Manual Page H 7 190 00356 02 Rev G Figure H 3 GNC 420W Typical Installation Sheet 2 of 2 ...

Page 184: ...Page H 8 400W Series Installation Manual Rev G 190 00356 02 Figure H 4 GPS 400W Typical Installation Sheet 1 of 2 ...

Page 185: ...400W Series Installation Manual Page H 9 190 00356 02 Rev G Figure H 4 GPS 400W Typical Installation Sheet 2 of 2 ...

Page 186: ...Page H 10 400W Series Installation Manual Rev G 190 00356 02 Figure H 5 Power Lighting and Antenna Interconnect Sheet 1 of 3 ...

Page 187: ...400W Series Installation Manual Page H 11 190 00356 02 Rev G Figure H 5 Power Lighting and Antenna Interconnect Sheet 2 of 3 ...

Page 188: ...Page H 12 400W Series Installation Manual Rev G 190 00356 02 Figure H 5 Power Lighting and Antenna Interconnect Sheet 3 of 3 ...

Page 189: ...400W Series Installation Manual Page H 13 190 00356 02 Rev G Figure H 6 Gray Code Altimeter Interconnect ...

Page 190: ...Page H 14 400W Series Installation Manual Rev G 190 00356 02 Figure H 7 Main Indicator Interconnect ...

Page 191: ...400W Series Installation Manual Page H 15 190 00356 02 Rev G Figure H 8 KI 209A Main Indicator Interconnect ...

Page 192: ...Page H 16 400W Series Installation Manual Rev G 190 00356 02 Figure H 9 KI 208A Main Indicator Interconnect ...

Page 193: ...400W Series Installation Manual Page H 17 190 00356 02 Rev G Figure H 10 RS 232 Serial Data Interconnect Sheet 1 of 2 ...

Page 194: ...Page H 18 400W Series Installation Manual Rev G 190 00356 02 Figure H 10 RS 232 Serial Data Interconnect Sheet 2 of 2 ...

Page 195: ...400W Series Installation Manual Page H 19 190 00356 02 Rev G Figure H 11 ARINC 429 EFIS Interconnect Sheet 1 of 2 ...

Page 196: ...Page H 20 400W Series Installation Manual Rev G 190 00356 02 H 11 ARINC 429 EFIS Interconnect Sheet 2 of 2 ...

Page 197: ...400W Series Installation Manual Page H 21 190 00356 02 Rev G Figure H 12 ARINC 429 Sandel EHSI Interconnect One 400W Series Unit One Sandel SN3308 Sheet 1 of 2 ...

Page 198: ...Page H 22 400W Series Installation Manual Rev G 190 00356 02 Figure H 12 ARINC 429 Sandel EHSI Interconnect One 400W Series Unit One Sandel SN3308 Sheet 2 of 2 ...

Page 199: ...400W Series Installation Manual Page H 23 190 00356 02 Rev G Figure H 13 ARINC 429 Sandel EHSI Interconnect Two GNS 430W One Sandel SN3308 Sheet 1 of 2 ...

Page 200: ...Page H 24 400W Series Installation Manual Rev G 190 00356 02 Figure H 13 ARINC 429 Sandel EHSI Interconnect Two GNS 430W One Sandel SN3308 Sheet 2 of 2 ...

Page 201: ...W Series Installation Manual Page H 25 190 00356 02 Rev G Figure H 14 ARINC 429 Sandel EHSI Interconnect Two GNS 430W Two Sandel SN3308 THE TWO GNS 430W TWO SN3308s CONFIGURATION IS CURRENTLY NOT SUPPORTED ...

Page 202: ...Page H 26 400W Series Installation Manual Rev G 190 00356 02 Figure H 15 ARINC 429 RS 232 Air Data IRU AHRS Interconnect Sheet 1 of 2 ...

Page 203: ...400W Series Installation Manual Page H 27 190 00356 02 Rev G Figure H 15 ARINC 429 RS 232 Air Data IRU AHRS Interconnect Sheet 2 of 2 ...

Page 204: ...Page H 28 400W Series Installation Manual Rev G 190 00356 02 Figure H 16 Traffic Advisory System Interconnect Sheet 1 of 2 ...

Page 205: ...400W Series Installation Manual Page H 29 190 00356 02 Rev G Figure H 16 Traffic Advisory System Interconnect Sheet 2 of 2 ...

Page 206: ...Page H 30 400W Series Installation Manual Rev G 190 00356 02 Figure H 17 GTX 330 Interconnect ...

Page 207: ...400W Series Installation Manual Page H 31 190 00356 02 Rev G Figure H 18 Weather and Terrain Interconnect Sheet 1 of 2 ...

Page 208: ...Page H 32 400W Series Installation Manual Rev G 190 00356 02 Figure H 18 Weather and Terrain Interconnect Sheet 2 of 2 ...

Page 209: ...400W Series Installation Manual Page H 33 190 00356 02 Rev G Figure H 19 Audio Panel Interconnect Sheet 1 of 2 ...

Page 210: ...Page H 34 400W Series Installation Manual Rev G 190 00356 02 Figure H 19 Audio Panel Interconnect Sheet 2 of 2 ...

Page 211: ...400W Series Installation Manual Page H 35 190 00356 02 Rev G Figure H 20 VOR ILS Indicator Interconnect ...

Page 212: ...Page H 36 400W Series Installation Manual Rev G 190 00356 02 Figure H 21 RMI OBI Interconnect ...

Page 213: ...400W Series Installation Manual Page H 37 190 00356 02 Rev G Figure H 22 King Serial Panel DME Tuning Interconnect ...

Page 214: ...Page H 38 400W Series Installation Manual Rev G 190 00356 02 Figure H 23 King Serial Remote DME Tuning Interconnect ...

Page 215: ...400W Series Installation Manual Page H 39 190 00356 02 Rev G Figure H 24 Parallel 2 of 5 DME Tuning Interconnect ...

Page 216: ...Page H 40 400W Series Installation Manual Rev G 190 00356 02 Figure H 25 Bendix King Analog Autopilot Interconnect ...

Page 217: ...400W Series Installation Manual Page H 41 190 00356 02 Rev G Figure H 26 Century Autopilot Interconnect Sheet 1 of 2 ...

Page 218: ...Page H 42 400W Series Installation Manual Rev G 190 00356 02 Figure H 26 Century Autopilot Interconnect Sheet 2 of 2 ...

Page 219: ...400W Series Installation Manual Page H 43 190 00356 02 Rev G Figure H 27 S TEC Autopilot Interconnect Sheet 1 of 2 ...

Page 220: ...Page H 44 400W Series Installation Manual Rev G 190 00356 02 Figure H 27 S TEC Autopilot Interconnect Sheet 2 of 2 ...

Page 221: ...400W Series Installation Manual Page H 45 190 00356 02 Rev G Figure H 28 ARINC 429 Sandel EHSI Interconnect One 400W One Sandel SN3500 Sheet 1 of 2 ...

Page 222: ...Page H 46 400W Series Installation Manual Rev G 190 00356 02 Figure H 28 ARINC 429 Sandel EHSI Interconnect One 400W One Sandel SN3500 Sheet 2 of 2 ...

Page 223: ...NUNCIATE LAMP VOLTAGE FROM DIMMER CIRCUIT VIVISUN INDICATOR CONNECTION NAV GPS INDICATOR GPS G VLOC W C D B G A P1 P1 VLOC GPS WHITE GREEN 6 GARMIN 1 2 VLOC ANNUNCIATE GPS ANNUNCIATE LAMP VOLTAGE FROM DIMMER CIRCUIT VIVISUN INDICATOR SWITCH CONNECTION NAV GPS INDICATOR SWITCH GPS G VLOC W C D B G A P1 P1 VLOC GPS WHITE GREEN 7 3 1 4 4 4 EXTERNAL NAVIGATION SOURCE SELECTION ANNUNCIATORS P4001 P4001...

Page 224: ...THESE UNITS ALSO PROVIDE NAVIGATION SOURCE SELECTION ANNUNCIATION MID CONTINENT ANNUNCIATION CONTROL UNITS FOR BOTH 14V AND 28V SYSTEMS SHOWN THIS DIAGRAM IS PROVIDED TO SHOW INTERCONNECTION BETWEEN GNS 400W SERIES UNIT AND ACU ONLY REFER TO MID CONTINENT INSTALLATION MANUALS FOR ADDITIONAL INSTALLATION INFORMATION 9 CDI SOURCE SELECTION AND ANNUNCIATION IS DONE WITH EXTERNAL RELAYS REFER TO MID C...

Page 225: ...400W Series Installation Manual Page H 49 190 00356 02 Rev G Figure H 30 Parallel Slip Code DME Tuning Interconnect ...

Page 226: ...Page H 50 400W Series Installation Manual Rev G 190 00356 02 Figure H 31 Cessna Autopilot Interconnect ...

Page 227: ...400W Series Installation Manual Page H 51 190 00356 02 Rev G Figure H 32 Bendix Autopilot Interconnect ...

Page 228: ...Page H 52 400W Series Installation Manual Rev G 190 00356 02 Figure H 33 Switches Interconnect ...

Page 229: ...400W Series Installation Manual Page H 53 190 00356 02 Rev G Figure H 34 ARINC 429 Avidyne PFD MFD Interconnect Sheet 1 of 2 ...

Page 230: ...Page H 54 400W Series Installation Manual Rev G 190 00356 02 Figure H 34 ARINC 429 Avidyne PFD MFD Interconnect Sheet 2 of 2 ...

Page 231: ... GS DEV UP GS DEV DOWN VOR LOC DEV LT VOR LOC DEV RT APC 65A APC 65G J1 J3 GARMIN 400W 420W 430W P4001 27 28 21 22 MAIN UP MAIN DOWN MAIN LEFT MAIN RIGHT FGC 65 FYD 65 J1 J3 NOTES 14 ILS GPS APPROACH 35 LOC FREQ GND 4 17 MAIN LATERAL SUPERFLAG NAV HL FLAG 54 53 41 44 35 4 54 53 41 44 35 4 TO MAIN CDI 4 1 NAV LL FLAG NAV LL FLAG 23 24 MAIN LATERAL FLAG MAIN LATERAL FLAG 4 1 12 9 GS LL FLAG GS LL FL...

Page 232: ...Page H 56 400W Series Installation Manual Rev G 190 00356 02 Figure H 36 Garmin GAD 42 Interconnect ...

Page 233: ...400W Series Installation Manual Page H 57 190 00356 02 Rev G Figure H 37 Garmin G600 Interconnect ...

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