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500 SERIES INSTALLATION MANUAL

Page 5-5

190-00181-02

Rev

Q

5.2.3 MAIN SYSTEM CONFIG

Select the MAIN SYSTEM CONFIG Page (see Figure 5-
3). This page allows you to configure the Fuel and Terrain
options.

Fuel

Select

Fuel

in the

CONFIGURE

field to select the FUEL

TYPE (

AV Gas, Jet A, or Jet B)

Selection Description
AV gas

The aircraft is using Aviation gas (5.8 lbs./gal.)

Jet A

The aircraft is using Jet A or Jet A-1 fuel (6.7 lbs./gal.)

Jet B

The aircraft is using Jet B (JP-4) fuel (6.5 lbs./gal.)

Terrain

Select

Terrain

in the

CONFIGURE

field to select the

TERRAIN TYPE (

NONE, TERRAIN,

or

TAWS

).

To test the Terrain Data Card, highlight the

TEST CARD

field and press the ENT key. Verify that the

TEST CARD

field indicates “PASS”. A “FAIL” condition indicates that
the Terrain Data Card is unusable.

The HW CONFIG field displays what type of Map Board
is installed in the 500 Series unit. The HW CONFIG field
will display "

TAWS

" if the appropriate hardware is

installed to enable the TAWS functionality. The HW
CONFIG field will display "

TERRAIN

" if the appropriate

hardware is installed to enable the TERRAIN functionality.
If neither the TAWS nor TERRAIN hardware is installed, the HW CONFIG field will display "

No

TERRAIN

".

Selection Description
None

No terrain functionality (TAWS) is installed.

TERRAIN

The unit is configured for TERRAIN capability.

TAWS

The unit is configured for TAWS capability.

500 Series TERRAIN units may be manually configured for

TERRAIN

or

None

. 500 Series TAWS unit

software will automatically detect TAWS hardware and automatically upgrade itself to

TAWS

if the

appropriate hardware is installed.

If an incorrect hardware/software combination is entered, the message "HARDWARE CONFLICT!
MANUALLY ENTER TERRAIN TYPE" is displayed on the MAIN SYSTEM CONFIG page beside the
part number field. Also, a “Terrain configuration conflict” message will be issued in NORMAL mode if an
incorrect hardware/software combination is selected.

Note that the 500 Series TERRAIN (and TAWS) functionality is not designed nor approved for use in
helicopters.

Figure 5-3. MAIN SYSTEM CONFIG

Page

Figure 5-4. MAIN SYSTEM CONFIG

Page

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Содержание GPS 500

Страница 1: ...national Inc 190 00181 02 Revision Q November 2005 500 SERIES INSTALLATION MANUAL GPS 500 and GNS TM 530 530A TAWS GNS is a trademark of Garmin Ltd or its subsidiaries and may not be used without the...

Страница 2: ...Technical Support Line Toll Free 888 606 5482 Web Site Address www garmin com Garmin Europe Ltd Unit 5 The Quadrangle Abbey Park Industrial Estate Romsey SO51 9DL U K Phone 44 0870 851241 RECORD OF RE...

Страница 3: ...tion of the EAR may be 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 reprod...

Страница 4: ...MOVAL 3 8 3 9 COM ANTENNA INSTALLATION CHECK GNS 530 3 8 4 SYSTEM INTERCONNECTS 4 1 PIN FUNCTION LIST 4 1 4 2 POWER LIGHTING AND ANTENNAS 4 6 4 3 ALTIMETER 4 7 4 4 MAIN INDICATOR 4 8 4 5 ANNUNCIATORS...

Страница 5: ...MOUNTING RACK INSTALLATION F 9 FIGURE F 5 GPS 500 MOUNTING RACK INSTALLATION F 11 FIGURE F 6 500 SERIES RECOMMENDED PANEL CUTOUT DIMENSIONS F 13 FIGURE F 7 500 SERIES SYSTEM INTERFACE DIAGRAM F 15 FIG...

Страница 6: ...rmin com using their Garmin provided user name and password MOD LEVEL SERVICE BULLETIN NUMBER SERVICE BULLETIN DATE PURPOSE OF MODIFICATION 1 0019 11 7 00 Replace fuse in COM circuit with a resistor 2...

Страница 7: ...udes IFR certified airborne VHF communications transceiver and an IFR certified airborne VOR Localizer and Glideslope receivers The A model is a 28 Vdc unit with a 16 Watt COM transmitter Both units a...

Страница 8: ...8 kg GNS 530 Weight Installed with rack and connectors 8 7 lbs 3 95 kg 1 3 2 General Specifications Operating Temperature Range 20qC to 55qC For more details see Environmental Qualification Form Humid...

Страница 9: ...The audio output shall not vary by more than 6 dB when the level of the RF input signal modulated 30 at 1000 Hz is varied from 5 PV to 450 000 PV Sensitivity S N N on all channels shall be greater th...

Страница 10: ...of an RF signal b in the absence of the 9960 Hz modulation c in the absence of either one of the two 30 Hz modulations d When the level of a standard VOR deviation test signal produces less than a 50...

Страница 11: ...racteristics From 86 dBm and 33 dBm input of a Standard VOR Audio Test Signal audio output levels shall not vary more than 3 dB Selectivity Nose Bandwidth The input signal level required to produce th...

Страница 12: ...channel At frequencies displaced by r132 kHz or greater the input signal shall be at least 60 dB down Standard deflection a With a standard deflection FLY DOWN condition 90 Hz dominant the output shal...

Страница 13: ...ature range Modifications not expressly approved by Garmin could invalidate the license and make it unlawful to operate the equipment 1 6 CERTIFICATION The GPS receivers in the 500 Series units are ce...

Страница 14: ...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 WARRANTY GIVES YOU SPE...

Страница 15: ...above the aircraft when in level flight Figure 2 1 illustrates a typical GPS antenna installation The antenna should be located at least three feet from transmitting antennas such as VHF COM HF trans...

Страница 16: ...ate as far as possible from all COM antennas and all COM transceivers including the 500 Series COM ELT antennas and DF receiver antennas The GPS antenna is less susceptible to harmonic interference if...

Страница 17: ...minute at a pressure equivalent to 0 1 inches of water Potential damage to your 500 Series unit may occur by using outside forced air to cool the equipment Therefore it is recommended that an electric...

Страница 18: ...proofness S Continuous Stream Fluids F Deicing Fluid Lightning 2A Direct Effects Icing C 0 15 thick 2 Electrical Characteristics LNA Supply voltage 4 5 0 5 Vdc LNA Supply Current 20 mA Maximum LNA Ope...

Страница 19: ...10 00325 00 011 00940 00 N Y N BLACK 14 or 28 V 10 W 010 00325 01 011 00940 00 N Y Y BLACK 14 or 28 V 10 W 010 00325 10 011 00940 10 N Y N GRAY 14 or 28 V 2 10 W 010 00325 11 011 00940 10 N Y Y GRAY 1...

Страница 20: ...00562 00 N N BLACK N 010 00176 01 011 00562 00 N Y BLACK N 010 00176 10 011 00562 10 N N GRAY Y 010 00176 11 011 00562 10 N Y GRAY Y 010 00291 00 011 00863 00 Y N BLACK N 010 00291 01 011 00863 00 Y Y...

Страница 21: ...SEMBLY 011 00147 00 1 NUT PLATE 115 00080 00 1 SCREW 10 32 x 5 8 211 62212 14 4 ANTENNA GASKET 253 00011 00 1 2 Other accessories include the following ITEM GARMIN P N MOUNTING RACK 500 530 115 00345...

Страница 22: ...HORIZONTAL YES 013 00079 11 14V DC 14V DC HORIZONTAL NO 013 00079 20 28V DC 5V DC HORIZONTAL YES 013 00079 21 28V DC 5V DC HORIZONTAL NO 013 00079 50 28V DC 28V DC VERTICAL YES 013 00079 51 28V DC 28V...

Страница 23: ...a considering a maximum drag load of 5 lbs For the GA 56 antennas at subsonic speed Install a doubler plate to reinforce thin skinned aircraft Observe guidelines for acceptable installation practices...

Страница 24: ...ION 4 Feed wires through the connector backshells before insertion into the 78 44 and 25 pin connectors 5 Contacts for the 78 44 and 25 pin connectors must be crimped onto the individual wires of the...

Страница 25: ...to change without notice 3 Alternate contacts for 18 AWG wire As an alternative to the Positronic contacts listed and provided in the installation kit the installer may use contacts made by ITT Cannon...

Страница 26: ...he left side of the rack viewing it from the cockpit and attaching it by replacing the two 4 40 screws 3 8 500 SERIES UNIT INSERTION AND REMOVAL It may be necessary to insert the hex drive tool into t...

Страница 27: ...ANNUNCIATE F Not implemented at time of publication 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 PO...

Страница 28: ...Out 53 TAWS AUDIO LO 54 GPS RS 232 OUT 4 Out 55 GPS RS 232 IN 4 In 56 GPS RS 232 OUT 1 Out 57 GPS RS 232 IN 1 In 58 GPS RS 232 OUT 2 Out 59 GPS RS 232 IN 2 In 60 ALTITUDE COMMON GROUND Out 61 ALTITUDE...

Страница 29: ...IO INHIBIT IN In 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 C...

Страница 30: ...ERVED 2 RESERVED 3 RESERVED 4 COM MIC KEY In 5 INTERCOM MIC HI In 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 1...

Страница 31: ...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 DME...

Страница 32: ...volt converter such as a KGS Electronics models RB 126 or UC 14 28 or equivalent must be used The voltage converter should include exactly one short circuit protection device on its output such as a...

Страница 33: ...01 62 In ALTITUDE C4 P5001 61 In ALTITUDE COMMON P5001 60 In These inputs are considered active if either the voltage to ground is 1 9 V or the resistance to ground is 375 These inputs are considered...

Страница 34: ...Indicator Electrical Characteristics 4 4 2 1 Deviation Pin Name Connector Pin I O MAIN LEFT P5001 21 Out MAIN RIGHT 2 5V COMMON P5001 22 Out MAIN UP P5001 27 Out MAIN DOWN 2 5V COMMON P5001 28 Out The...

Страница 35: ...N 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...

Страница 36: ...5 1 3 CDI SOURCE SELECT GNS 530 Only This CDU Source Select 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...

Страница 37: ...enever the TAWS functionality is inhibited either from the 500 Series unit or the external annunciator x The amber TERR N A annunciator is illuminated whenever the TAWS functionality is unavailable lo...

Страница 38: ...TIME MARK OUT is a logic level output capable of sourcing 1 mA at up greater than 3 8 V and sinking 1 mA at less than 0 4 V 4 5 3 Annunciators Switches Configuration None 4 5 4 Annunciators Switches C...

Страница 39: ...sition latitude and longitude and magnetic variation NOTE Aviation RS 232 data may be transmitted with or without the current GPS altitude in feet Refer to section 5 2 2 The 500 Series unit can receiv...

Страница 40: ...rack Distance 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...

Страница 41: ...y traffic information on the 500 Series unit 4 6 2 Serial Data Electrical Characteristics 4 6 2 1 RS 232 Pin Name Connector Pin I O GPS RS 232 OUT 1 P5001 56 Out GPS RS 232 IN 1 P5001 57 In GPS RS 232...

Страница 42: ...t Refer to section 5 3 2 for the serial data checkout Refer to sections 5 2 14 5 2 15 and 5 2 16 for the Stormscope checkout Refer to section 5 2 17 for the Skywatch checkout Refer to sections 5 2 17...

Страница 43: ...T INTERLOCK is active the GNS 530 COM receiver sensitivity is decreased This input is intended to reduce interference from other transmitters in the aircraft The TRANSMIT INTERLOCK input should be con...

Страница 44: ...COM 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 discrete inputs are considered ac...

Страница 45: ...y 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...

Страница 46: ...BS 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 Nam...

Страница 47: ...n the 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 M...

Страница 48: ...age current with respect to ground is less than 10 PA 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 ei...

Страница 49: ...tuning interconnect Refer to Figure F 30 on page F 61 for the King Serial Remote DME tuning interconnect Refer to Figure F 31 on page F 63 for the parallel 2 of 5 DME tuning interconnect Refer to Figu...

Страница 50: ...e RTC Avoidance Forward Looking Terrain Avoidance FLTA sub function Yes Yes No Imminent Terrain Impact Avoidance Forward Looking Terrain Avoidance FLTA sub function Yes Yes No Premature Descent Alert...

Страница 51: ...ies TAWS unit or via the external annunciator if installed TAWS AUDIO INHIBIT IN is used to inhibit TAWS audio This can be connected to inhibit output lines of another unit whose audio is higher in pr...

Страница 52: ...Page 4 26 500 SERIES INSTALLATION MANUAL Rev Q 190 00181 02 This page intentionally left blank...

Страница 53: ...ware version 6 01 All configuration pages shown apply to the GNS 530 but not all apply to the GPS 500 Those pages and fields that apply only to certain 500 Series units are denoted as such 5 2 1 MAIN...

Страница 54: ...n format Only high speed ARINC 429 should be used Garmin GTX 330 Garmin GAD 42 Selected course heading and true airspeed data from the Garmin GAD 42 Honeywell EFIS Selected course heading and joystick...

Страница 55: ...Graphics w Int ARINC 429 data as defined by the GAMA General Aviation Subset 2nd Edition including GAMA Graphics Protocol A The output data includes navigation and flight plan information including gr...

Страница 56: ...ion from the following units Shadin 91204XM Digital Fuel Management System Shadin 91053XM Digital Fuel Management System JP Instruments EDM 700 or EDM 760 Engine Monitor WX 500 Lightning strike inform...

Страница 57: ...ble the TAWS functionality The HW CONFIG field will display TERRAIN if the appropriate hardware is installed to enable the TERRAIN functionality If neither the TAWS nor TERRAIN hardware is installed t...

Страница 58: ...e and longitude of a joystick waypoint sent by an EFIS or RADAR indicator 5 2 5 INSTRUMENT PANEL SELF TEST Page Select the INSTRUMENT PANEL SELF TEST Page see Figure 5 6 This page allows verification...

Страница 59: ...splay brightness tracks the 500 Series unit s photocell using additional parameters PHOTO TRANS and PHOTO SLP OFFST described below RESP TIME Response Time Sets the speed with which the brightness res...

Страница 60: ...the 500 Series unit s photocell This field has a range of 0 zero 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 des...

Страница 61: ...and inactive as selected on this page INTEG The INTEG annunciator is active and inactive as selected on this page MSG The MSG annunciator is active and inactive as selected on this page OBS The OBS an...

Страница 62: ...he TO FROM flag is hidden TO The TO flag is in view SELECTED COURSE Select 150 on the CDI HSI that is connected to the 500 Series unit s MAIN OBS inputs The SELECTED COURSE field should indicate near...

Страница 63: ...ed on the EFIS or its control panel OBI SOURCE GNS 530 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 King KI...

Страница 64: ...ed The higher the SQ 250 number the more signal is required to break squelch SQ 833 Sets the squelch threshold for 8 33 kHz channel spacing operation May be set to any value between 0 zero and 63 The...

Страница 65: ...ect the format for DME tuning data Using the controls on the GNS 530 front panel make the selections below and verify the interfaces as appropriate NOTE The LAT VERT and SELECTED COURSE configurations...

Страница 66: ...ction Description King Serial King Serial DME tuning data not operational for MAIN software versions 2 02 and lower Parallel 2x5 2 of 5 parallel DME tuning Parallel BCD Shifted BCD Binary Coded Decima...

Страница 67: ...as reported by the WX 500 through RS 232 data Verify that the STATUS field indicates Ok and that the other displayed parameters are correct Verify that all the boxes in the lower portion of the page a...

Страница 68: ...ywatch this page shows 1 The altitude mode below BLW normal NORM above ABV or unrestricted UNR 2 The operating mode standby STBY or operating OPER 3 Current altitude ALT 4 Altitude limits being impose...

Страница 69: ...Series unit is configured for GAD 42 interface Select the GAD 42 CONFIG Page see Figure 5 22 This page allows remote configuration of a GAD 42 Interface Adapter Unit For details of this function plea...

Страница 70: ...ription Message When configured for this option each TAWS alert message is played by itself Default 5 2 21 4 VOLUME Field The VOLUME field sets the volume of the TAWS alerts from 0 volume left side to...

Страница 71: ...the TAWS AUDIO CONFIG Page 2 see Figure 5 25 This page allows configuration of TAWS audio 5 2 22 1 RTC CAUTION Field Selection Description Caution Terrain 2x Sets the Forward Looking Terrain Clearanc...

Страница 72: ...fied text Terrain Ahead 2x Sets the Forward Looking Terrain Clearance FLTA Imminent Terrain Impact ITI cautionary alert to the specified text Default 5 2 22 6 ITI WARNING Field Selection Description T...

Страница 73: ...ing the Instrument Panel Self test Page verify that the following parameters are displayed on equipment in the aircraft as listed below NOTE Electronic displays which monitor the 500 Series unit s ARI...

Страница 74: ...flags may be checked with either GPS or VOR ILS and vertical deviation and flags must be checked with Glideslope Verify that the flags are hidden at the correct times and that the flag is in view at...

Страница 75: ...in close proximity Press the squelch disable button to defeat the automatic squelch feature and listen for any unusual electrical noise which would increase the squelch threshold If possible verify th...

Страница 76: ...onditions x Evaluate the TAWS audio messages for acceptable volume and intelligibility during both low and high cockpit noise levels idle descent at low speed and high power at Vmo x Adjust the TAWS a...

Страница 77: ...re NOT illuminated If any TAWS annunciators are illuminated a fault exists x Verify that all four TAWS annunciators amber TERR white TERR INHB amber TERR N A red PULL UP shown on the external TAWS ann...

Страница 78: ...s are illuminated either on the 500 Series unit or on the external TAWS annunciator unit a fault exists 4 Select TER N A in the DISCRETE TOGGLE field on the MAIN DISCRETE I O page of the 500 Series un...

Страница 79: ...s shown in the terrain annunciator field lower left portion of the display 4 Go to the TERRAIN page and verify the text TERRAIN TEST is displayed in the middle of the TERRAIN page 5 Verify that the TE...

Страница 80: ...Page 5 28 500 SERIES INSTALLATION MANUAL Rev Q 190 00181 02 This page intentionally left blank...

Страница 81: ...his document identifies the Instructions for Continued Airworthiness for the modification of the above aircraft by installation of a Garmin 500 Series unit Applicability Applies to aircraft altered by...

Страница 82: ...additional overhaul time limitations 15 Airworthiness Limitation Section Refer to the 500 Series unit Sample Flight Manual Supplement 16 Revision To revise this ICA a letter must be submitted to the l...

Страница 83: ...tly from Garmin under the following part number GNC 500 Environmental Qualification Form Garmin part number 005 00096 64 To obtain a copy of this form see the dealer OEM portion of the Garmin web site...

Страница 84: ...Page A 4 500 SERIES INSTALLATION MANUAL Rev Q 190 00181 02 This page intentionally left blank...

Страница 85: ...s primary line of sight as should any indication requiring immediate aircrew action Other annunciations should be installed in the normal field of view e g a location in the center radio stack or oth...

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Страница 95: ...scription ETX ASCII end of text character 03 hex C 3 OUTPUT SENTENCE TYPE 1 The Type 1 output sentences shall have the following general format id item designator single ASCII alphabetic character ddd...

Страница 96: ...urrent 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 nau...

Страница 97: ...carriage return character 0D hex LF ASCII line feed character 0A hex Each waypoint in the route being navigated by the 500 Series unit shall have a Type 2 sentence output by the 500 Series unit appro...

Страница 98: ...r 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...

Страница 99: ...Altitude 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...

Страница 100: ...03 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 ra...

Страница 101: ...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...

Страница 102: ...ow 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 Si...

Страница 103: ...el used right tenths gallons SO4567 CR LF SO ASCII characters 4567 represents fuel flow left tenths gallons hour SP89012 CR LF SP ASCII characters 89012 represents fuel used left tenths gallons SQ345...

Страница 104: ...cator 0x2b or 0x2d ETX end transmit character 0x03 Note Checksum is calculated by adding each byte in the message including all characters from STX up to and including the error log reason indicator s...

Страница 105: ...n PS Engineering Audio Panel KMA 24 GMA 340 PMA 6000 KMA 24H 70 71 E 2 GARMIN 500 530 LRU INTERFACE Function Bendix King B D Air Data Computer KDC 281 2600 KDC 481 2601 2800 90004 003 Function Shadin...

Страница 106: ...75 AB LTN 91 HG 1095 AB LTN 92 Function Bendix King Garmin Century Collins Sperry S Tec Nav KI 202A GI 102 A NSD 360A 331A 6P RD 550A ST 180 Indicator KI 203 GI 106 A NSD 1000 331A 6G RD 650 KI 204 KI...

Страница 107: ...Figure F 9 GPS 500 Typical Installation Figure F 10 Power Lighting and Antennas Interconnect Figure F 11 Altimeter Interconnect Figure F 12 Main Indicator Interconnect Figure F 13 KI 209A Main Indicat...

Страница 108: ...1 02 Figure F 29 King Serial Panel DME Tuning Interconnect Figure F 30 King Serial Remote DME Tuning Interconnect Figure F 31 Parallel 2 OF 5 DME Tuning Interconnect Figure F 32 Parallel BCD Slip Code...

Страница 109: ...500 SERIES INSTALLATION MANUAL Page F 3 Page F 4 blank 190 00181 02 Rev Q Figure F 1 GA 56 Antenna Installation Drawing...

Страница 110: ...500 SERIES INSTALLATION MANUAL Page F 5 Page F 6 blank 190 00181 02 Rev Q Figure F 2 GNS 530 Mounting Rack Dimensions...

Страница 111: ...500 SERIES INSTALLATION MANUAL Page F 7 Page F 8 blank 190 00181 02 Rev Q Figure F 3 GPS 500 Mounting Rack Dimensions...

Страница 112: ...500 SERIES INSTALLATION MANUAL Page F 9 Page F 10 blank 190 00181 02 Rev Q Figure F 4 GNS 530 Mounting Rack Installation...

Страница 113: ...500 SERIES INSTALLATION MANUAL Page F 11 Page F 12 blank 190 00181 02 Rev Q Figure F 5 GPS 500 Mounting Rack Assembly...

Страница 114: ...500 SERIES INSTALLATION MANUAL Page F 13 Page F 14 blank 190 00181 02 Rev Q Figure F 6 500 Series Recommended Panel Cutout Dimensions...

Страница 115: ...500 SERIES INSTALLATION MANUAL Page F 15 Page F 16 blank 190 00181 02 Rev Q Figure F 7 500 Series System Interface Diagram...

Страница 116: ...500 SERIES INSTALLATION MANUAL Page F 17 Page F 18 blank 190 00181 02 Rev Q Figure F 8 GNS 530 A Typical Installation...

Страница 117: ...500 SERIES INSTALLATION MANUAL Page F 19 Page F 20 blank 190 00181 02 Rev Q Figure F 9 GPS 500 Typical Installation...

Страница 118: ...500 SERIES INSTALLATION MANUAL Page F 21 Page F 22 blank 190 00181 02 Rev Q Figure F 10 Power Lighting and Antennas Interconnect...

Страница 119: ...500 SERIES INSTALLATION MANUAL Page F 23 Page F 24 blank 190 00181 02 Rev Q Figure F 11 Altimeter Interconnect...

Страница 120: ...500 SERIES INSTALLATION MANUAL Page F 25 Page F 26 blank 190 00181 02 Rev Q Figure F 12 Main Indicator Interconnect...

Страница 121: ...500 SERIES INSTALLATION MANUAL Page F 27 Page F 28 blank 190 00181 02 Rev Q Figure F 13 KI 209A Main Indicator Interconnect...

Страница 122: ...500 SERIES INSTALLATION MANUAL Page F 29 Page F 30 blank 190 00181 02 Rev Q Figure F 14 KI 208A Main Indicator Interconnect...

Страница 123: ...500 SERIES INSTALLATION MANUAL Page F 31 Page F 32 blank 190 00181 02 Rev Q Figure F 15 Annunciators Switches Interconnect...

Страница 124: ...500 SERIES INSTALLATION MANUAL Page F 33 Page F 34 blank 190 00181 02 Rev Q Figure F 16 RS 232 Serial Data Interconnect...

Страница 125: ...500 SERIES INSTALLATION MANUAL Page F 35 Page F 36 blank 190 00181 02 Rev Q Figure F 17 ARINC 429 EFIS Interconnect...

Страница 126: ...500 SERIES INSTALLATION MANUAL Page F 37 Page F 38 blank 190 00181 02 Rev Q Figure F 18 ARINC 429 Sandel EHSI Interconnect 1 500 Series Unit 1 Sandel SN3308...

Страница 127: ...500 SERIES INSTALLATION MANUAL Page F 39 Page F 40 blank 190 00181 02 Rev Q Figure F 19 ARINC 429 Sandel EHSI Interconnect 2 GNS 530 1 Sandel SN3308...

Страница 128: ...500 SERIES INSTALLATION MANUAL Page F 41 Page F 42 blank 190 00181 02 Rev Q Figure F 20 ARINC 429 Sandel EHSI Interconnect 2 GNS 530 2 Sandel SN3308...

Страница 129: ...500 SERIES INSTALLATION MANUAL Page F 43 Page F 44 blank 190 00181 02 Rev Q Figure F 21 ARINC 429 RS 232 Air Data IRU AHRS Interconnect...

Страница 130: ...500 SERIES INSTALLATION MANUAL Page F 45 Page F 46 blank 190 00181 02 Rev Q Figure F 22 ARINC 429 Flight Control Interconnect...

Страница 131: ...500 SERIES INSTALLATION MANUAL Page F 47 Page F 48 blank 190 00181 02 Rev Q Figure F 23 Traffic Advisory System Interconnect...

Страница 132: ...500 SERIES INSTALLATION MANUAL Page F 49 Page F 50 blank 190 00181 02 Rev Q Figure F 24 GTX 330 Interconnect...

Страница 133: ...500 SERIES INSTALLATION MANUAL Page F 51 Page F 52 blank 190 00181 02 Rev Q Figure F 25 Weather and Terrain Interconnect...

Страница 134: ...500 SERIES INSTALLATION MANUAL Page F 53 Page F 54 blank 190 00181 02 Rev Q Figure F 26 Audio Panel Interconnect...

Страница 135: ...500 SERIES INSTALLATION MANUAL Page F 55 Page F 56 blank 190 00181 02 Rev Q Figure F 27 VOR ILS Indicator interconnect...

Страница 136: ...500 SERIES INSTALLATION MANUAL Page F 57 Page F 58 blank 190 00181 02 Rev Q Figure F 28 RMI OBI Interconnect...

Страница 137: ...500 SERIES INSTALLATION MANUAL Page F 59 Page F 60 blank 190 00181 02 Rev Q Figure F 29 King Serial Panel DME Tuning Interconnect...

Страница 138: ...500 SERIES INSTALLATION MANUAL Page F 61 Page F 62 blank 190 00181 02 Rev Q Figure F 30 King Serial Remote DME Tuning Interconnect...

Страница 139: ...500 SERIES INSTALLATION MANUAL Page F 63 Page F 64 blank 190 00181 02 Rev Q Figure F 31 Parallel 2 OF 5 DME Tuning Interconnect...

Страница 140: ...500 SERIES INSTALLATION MANUAL Page F 65 Page F 66 blank 190 00181 02 Rev Q Figure F 32 Parallel BCD Slip Code DME Tuning Interconnect...

Страница 141: ...500 SERIES INSTALLATION MANUAL Page F 67 Page F 68 blank 190 00181 02 Rev Q Figure F 33 TAWS Interconnect...

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