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Page 5-36

500W Series Installation Manual

Rev. D

190-00357-02

NOTE

The following sections only verify the correct interface of GDL 69/69A to the GNS
500W Series unit. It does not activate the GDL 69 XM data link radio. Complete
instructions for activating the XM data link radio can be found in document
190-00355-04.

5.5.7.9.1 XM Satellite Radio Weather Checkout Procedure

1.

With the 500W Series unit running in the normal mode, go to the XM Information page (in the
AUX page group).

2.

Verify that the DATA ID field has a valid ID and does not contain “---“. For a GDL 69A, the
AUDIO ID field should also display a valid ID.

3.

Go to the XM WX Timestamp page and verify that timestamp data is displayed. This may take
several minutes. (Time stamp data will not be available if the XM subscription has not been
activated.)

During XM activation, “Detecting Activation” will be displayed in the SERVICE CLASS field on the
XM Information page, and “Aviator” will be displayed once the XM signal is detected.

5.5.7.9.2 XM Satellite Radio Audio 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 required.

5.5.7.10 Crossfill Check (If Dual Units Installed With RS-232 Crossfill Connected)

Turn on both 500W Series units in the aircraft. For each 500W Series unit:

1.

Select the first AUX page (titled “FLIGHT PLANNING”).

2.

Select “CROSSFILL”.

3.

Verify that the displayed status is “Ready”. If “Not Available” is displayed, there may be an RS-
232 wiring problem between the two 500W Series units.

5.5.7.11 External RMI/OBI Interface Check

The GNS 500W Series unit RMI/OBI output can be used to drive an RMI (or OBI) navigation indicator.
This check verifies that the RMI/OBI is receiving data from the GNS 500W Series unit. If the following
steps do not perform correctly, check the electrical connections and configuration setup.

NOTE

The aircraft heading system must be operating properly in order for the RMI needle to
point correctly.

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Содержание GNS 530W

Страница 1: ...r 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 p...

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

Страница 3: ...anual 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 888 606 548...

Страница 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...

Страница 5: ...ubject 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 doc...

Страница 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...

Страница 7: ...rocedure 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 M...

Страница 8: ...S 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 Installatio...

Страница 9: ...ect 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...

Страница 10: ...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...

Страница 11: ...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 Ser...

Страница 12: ...Page viii 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

Страница 13: ...ade 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...

Страница 14: ...dards 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...

Страница 15: ...on 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 t...

Страница 16: ...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 receiv...

Страница 17: ...tion 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 Reacquisit...

Страница 18: ...ling 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...

Страница 19: ...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 eit...

Страница 20: ...quencies 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...

Страница 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 AT5...

Страница 22: ...p 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 Anten...

Страница 23: ...e 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 ha...

Страница 24: ...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...

Страница 25: ...ntal 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...

Страница 26: ...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 p...

Страница 27: ...iodic 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...

Страница 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 L...

Страница 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 5...

Страница 30: ...ic 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...

Страница 31: ...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...

Страница 32: ...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 l...

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

Страница 34: ...tenna 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...

Страница 35: ...ith 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 m...

Страница 36: ...e 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 e...

Страница 37: ...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...

Страница 38: ...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 1...

Страница 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 requireme...

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

Страница 41: ...0 010 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...

Страница 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 013 002...

Страница 43: ...its 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 10...

Страница 44: ...ow loss splitter used with the VOR LOC antenna Headphones 500 nominal impedance Microphone Low impedance carbon or dynamic with transistorized pre amp For a list of optional accessories source selecti...

Страница 45: ...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...

Страница 46: ...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 con...

Страница 47: ...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 p...

Страница 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...

Страница 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 coax...

Страница 50: ...0 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 frequenci...

Страница 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 96...

Страница 52: ...NC 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 S...

Страница 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 c...

Страница 54: ...tation 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 app...

Страница 55: ...CIATE 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 1...

Страница 56: ...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 AL...

Страница 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...

Страница 58: ...n 6 COM MIC AUDIO HI In 7 500 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 IN...

Страница 59: ...14 PARALLEL DME 8MHZ Out 15 VOR LOC SUPERFLAG Out 16 500 VOR ILS AUDIO HI Out 17 500 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 DM...

Страница 60: ...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...

Страница 61: ...tance to ground is 375 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 p...

Страница 62: ...4 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 P500...

Страница 63: ...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 rotor...

Страница 64: ...oint 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 th...

Страница 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 signal...

Страница 66: ...1 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...

Страница 67: ...gnetic 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 fu...

Страница 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 Aut...

Страница 69: ...sion 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 followin...

Страница 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...

Страница 71: ...hen 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 s...

Страница 72: ...o 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...

Страница 73: ...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 P5006 15 Out GLIDESLOPE SUPERFLAG P...

Страница 74: ...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...

Страница 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 OB...

Страница 76: ...e leakage current with respect to ground is less than 10 A 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...

Страница 77: ...g 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 89...

Страница 78: ...d 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 activ...

Страница 79: ...oper 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 Co...

Страница 80: ...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 pe...

Страница 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...

Страница 82: ...ned 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 pla...

Страница 83: ...ccess 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 Tra...

Страница 84: ...armin 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 G...

Страница 85: ...ECT 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 pilo...

Страница 86: ...mperature 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...

Страница 87: ...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 mi...

Страница 88: ...o 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 disp...

Страница 89: ...he 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...

Страница 90: ...M 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 a...

Страница 91: ...ore 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 accompl...

Страница 92: ...he 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...

Страница 93: ...lect 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...

Страница 94: ...eflected 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...

Страница 95: ...X 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 Accep...

Страница 96: ...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 Vert...

Страница 97: ...RMSCOPE 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 tes...

Страница 98: ...f 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...

Страница 99: ...o 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 n...

Страница 100: ...e 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 Descripti...

Страница 101: ...fied 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 T...

Страница 102: ...ction 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...

Страница 103: ...tput 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 cor...

Страница 104: ...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 da...

Страница 105: ...el 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 u...

Страница 106: ...isplayed 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 Way...

Страница 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 5...

Страница 108: ...z 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...

Страница 109: ...e 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...

Страница 110: ...S40 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...

Страница 111: ...ctive 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...

Страница 112: ...e 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...

Страница 113: ...scope 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 gro...

Страница 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 subscripti...

Страница 115: ...l 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...

Страница 116: ...t 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...

Страница 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 anticipa...

Страница 118: ...ure 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 AFM...

Страница 119: ...______ Source ___________ __________ Out High Low __________________ Resp Time Min ____ _____ ____ _____ Slope Offset ____ _____ ____ _____ SDI Common LNAV 1 LNAV 2 Photo Trans ___________ N A Photo S...

Страница 120: ...in 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 c...

Страница 121: ...8 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 c...

Страница 122: ...Page 5 44 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

Страница 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...

Страница 124: ...rt 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 Wi...

Страница 125: ...o 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 re...

Страница 126: ...ort 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...

Страница 127: ...pproved 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 equipmen...

Страница 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 ai...

Страница 129: ...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...

Страница 130: ...Page 7 4 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

Страница 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 w...

Страница 132: ...Page 8 2 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

Страница 133: ...cation 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 50...

Страница 134: ...Page A 2 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

Страница 135: ...urpose 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...

Страница 136: ...Page B 2 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

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

Страница 138: ...Page C 2 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

Страница 139: ...ription 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 d...

Страница 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 na...

Страница 141: ...II 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 approxim...

Страница 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...

Страница 143: ...tude 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 indi...

Страница 144: ...x03 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 r...

Страница 145: ...8 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 n...

Страница 146: ...low 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 S...

Страница 147: ...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 chara...

Страница 148: ...Page E 6 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

Страница 149: ...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...

Страница 150: ...Page F 2 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

Страница 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 Dimen...

Страница 152: ...E 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...

Страница 153: ...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...

Страница 154: ...M 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 NOTE...

Страница 155: ...e 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 7...

Страница 156: ...n 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...

Страница 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 interfac...

Страница 158: ...g 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 SkyWat...

Страница 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...

Страница 160: ...Page G 6 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

Страница 161: ...nect 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 Adviso...

Страница 162: ...Page H 2 500W Series Installation Manual Rev D 190 00357 02 This Page Intentionally Left Blank...

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

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

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

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

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

Страница 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...

Страница 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...

Страница 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...

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

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

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

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

Страница 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...

Страница 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...

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

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

Страница 179: ...LID 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 San...

Страница 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...

Страница 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...

Страница 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...

Страница 183: ...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 SUPPO...

Страница 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...

Страница 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...

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Страница 204: ...n 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 Un...

Страница 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...

Страница 206: ...CIATE 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 ANNUNC...

Страница 207: ...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...

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

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

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

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

Страница 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...

Страница 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...

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

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