Garmin GNS 530AW Installation Manual Download Page 1

Page: 1 / 216

190-00357-02

October 2007

Rev. D

Garmin International, Inc.

500W SERIES

INSTALLATION MANUAL

GPS 500W and GNS

530W/530AW/TAWS

GNS is a trademark of Garmin Ltd. or its subsidiaries and may not be
used without the express permission of Garmin.

Summary of Contents for GNS 530AW

Page 1: ...er 2007 Rev D Garmin International Inc 500W SERIES INSTALLATION MANUAL GPS 500W and GNS TM 530W 530AW TAWS GNS is a trademark of Garmin Ltd or its subsidiaries and may not be used without the express permission of Garmin ...

Page 2: ...500W Series Installation Manual 190 00357 02 Rev D ...

Page 3: ...manual or any revision hereto is strictly prohibited Garmin International Inc 1200 E 151st Street Olathe KS 66062 USA Telephone 913 397 8200 Aviation Dealer Technical Support Line Toll Free 888 606 5482 Web Site Address www garmin com Garmin Europe Ltd Liberty House Bull Copse Road Hounsdown Business Park Southampton SO40 9RB UK Telephone 44 0 8708501241 RECORD OF REVISIONS Revision Revision Date ...

Page 4: ... Section 3 3 1 through 3 14 Section 4 4 1 through 4 24 Section 5 5 1 through 5 44 Section 6 6 1 through 6 4 Section 7 7 1 through 7 4 Section 8 8 1 through 8 2 Appendix A A 1 through A 2 Appendix B B 1 through B 2 Appendix C C 1 through C 2 Appendix D D 1 through D 4 Appendix E E 1 through E 6 Appendix F F 1 through F 6 Appendix G G 1 through G 6 Appendix H H 1 through H 54 ...

Page 5: ...subject to a penalty of up to 10 years imprisonment and a fine of up to 1 000 000 under 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 acco...

Page 6: ... and Wiring Considerations 2 11 2 7 Air Circulation and Cooling 2 11 2 8 Compass Safe Distance 2 11 3 INSTALLATION PROCEDURES 3 1 3 1 Unit and Accessories 3 1 3 2 Optional Accessories 3 2 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 7 Special Tools Required 3 5 3 8 Cable Installation 3 6 3 9 Eq...

Page 7: ...Procedure 6 1 6 2 Contacting the Factory for Assistance 6 4 7 LIMITATIONS 7 1 7 1 Operations 7 1 7 2 Installation 7 2 7 3 Rotorcraft Installation 7 3 7 4 Aircraft Radio Station License 7 3 8 PERIODIC MAINTENANCE 8 1 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 Informatio...

Page 8: ...PS Antenna Installation Considerations 2 5 Figure 2 2 Source Selection Annunciation Field of View 2 9 Figure 2 3 GPS Navigation TAWS Annunciation Field of View 2 10 Figure 3 1 Coaxial Cable Installation 3 6 Figure 5 1 MAIN ARINC 429 CONFIG Page 5 2 Figure 5 2 MAIN RS 232 CONFIG Page 5 5 Figure 5 3 MAIN SYSTEM CONFIG Page 5 6 Figure 5 4 MAIN SYSTEM CONFIG Page 5 7 Figure 5 5 MAIN SYSTEM CONFIG Page...

Page 9: ...nect H 17 Figure H 11 ARINC 429 Sandel EHSI Interconnect One 500W Series Unit One Sandel SN3308 H 19 Figure H 12 ARINC 429 Sandel EHSI Interconnect Two GNS 530W One Sandel SN3308 H 21 Figure H 13 ARINC 429 Sandel EHSI Interconnect Two GNS 530W Two Sandel SN3308 H 23 Figure H 14 ARINC 429 RS 232 Air Data IRU AHRS Interconnect H 24 Figure H 15 Traffic Advisory System Interconnect H 26 Figure H 16 GT...

Page 10: ...1 4 TSO Authorization 1 12 Table 3 1 Catalog Part Numbers 3 1 Table 3 2 Standard Kit Accessories 3 1 Table 3 3 Recommended Crimp Tools or Equivalent 3 5 Table 3 4 Pin Contact Part Numbers 3 7 Table 3 5 Unit Weights 3 10 Table 3 6 500W Series Unit Power Input 3 11 Table 5 1 GNS 500W Series Post Installation Checkout Log 5 41 Table 6 1 Troubleshooting Guide 6 1 Table A 1 Environmental Qualification ...

Page 11: ...n 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 password...

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Page 13: ...made to the GPS 500W or GNS 530W will apply equally to the TAWS version of these units Table 1 1 500W Series Units MODEL PART NUMBER COLOR NOTES GPS 500W 011 01062 00 BLACK 011 01062 10 GRAY 011 01062 40 BLACK NOTE 1 011 01062 50 GRAY NOTE 1 GPS 500W w TAWS 011 01063 00 BLACK 011 01063 10 GRAY 011 01063 40 BLACK NOTE 1 011 01063 50 GRAY NOTE 1 GNS 530W 011 01064 00 BLACK 011 01064 10 GRAY 011 0106...

Page 14: ...ndards Information Bulletin for Airworthiness FSAW 94 32 Guidance for Performing Field Approvals of Installation and Operational Use of Global Positioning Systems 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 application for installation and operational a...

Page 15: ...ion 47 CFR 22 925 prohibits airborne operation of ground based cellular 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 disrup...

Page 16: ...0 mA 28 VDC maximum 1 6 A 14 VDC maximum GNS 530W GNS530AW Main Connector 1 4 A 28 VDC maximum 3 0 A 14 VDC maximum GNS 530W COM Connector 15 mA 28 VDC receive 3 0 A 28 VDC transmit 15 mA 14 VDC receive 6 0 A 14 VDC transmit GNS 530AW COM Connector 15 mA 28 VDC receive 3 0 A 28 VDC transmit Superflag Power Requirements 500 mA maximum per superflag output Environmental Testing See Environmental Qua...

Page 17: ...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 18: ...nneling 6 dB BW is greater than 2 778 kHz for 8 33 kHz channeling 60 dB BW is less than 7 37 kHz for 8 33 kHz channeling Spurious Response Greater than 85 dB Transmitter Power At least 10 Watts 16 watts for AW models Transmitter Duty Cycle Recommended 10 maximum Modulation Capability The modulation is not less than 70 and not greater than 98 with a standard modulator signal applied to the transmit...

Page 19: ...m S N N is not 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 deviation te...

Page 20: ...equencies 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 is 78 mV 7 8 mV b With a standard deflection FLY UP condition 150 Hz dominant the output is 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 deflection of ...

Page 21: ... 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 22: ...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 23: ...se visit the FCC web site http wireless fcc gov aviation If an aircraft license is required make application 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 The GNS 530W owner accepts all responsibility for obtaining the proper licensing before using the transceiver CAUTION THE VHF TRANSMITTER IN THIS EQU...

Page 24: ...X main software uses Level D software for the COM tuning function All other COM functions are Level C In later versions of the main software the software level for the COM tuning function is Level C AC 20 67B Airborne VHF Communications Equipment Installations AC43 13 1B Acceptable Methods Techniques and Practices Aircraft Inspection and Repair AC43 13 2A Acceptable Methods Techniques and Practice...

Page 25: ...ental Conditions and Test Procedures for Airborne Equipment TSO C113 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 2 Garmin was granted a deviation from TSO C113 section 2 1 2 3 to use RTCA DO 160D instead of RTCA DO 160B as the standard for Environmen...

Page 26: ...h operational limitations to a level commensurate with test conditions used in the original TSO qualification tests d The ability to use 128 dBmic as the minimum GPS satellite signal in space for the purpose of assessing the operational limitation 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...

Page 27: ...riodic cycles and is available from Garmin TAWS 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 TAWS 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 fo...

Page 28: ... 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 29: ... closing the work area in case problems occur 2 2 Minimum System Configuration 2 2 1 VFR Installation The minimum 500W Series unit installation requires the following items for a VFR Installation GNS 500W 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 ins...

Page 30: ...ric altitude is not required by the 500W Series unit to meet the requirements of TSO C146a 2 3 1 Multiple Uncorrected Pressure Altitude Sources The 500W Series unit 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 G...

Page 31: ...a a NAV antenna and a Glideslope antenna Structural substantiation for mounting of antennas is beyond the scope of the 500W Series 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 ...

Page 32: ...e GPS antenna should be mounted no closer than 6 inches edge to edge from other antennas including passive antennas such as another GPS 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 ...

Page 33: ...500W Series Installation Manual Page 2 5 190 00357 02 Rev D Figure 2 1 GPS Antenna Installation Considerations ...

Page 34: ...ntenna including the GNS 530W COM antenna ELT antenna and DF receiver antenna is critical Use the following guidelines in addition to others in this document when locating the 500W Series unit and its antennas GPS Antenna Locate as far as possible from all COM antennas and all COM transceivers including the 500W Series unit COM ELT antennas and DF receiver antennas The GPS antenna is less suscepti...

Page 35: ...with a built in annunciation may also be used in lieu of a separate external annunciator to satisfy the source selection annunciation requirement In addition any required GPS navigation annunciations must be within 16 805 inches of the pilot view centerline If the 500W Series unit display is within this area then no external GPS navigation annunciations are required The 500W Series unit as a redun...

Page 36: ...he right of the primary instruments the internal display of annunciation within the 500W Series unit is considered to be within the acceptable field of view if the following criteria are met The left edge of the 500W Series unit is within 12 1 inches of the primary view centerline and the top edge of the 500W Series unit is no lower than the bottom edge of the primary flight instruments or the uni...

Page 37: ...f Section 2 5 1 1 2 Measure the horizontal distance from the primary view centerline to the left or right edge of the 500W Series as appropriate 3 If the 500W Series unit is mounted to the right of the primary instruments the internal display of annunciation within the 500W Series unit is considered to be within the acceptable field of view if the following criteria are met The left edge of the 50...

Page 38: ...S units only If the internal display of TAWS annunciations within the 500W Series unit does not meet the criteria defined in Section 2 5 1 2 an external TAWS annunciator unit must be installed within 16 805 inches of the view centerline refer to Figure 2 3 NOTE The entire annunciator must be within 16 805 inches of the view centerline The external TAWS annunciator unit must contain at a minimum th...

Page 39: ... 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 500W 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 40: ...Page 2 12 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank ...

Page 41: ...00 010 00417 01 011 01065 00 BLK 10W X X 14 28 010 00417 10 010 00417 11 011 01065 10 GRY 10W X X 14 28 010 00417 40 010 00417 41 011 01065 40 BLK 10W X X 14 28 X 010 00417 45 010 00417 46 011 01065 45 BLK 10W X X 28 X 010 00417 50 010 00417 51 011 01065 50 GRY 10W X X 14 28 X GNS 530AW 010 00418 00 010 00418 01 011 01066 00 BLK 16W X 28 010 00418 10 010 00418 11 011 01066 10 GRY 16W X 28 010 0041...

Page 42: ... 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 43: ...nits 011 00558 00 3 3 Database 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...

Page 44: ...or low loss splitter used with the VOR LOC antenna Headphones 500Ω nominal impedance Microphone Low impedance carbon or dynamic with transistorized pre amp For a list of optional accessories source selection annunciators refer to Appendix G 3 6 2 Materials Required But Not Supplied New Installations Only The 500W Series is intended for use with the standard aviation accessories The following items...

Page 45: ...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 46: ...g instructions on Figure 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 500W Series unit back plate Feed wires through the connector backshells before insertion into the 25 44 and 78 pin connectors Contacts for the 25...

Page 47: ...d in 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...

Page 48: ... unit 3 Install 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 rep...

Page 49: ...ditional 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 ...

Page 50: ...50Ω horizontally polarized NAV VOR Localizer Glideslope antenna 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 install...

Page 51: ... 3 6 500W Series Unit Power Input 14 VDC 28 VDC Input Connector Mode Typical Max Typical Max GPS 500W GPS 500W TAWS Main power P5001 950mA 1 60A 490mA 800mA GNS 530W GNS 530W TAWS Main power P5001 1 96A 3 0A 970mA 1 4A COM power P5002 RX 4mA 15mA 8mA 15mA TX 3 25A 6 0A 1 6A 3 0A GNS 530AW GNS 530AW TAWS Main power P5001 N A N A 970mA 1 4A COM power P5002 RX N A N A 3mA 15mA TX N A N A 1 6A 3 0A NO...

Page 52: ...INC 429 roll steering I II X a 4 III IV X X a 3 Century 21 X ii a 4 31 41 X X ii a 3 2000 X X ii a 3 Triden X X ii a 3 System 20 30 40 50 55 X i a 4 System 55X X X X a 2 ARINC 429 roll steering S TEC System 60 1 X i a 4 System 60 2 65 X X i a 3 System 60 PSS X a 3 Cessna 300B 400B 800B X X a 3 Bendix M4C X X a 3 i Roll steering may be provided through the ST 901 GPSS converter ii Roll steering may...

Page 53: ... However 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 limitat...

Page 54: ...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 55: ...NCIATE 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 MAIN FROM Out...

Page 56: ...S 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 SOURCE S...

Page 57: ... 3 SPARE INPUT 4 In 4 SPARE INPUT 3 In 5 SPARE INPUT 2 In 6 SPARE INPUT 1 In 7 RESERVED 8 RESERVED 9 TERRAIN NOT AVAILABLE ANNUNCIATE Out 10 TERRAIN WARNING ANNUNCIATE Out 11 TERRAIN CAUTION ANNUNCIATE Out 12 TAWS INHIBIT ANNUNCIATE Out 13 SPARE ANNUN 2 Out 14 SPARE ANNUN 1 Out 15 TAWS AUDIO ACTIVE OUT Out 16 RESERVED 17 21 GROUND 22 59 NO CONNECT 60 RS 232_OUT_5 Out 61 RS 232_IN_5 In 62 NO CONNEC...

Page 58: ...n 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 21 20 ...

Page 59: ... 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 60: ...e converter should include exactly one short circuit protection device on its output such as a circuit breaker P5002 11 and P5002 12 supply power to the COM transmitter The other power input pins P5001 19 P5001 20 P5001 15 P5001 72 and P5006 44 accept 11 33 VDC Refer to Figure H 4 A power connection on P5006 44 is only required if NAV SUPERFLAG or G S SUPERFLAG is utilized The power inputs P5001 1...

Page 61: ...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 62: ... 2 Main Indicator Electrical Characteristics 4 4 2 1 Deviation Pin Name Connector Pin I O MAIN LEFT P5001 21 Out MAIN RIGHT 1 65V COMMON P5001 22 Out MAIN UP 1 65V COMMON P5001 27 Out MAIN DOWN P5001 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 maximu...

Page 63: ...S STATOR E 2 5V COMMON OBS P5001 34 Out MAIN OBS STATOR F P5001 35 In MAIN OBS STATOR G 2 5V COMMON OBS P5001 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...

Page 64: ...point the waypoint annunciator flashes 4 5 1 3 CDI SOURCE SELECT GNS 530W Only The CDI Source Select 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 530W bezel 4 5 1 4 VLOC ANNUNCIATE GNS 530W Only The VLOC annunciate output is driven...

Page 65: ... be used to select Demo Mode on the 500W Series unit A low on this pin at time of unit power up invokes the Demo Mode Demo Mode allows the 500W 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 ...

Page 66: ... 73 In COM REMOTE RECALL 1 P5001 74 In DEMO MODE SELECT P5001 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 P5001 16 Out TIME MARK OUT outputs a 1 ms 1...

Page 67: ...agnetic 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 500W Series unit can receive pressure altitude air data and fuel data from certain systems on the GPS RS 232 IN 1 port The 500W 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 inf...

Page 68: ... 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 Time to Go 260G Date BCD 261G GPS Discrete Word 1 275G LRN Status Word 300G Station Declination T...

Page 69: ...ssion 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 Course 1 173 Localizer Deviation 174 Glideslope Deviation 22...

Page 70: ... Pin I O GPS ARINC 429 OUT A P5001 46 Out GPS ARINC 429 OUT B P5001 47 Out GPS ARINC 429 IN 1 A P5001 48 In GPS ARINC 429 IN 1 B P5001 49 In GPS ARINC 429 IN 2 A P5001 50 In GPS ARINC 429 IN 2 B P5001 51 In VOR ILS ARINC 429 OUT A P5006 24 Out VOR ILS ARINC 429 OUT B P5006 23 Out VOR ILS ARINC 429 IN A P5006 36 In VOR ILS ARINC 429 IN B P5006 35 In The GPS and VOR ILS ARINC 429 outputs conform to ...

Page 71: ...en TRANSMIT INTERLOCK is active the GNS 530W 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 transmit simultaneously 4...

Page 72: ...audio and INTERCOM MIC audio 4 7 2 4 DISCRETE INPUTS Pin Name Connector Pin I O TRANSMIT INTERLOCK P5002 14 In COM REMOTE TRANSFER P5002 15 In VLOC REMOTE TRANSFER P5006 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 73: ...OC 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 P5006 15 Out GLIDESLOPE SUPERFLAG P5006 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 The...

Page 74: ...S 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 P5006 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 75: ... data stream set to indicate that a localizer frequency is tuned which stows the needle or drive it to the 3 o clock position 4 9 2 RMI OBI Electrical Characteristics Pin Name Connector Pin I O MAIN OBI CLOCK P5001 43 Out MAIN OBI SYNC P5001 45 Out MAIN OBI DATA P5001 44 Out Pin Name Connector Pin I O VOR OBI CLOCK P5006 25 Out VOR OBI SYNC P5006 26 Out VOR OBI DATA P5006 27 Out The output driver ...

Page 76: ...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 Connect...

Page 77: ...ng configuration 4 10 4 DME Tuning Calibration and Checkout None 4 10 5 DME Tuning Interconnect Refer to Appendix H for interconnect information NOTE For the GNS 530W 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 Section 5 3 12 and Figure H 23 ...

Page 78: ...ad 4 11 4 Miscellaneous Pin Name Connector Pin I O TAWS INHIBIT IN P5050 1 In TAWS AUDIO INHIBIT IN P5050 2 In TAWS AUDIO ACTIVE OUT P5050 15 Out The TAWS INHIBIT IN and TAWS AUDIO INHIBIT IN are active low NOTE TAWS functions can also be inhibited via the 500W Series user interface TAWS AUDIO INHIBIT IN is used to inhibit TAWS audio This can be connected to inhibit output lines of another unit wh...

Page 79: ...roper installation 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 500W Series unit turned off press and hold the ENT key and turn the unit on Release the ENT key when the display activates ...

Page 80: ...s can each be configured independently for the desired function s SPEED Selection Description Low Standard low speed ARINC 429 nominally 12 5 Kb per second High High speed ARINC 429 nominally 100 Kb 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 400W 50...

Page 81: ... course information from the following Flight Control systems Bendix King KFC 400 Garmin GAD 42 Selected course heading and true airspeed data from the Garmin GAD 42 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 heading and joystick waypoint information from the following EFIS...

Page 82: ...ined by the GAMA General Aviation Subset 2 nd Edition including GAMA Graphics Protocol A The output data includes navigation and flight plan information including graphical representation of flight plan procedures to the following systems Sandel SN3308 Sandel SN3500 GAMA 429 Pro Line 21 ARINC 429 data as defined by the GAMA General Aviation Subset 2 nd Edition The output data includes navigation a...

Page 83: ...access to weather and messaging from the following units Garmin GDL 69 69A Icarus alt Serial altitude data from the following units Icarus Instruments 3000 Sandia SAE5 35 Garmin GTX 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 ...

Page 84: ...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 500W Series units GDL 69 Serial communication to a Garmin GDL 69 69A HW EGPWS Serial communication to a Bendix King Honeywell KGP 560 EGPWS Ryan TCAD Serial communication with a Ryan TCAD 9900B Series system WX 500 Serial communication to an L3 Commun...

Page 85: ...LECT Selection Description Auto When in GPS mode the GPS Select discrete is unasserted open whenever a GPS approach mode is active no associated messages appear and no pilot action is required The pilot is also allowed to select automatic or manual GPS to ILS CDI transitions on the AUX CDI ALARMS page Prompt When in GPS mode the GPS Select discrete is unasserted open whenever a GPS approach mode i...

Page 86: ...emperature SAT Static Air Temperature TAT Total Air Temperature IAS Indicated Airspeed TAS True Airspeed W SPD Wind Speed HDG True Heading W DIR Wind Direction GPS SC GPS Selected Course VLC SC VOR LOC Selected Course GNS 530W Only CDI Status of the CDI key GNS 530W Only B ALT Barometric corrected Altitude D ALT Density Altitude P ALT Pressure Altitude L FF Left Engine Fuel Flow R FF Right Engine ...

Page 87: ...e 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 18 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 ve...

Page 88: ...ro to 99 and is set to 25 at the factory PHOTO SLP OFFST Photocell Slope Offset These fields are equivalent to the SLOPE OFFSET fields described above with the exception that they only control the display lighting characteristics when the lighting bus control is below the level specified in the PHOTO TRANS field Both fields have a range of 0 zero to 99 and are set to 50 at the factory 5 3 7 GPS DA...

Page 89: ...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 as selected on this page TERM The TERM annunciator is active and inactive as selected on this page VLOC The VLOC source select annunciator is active and inactive as selected on this page WPT The WPT annunciator ...

Page 90: ...OM flag is hidden To The TO flag is in view SELECTED COURSE Select 150 on the CDI HSI that is connected to the 500W Series unit s MAIN OBS inputs The SELECTED COURSE field should indicate near to 150 and a Calibrate to 150 field appears Selecting this field calibrates the 500W Series unit to match the input source Verify OBS operation by checking that the course displayed on the 500W Series unit i...

Page 91: ...nore CDI key This causes the field above the CDI key to always display GPS regardless of CDI key presses This may be necessary for certain EFIS systems where navigation sensor selection must be accomplished on the EFIS or its control panel OBI SOURCE GNS 530W Only Selection Description Always GPS The MAIN King Serial OBI outputs are always GPS This is useful if it is desired to switch a Bendix Kin...

Page 92: ...the SQ 250 setting 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 00 zero and 63 The higher the number the more signal is required to break squelch SIDETN Sets the sidetone audio output level May be set to any value between 00 zero and 63 NOTE The sidetone...

Page 93: ...elect the VOR DISCRETE INPUTS page see Figure 5 14 This page allows you to verify the operation of an external VLOC transfer switch that may be present in the installation Selection Verify That REMOTE XFR The box is filled in while a remote VLOC transfer switch is pressed Figure 5 14 VOR DISCRETE INPUTS Page ...

Page 94: ...deflected left of center Center The CDI is centered Std right The CDI is deflected right of center Full right The CDI is deflected full scale to the right down Max right The CDI is pegged to the right down NAV FLAG LAT VERT Selection Verify That Hide The LAT VERT flag is hidden View The LAT VERT flag is in view SPR FLG LAT VERT Selection Verify That Hide The LAT VERT superflag is hidden View The L...

Page 95: ...RX and TX Selection Description Low Standard low speed ARINC 429 nominally 12 5 kilobits per second High High speed ARINC 429 nominally 100 kilobits per second SDI Selection Description Common RX Accepts all 429 inputs TX Generates all 429 outputs with SDI 0 VOR ILS 1 Number 1 Pilot VOR ILS Receiver RX Accepts 429 inputs with SDI 0 or 1 TX Generates all 429 outputs with SDI 1 VOR ILS 2 Number 2 Co...

Page 96: ...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 17 Figure 5 17 Measurement of GPS Vertical Offset Use the large and small knobs to enter the offset value and press ENT to save Figure 5 18 GPS Vertical Offset Page ...

Page 97: ...ORMSCOPE TEST page see Figure 5 20 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 mode ...

Page 98: ...lf test mode by highlighting Test Mode and pressing ENTER on the 500W Series unit Refer to the L3 Communications SkyWatch installation manual for system checkout For Ryan TCAD see Figure 5 23 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 Unrestricted UNR and that the TCAD is reporting the co...

Page 99: ...to annunciate TAWS alerts Default Male Select the male voice to annunciate TAWS alerts 5 3 21 2 PLAY MSG Field The PLAY MSG field allows the playback of all the individual TAWS alert messages It does not control the configuration of the messages in any manner 5 3 21 3 VOLUME Field The VOLUME field sets the volume of the TAWS alerts from 0 volume left side to 100 volume right side The default value...

Page 100: ...he specified text Default 5 3 22 TAWS AUDIO CONFIG 2 Page Select the TAWS AUDIO CONFIG 2 page see Figure 5 27 This page allows configuration of TAWS audio 5 3 22 1 RTC CAUTION Field Selection Description Caution Terrain 2x Sets the Forward Looking Terrain Clearance FLTA Reduced Required Terrain Clearance RTC cautionary alert to the specified text Default Terrain Ahead 2x Sets the Forward Looking T...

Page 101: ...ified text Terrain Ahead 2x Sets the Forward Looking Terrain Clearance FLTA Imminent Terrain Impact ITI cautionary alert to the specified text Default 5 3 22 6 ITI WARNING Field Selection Description Terrain 2x Pull Up 2x Sets the Forward Looking Terrain Clearance FLTA Imminent Terrain Impact ITI warning alert to the specified text Terrain Ahead Pull Up 2x Sets the Forward Looking Terrain Clearanc...

Page 102: ...ection Description Attenuation Sets the attenuation value for the GDL 69 69A Refer to the GDL 69 69A Installation manual 190 00355 02 to determine the correct attenuation value Model Sets the model to either GDL 69 weather only or GDL 69A weather and audio 5 3 24 DATA LINK DIAGNOSTICS Page The 8 character test word returned from the GDL 69 is displayed on the DATA LINK DIAGNOSTICS page for each of...

Page 103: ...utput perform the following 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 500W Series unit is connected to external annunc...

Page 104: ...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 500W 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 105: ...nel should also be turned on for this test The TAWS audio volume has an initial default of 60 of the maximum volume value The TAWS volume needs to be set so as to ensure that aural alerts are audible under all anticipated noise environmental conditions 1 Select the configuration page labeled TAWS AUDIO CONFIG 1 2 Go to the PLAY MSG field Rotate the small right knob to play the various TAWS audio m...

Page 106: ...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 500W 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 107: ... all 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 500W Series When installing GNS 500W Series equipment in accordance with the appropriate STC it is the responsibility of the installer to ensure that the GNS 500W Series unit modification is compatibl...

Page 108: ...Hz 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 the...

Page 109: ...ne the unit to a local VHF frequency and verify the receiver output produces a clear and understandable audio output Verify the transmitter functions properly by contacting another station and getting a report of reliable communications 5 5 6 TAWS System Check For Units With TAWS Only While on the ground turn the 500W Series unit on following normal power up procedures The audio panel should also ...

Page 110: ...FS40 50 is displayed correctly 6 Cycle power to the second GNS 500W Series unit and acknowledge the prompts until it gets to the self test page see Section 5 5 1 7 Switch to GPS2 data by pressing the 1 2 key on the EFS40 50 control panel and repeat steps 3 through 5 with the second GNS 500W Series unit 5 5 7 2 Sandel SN3308 Interface Check If a Sandel SN3308 EHSI has been connected to the GNS 500W...

Page 111: ...Active Waypoint GARMN 6 On the first GNS 500W Series unit verify that an OBS value is displayed and not dashed out 7 Acknowledge the self test on the first GNS 500W Series unit by pressing the ENT key 8 Select VLOC on the first GNS 500W Series unit and verify that the SN3308 displays NAV 1 or NAV 2 depending on what navigation source the GNS 530W is 9 Using a VOR test set verify that the CDI devia...

Page 112: ...he GNS 530W is 7 Ensure that the NAV1 or NAV2 indication does not have a red line through it 5 5 7 4 EHSI Deviation Scaling If HSI CDI Is Driven by the 500W Series Unit Via Serial Data If the GNS 500W Series unit has a serial connection to an EFIS display not covered by the AML STC proper scaling of the EFIS CDI and VDI must be verified 1 Cycle power to the GNS 500W Series unit and acknowledge the...

Page 113: ...mscope has been connected to the GNS 500W Series unit the Stormscope interface should be verified as described in this section 1 Go to the Lightning page on the GNS 500W 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 7 8 GMX 2...

Page 114: ... Checkout Procedure 1 Go to the XM Audio page in the AUX 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 re...

Page 115: ...ll points towards the GPS waypoint selected 5 5 7 11 2 VOR OBI Output GNS 530W Only If the VOR OBI output from the GNS 530W is connected to an RMI navigation indicator verify the interface as described in this section 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 V...

Page 116: ...at the 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 GNS 530W 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 least 50 ...

Page 117: ... 530W Verify that the GPSS mode disengages 5 6 6 TAWS Audio Flight Check for units with TAWS only NOTE The TAWS volume needs to be loud enough to ensure that aural alerts are audible under all anticipated noise environmental conditions This check verifies that TAWS aurals can be heard during flight but the ambient noise conditions under which it is verified are not worst case Consequently the Five...

Page 118: ...sure that the Airplane Flight Manual Supplement AFMS is completed and inserted in the Airplane Flight Manual AFM or Pilot s Operating Handbook POH 1 Fill in the required airplane information in the AFMS 2 Fill in the appropriate checkbox in the Limitations section of the AFMS corresponding to the type of GPS antenna that was installed 3 Fill in the appropriate checkbox in the Limitations section o...

Page 119: ..._______ 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 _______________ _______________ SEL CRS for GPS...

Page 120: ...ain 2x DME Mode Directed freq 1 Directed freq 2 Terrain Ahead 2x ITI Warning Terrain 2x Pull Up 2x GDL Configuration N A Terrain Ahead Pull Up 2x Attenuation ______________ Model GDL 69A GDL 69 After completing configuration and prior to checkout restart unit for changes to take effect SYSTEM CHECKOUT Ground Checks Configuration Mode MAIN ANALOG INDICATOR N A ANNUNCIATOR OUTPUTS CDI left centered ...

Page 121: ...08 VHF com interference checked N A Sandel SN3500 N A ARINC 429 Traffic System VHF NAV CHECKOUT GNS 530W ONLY N A Ryan TCAD VOR reception checked N A L 3 Communications Stormscope Localizer reception checked N A Garmin GMX 200 MX20 Deviation needle and flag checked N A Garmin GDL 69 69A N A Crossfill check VHF COM CHECKOUT GNS 530W ONLY N A External RMI Receiver Transmitter operation checked N A D...

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Page 123: ... levels drop when avionics are turned on Noise interference from other avionics Turn all avionics 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...

Page 124: ...ort speed setting for port that device is connected to and verify that the speed is correct for that device 500W Series unit is not receiving heading from compass system ARINC 429 heading input used Wiring connections are incorrect Check wiring 500W Series unit does not have a position or flight plan entered Acquire GPS position and enter a flight plan 500W Series unit ARINC 429 output not configu...

Page 125: ...to ARINC 429 output port speed not correct Check ARINC 429 output port speed setting for port that device is connected to and verify that the speed is correct for that device ARINC 429 device is not receiving data from the GPS 500W GNS 530W Wiring connections are incorrect Check wiring 500W Series unit RS 232 port not configured correctly Check RS 232 port setting for port that device is connected...

Page 126: ...port for assistance GARMIN International Inc 1200 East 151st Street Olathe KS 66062 3426 USA Phone 913 397 8200 FAX 913 397 8282 http www garmin com Be prepared to offer the following information about the installation Installation configuration list of any accessories Model number part number with mod levels and serial number Software Versions Description of problem Efforts made to isolate the pr...

Page 127: ...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 500W 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 128: ... 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 500W Series GPS WAAS receiver when installed with an appropriate antenna li...

Page 129: ...s and data provided in this manual may be used to perform the alteration and obtain other FAA approval The 500W Series unit TAWS functionality is not approved for use in rotorcraft The 500W 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...

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Page 131: ... 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 500W Series unit will display a Low Battery and Unit Needs Service message when replacement is required Once the low battery message is displayed the battery should be replaced within 1 to 2 months If the battery is n...

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Page 133: ...ication Forms EQFs visit the Dealers Only site 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 500W 005 00221 09 GPS 500W TAWS 005 00221 41 GNS 530W 005 00221 42 GNS 530W TAWS 005 00221 43 GNS 530AW 005 00221 44 GNS 530AW TAWS 005 00221 45 ...

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Page 135: ...purpose of installation and approval of installation of the 500W Series unit equipment and associated interfaces to other previously approved equipment B 3 Continued Airworthiness Instructions Refer to the 500W Series Instructions for Continued Airworthiness P N 190 00357 65 B 4 STC Approved Model List The 400W 500W Series STC SA01933LA Approved Model List AML includes airplanes that are type cert...

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Page 137: ...500W Series Installation Manual Page C 1 190 00357 02 Rev D Appendix C RESERVED ...

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Page 139: ...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 500W Series unit approximately once every se...

Page 140: ... Current longitude where s E east or W west ddd degrees mm minutes hh hundredths of minutes C d d d Track in whole degrees D s s s Ground speed in 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...

Page 141: ...CII carriage return character 0D hex LF ASCII line feed character 0A hex Each waypoint in the route being navigated by the 500W Series unit has a Type 2 sentence output by the 500W Series unit approximately once every second If no route is being navigated by the 500W Series unit i e the active route is empty the following Type 2 sentence is output approximately once every second id item designator...

Page 142: ... 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 2 3 4 s x x x x...

Page 143: ...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 144: ...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 500W Series unit is capable of receiving the following 13 byte message from the ARNAV or Electronics Inte...

Page 145: ...78 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 chara...

Page 146: ...flow 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...

Page 147: ...s error 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...

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Page 149: ...L DRAWINGS F 1 Drawing List The following drawings are included in this section Figure F 1 GNS 530W Mounting Rack Dimensions Figure F 2 GNS 530W Mounting Rack Installation Figure F 3 GPS 500W Mounting Rack Installation Figure F 4 500W Series unit Recommended Panel Cutout Dimensions ...

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Page 151: ... Series Installation Manual Page F 3 190 00357 02 Rev D 2 3 58 4 3 1 78 7 2 6 66 C B 4 7 119 2 9 73 7 4 5 114 DIMENSIONS GPS 500W MODEL GNS 530W A GNS 530W SHOWN Figure F 1 GNS 530W Mounting Rack Dimensions ...

Page 152: ...TE ASSEMBLY 2 PART OF 011 00351 00 CONNECTOR KIT 330 00220 50 2 2 125 00046 00 1 2 2 2 3 1 4 FEED HARNESS WIRES THROUGH BACKSHELL BEFORE INSERTION INTO CONNECTOR 5 SNAP NUTPLATE OVER BACKSHELL 7 APPLY THREAD LOCKING COMPOUND 291 00023 02 TO ALL THREADED FASTENERS 4 5 4 5 2 212 00022 00 4 PLCS 1 5 2 4 330 00220 50 4 2 125 00045 00 2 5 330 00185 78 336 00021 00 AS REQD 3 6 REMOVE ADHESIVE BACKING AN...

Page 153: ...L THREADED FASTENERS 4 5 2 1 4 2 2 5 3 6 REMOVE ADHESIVE BACKING AND APPLY FOAM TO 3 1 REAR VIEW OF CONNECTOR PLATE 78 PIN 44 PIN 25 PIN P5001 P5006 P5002 78 PIN P5050 8 DASHED ELIPSE INDICATES CHANGED CONTENT 211 60234 10 2 PLCS 115 00345 00 211 63234 12 2 PLCS 330 00053 01 252 00062 00 211 63234 12 125 00050 00 SHIELD GROUND 212 00022 00 NUT SUPPLIED WITH CONNECTOR 330 00185 78 336 00021 00 AS R...

Page 154: ...OM BACK OF AIRCRAFT PANEL ONLY OPTION 3 MAXIMUM AIRCRAFT PANEL THICKNESS IS 125 INCH 3 2 mm 4 61 117 1 6 32 160 5 6 32 160 5 05 1 3 2 79 70 9 75 19 1 75 19 1 2 75 69 9 4 46 113 3 6 25 158 8 05 1 3 NOTES 1 DIMENSIONS INCH mm 2 IF THE FRONT LIP OF THE MOUNTING RACK IS BEHIND THE SURFACE OF THE AIRCRAFT PANEL THE 500W SERIES UNIT CONNECTORS MAY NOT FULLY ENGAGE Figure F 4 500W Series Unit Recommended...

Page 155: ...he aircraft always refer to the manufacturers documentation for complete pinout and interconnect information G 1 Audio Panels 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 Manufacturer Model Data Format Not...

Page 156: ...on Discrete Honeywell Bendix King KFC 225 Analog Deviation Discrete ARINC 429 GPSS I II III IV 21 31 41 2000 Triden Analog Deviation Discrete Century AK 1081 ARINC 429 GPSS GPSS Roll Steering Converter System Twenty Thirty 40 50 55 60 1 60 2 60 PSS 65 Analog Deviation Discrete System Fifty Five X Analog Deviation Discrete ARINC 429 GPSS S TEC ST 901 ARINC 429 GPSS GPSS Roll Steering Converter Cess...

Page 157: ... ARINC 429 PFD software P N 530 00194 or later is required G 7 EHSI Manufacturer Model Data Format Notes SN 3308 Analog ARINC 429 GPS lateral and vertical guidance is provided using the analog interface Sandel SN3500 ARINC 429 Vertical guidance is provided for GPS approaches G 8 IRU AHRS Manufacturer Model Data Format Notes Honeywell Bendix King KAU 461 ARINC 429 Collins AHC 85E ARINC 429 Honeywel...

Page 158: ...ng KGP 560 KTA 870 KTA 810 KMH 880 KMH 820 KTA 970 KTA 910 1 KMH 980 KMH 920 1 RS 232 ARINC 429 ARINC 429 ARINC 429 ARINC 429 High Speed High Speed High Speed High Speed L3 Communications SKY497 SkyWatch SKY899 SkyWatch HP WX 500 ARINC 429 ARINC 429 RS 232 High Speed High Speed Ryan 9900B BX RS 232 1 500W series main software version 3 00 or later is required G 11 DME Manufacturer Model Data Forma...

Page 159: ... P N 14 113 Mid Continent MD41 1408A MD41 1404A MD41 1418A MD41 1414A MD41 1468A MD41 1478A MD41 1464A MD41 1474A MD41 1470 MD41 1484W MD41 1488W Indicator Switch GPS Annunciations Both 14VDC and 28VDC indicators refer to Mid Continent documentation for availability of switch functions on each unit Vendor Contact Information provided for convenience only Staco Switch 1139 Baker Street Costa Mesa C...

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Page 161: ...nnect Two GNS 530W One Sandel SN3308 Figure H 13 ARINC 429 Sandel EHSI Interconnect Two GNS 530W Two Sandel SN3308 Figure H 14 ARINC 429 RS 232 Air Data IRU AHRS Interconnect Figure H 15 Traffic Advisory System Interconnect Figure H 16 GTX 330 Interconnect Figure H 17 Weather and Terrain Interconnect Figure H 18 Audio Panel Interconnect Figure H 19 VOR ILS Indicator Interconnect Figure H 20 RMI OB...

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Page 163: ...500W Series Installation Manual Page H 3 190 00357 02 Rev D Figure H 1 500W Series Unit System Interface Diagram ...

Page 164: ...Page H 4 500W Series Installation Manual Rev D 190 00357 02 Figure H 2 GNS 530W Typical Installation Sheet 1 of 2 ...

Page 165: ...500W Series Installation Manual Page H 5 190 00357 02 Rev D Figure H 2 GNS 530W Typical Installation Sheet 2 of 2 ...

Page 166: ...Page H 6 500W Series Installation Manual Rev D 190 00357 02 Figure H 3 GPS 500W Typical Installation Sheet 1 of 2 ...

Page 167: ...500W Series Installation Manual Page H 7 190 00357 02 Rev D Figure H 3 GPS 500W Typical Installation Sheet 2 of 2 ...

Page 168: ...Page H 8 500W Series Installation Manual Rev D 190 00357 02 Figure H 4 Power Lighting and Antennas Interconnect Sheet 1 of 3 ...

Page 169: ...500W Series Installation Manual Page H 9 190 00357 02 Rev D Figure H 4 Power Lighting and Antennas Interconnect Sheet 2 of 3 ...

Page 170: ...Page H 10 500W Series Installation Manual Rev D 190 00357 02 Figure H 4 Power Lighting and Antennas Interconnect Sheet 3 of 3 ...

Page 171: ...500W Series Installation Manual Page H 11 190 00357 02 Rev D Figure H 5 Gray Code Encoding Altimeter Blind Encoder Interconnect ...

Page 172: ...Page H 12 500W Series Installation Manual Rev D 190 00357 02 Figure H 6 Main Indicator Interconnect ...

Page 173: ...500W Series Installation Manual Page H 13 190 00357 02 Rev D Figure H 7 KI 209A Main Indicator Interconnect ...

Page 174: ...Page H 14 500W Series Installation Manual Rev D 190 00357 02 Figure H 8 KI 208A Main Indicator Interconnect ...

Page 175: ...500W Series Installation Manual Page H 15 190 00357 02 Rev D Figure H 9 RS 232 Serial Data Interconnect Sheet 1 of 2 ...

Page 176: ...Page H 16 500W Series Installation Manual Rev D 190 00357 02 Figure H 9 RS 232 Serial Data Interconnect Sheet 2 of 2 ...

Page 177: ...500W Series Installation Manual Page H 17 190 00357 02 Rev D Figure H 10 ARINC 429 EFIS Interconnect Sheet 1 of 2 ...

Page 178: ...Page H 18 500W Series Installation Manual Rev D 190 00357 02 Figure H 10 ARINC 429 EFIS Interconnect Sheet 2 of 2 ...

Page 179: ...ALID FLAG NAV VALID FLAG 37 19 CDI L CDI R 15 33 GS VALID FLAG GS VALID FLAG 17 35 TO FLAG FROM FLAG 16 34 GSI UP GSI DOWN 27 ILS 1 ENERGIZE 25 26 MAIN TO MAIN FROM 5 7 6 P1 8 Figure H 11 ARINC 429 Sandel EHSI Interconnect One 500W Series Unit One Sandel SN3308 Sheet 1 of 2 ...

Page 180: ...Page H 20 500W Series Installation Manual Rev D 190 00357 02 Figure H 11 ARINC 429 Sandel EHSI Interconnect One 500W Series Unit One Sandel SN3308 Sheet 2 of 2 ...

Page 181: ...500W Series Installation Manual Page H 21 190 00357 02 Rev D Figure H 12 ARINC 429 Sandel EHSI Interconnect Two GNS 530W One Sandel SN3308 Sheet 1 of 2 ...

Page 182: ...Page H 22 500W Series Installation Manual Rev D 190 00357 02 Figure H 12 ARINC 429 Sandel EHSI Interconnect Two GNS 530W One Sandel SN3308 Sheet 2 of 2 ...

Page 183: ...W Series Installation Manual Page H 23 190 00357 02 Rev D Figure H 13 ARINC 429 Sandel EHSI Interconnect Two GNS 530W Two Sandel SN3308 THE TWO GNS 530W TWO SN3308s CONFIGURATION IS CURRENTLY NOT SUPPORTED ...

Page 184: ...Page H 24 500W Series Installation Manual Rev D 190 00357 02 Figure H 14 ARINC 429 RS 232 Air Data IRU AHRS Interconnect Sheet 1 of 2 ...

Page 185: ...500W Series Installation Manual Page H 25 190 00357 02 Rev D Figure H 14 ARINC 429 RS 232 Air Data IRU AHRS Interconnect Sheet 2 of 2 ...

Page 186: ...Page H 26 500W Series Installation Manual Rev D 190 00357 02 Figure H 15 Traffic Advisory System Interconnect Sheet 1 of 2 ...

Page 187: ...500W Series Installation Manual Page H 27 190 00357 02 Rev D Figure H 15 Traffic Advisory System Interconnect Sheet 2 of 2 ...

Page 188: ...Page H 28 500W Series Installation Manual Rev D 190 00357 02 Figure H 16 GTX 330 Interconnect ...

Page 189: ...500W Series Installation Manual Page H 29 190 00357 02 Rev D Figure H 17 Weather and Terrain Interconnect Sheet 1 of 2 ...

Page 190: ...Page H 30 500W Series Installation Manual Rev D 190 00357 02 Figure H 17 Weather and Terrain Interconnect Sheet 2 of 2 ...

Page 191: ...500W Series Installation Manual Page H 31 190 00357 02 Rev D Figure H 18 Audio Panel Interconnect Sheet 1 of 2 ...

Page 192: ...Page H 32 500W Series Installation Manual Rev D 190 00357 02 Figure H 18 Audio Panel Interconnect Sheet 2 of 2 ...

Page 193: ...500W Series Installation Manual Page H 33 190 00357 02 Rev D Figure H 19 VOR ILS Indicator Interconnect ...

Page 194: ...Page H 34 500W Series Installation Manual Rev D 190 00357 02 Figure H 20 RMI OBI Interconnect ...

Page 195: ...500W Series Installation Manual Page H 35 190 00357 02 Rev D Figure H 21 King Serial Panel DME Tuning Interconnect ...

Page 196: ...Page H 36 500W Series Installation Manual Rev D 190 00357 02 Figure H 22 King Serial Remote DME Tuning Interconnect ...

Page 197: ...500W Series Installation Manual Page H 37 190 00357 02 Rev D Figure H 23 Parallel 2 of 5 DME Tuning Interconnect ...

Page 198: ...Page H 38 500W Series Installation Manual Rev D 190 00357 02 Figure H 24 TAWS Interconnect ...

Page 199: ...500W Series Installation Manual Page H 39 190 00357 02 Rev D Figure H 25 Bendix King Analog Autopilot Interconnect ...

Page 200: ...Page H 40 500W Series Installation Manual Rev D 190 00357 02 Figure H 26 Century Autopilot Interconnect Sheet 1 of 2 ...

Page 201: ...500W Series Installation Manual Page H 41 190 00357 02 Rev D H 26 Century Autopilot Interconnect Sheet 2 of 2 ...

Page 202: ...Page H 42 500W Series Installation Manual Rev D 190 00357 02 Figure H 27 S TEC Autopilot Interconnect Sheet 1 of 2 ...

Page 203: ...500W Series Installation Manual Page H 43 190 00357 02 Rev D Figure H 27 S TEC Autopilot Interconnect Sheet 2 of 2 ...

Page 204: ...on Manual Rev D 190 00357 02 SN3500 Sandel 3 35 33 21 P2 30 15 31 2 17 32 A B Nav 429 In Port 1 2 A B 429 Out A B GPS 429 In Port 1 2 5 Figure H 28 ARINC 429 Sandel EHSI Interconnect One 500W Series Unit One Sandel SN3500 Sheet 1 of 2 ...

Page 205: ...500W Series Installation Manual Page H 45 190 00357 02 Rev D Figure H 28 ARINC 429 Sandel EHSI Interconnect One 500W Series Unit One Sandel SN3500 Sheet 2 of 2 ...

Page 206: ...NCIATE GPS ANNUNCIATE 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 500W 530W 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 A...

Page 207: ...8 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 500W 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...

Page 208: ...Page H 48 500W Series Installation Manual Rev D 190 00357 02 Figure H 30 Parallel Slip Code DME Tuning Interconnect ...

Page 209: ...500W Series Installation Manual Page H 49 190 00357 02 Rev D Figure H 31 Cessna Autopilot Interconnect ...

Page 210: ...Page H 50 500W Series Installation Manual Rev D 190 00357 02 Figure H 32 Bendix Autopilot Interconnect ...

Page 211: ...500W Series Installation Manual Page H 51 190 00357 02 Rev D Figure H 33 Switches Interconnect ...

Page 212: ...Page H 52 500W Series Installation Manual Rev D 190 00357 02 Figure H 34 ARINC 429 Avidyne PFD MFD Interconnect Sheet 1 of 2 ...

Page 213: ...500W Series Installation Manual Page H 53 190 00357 02 Rev D Figure H 34 ARINC 429 Avidyne PFD MFD Interconnect Sheet 2 of 2 ...

Page 214: ...Page H 54 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank ...

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