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500 SERIES INSTALLATION MANUAL

Page 5-7

190-00181-02

Rev

Q

SOURCE

Selection Description
PHOTO

Backlight level is determined by the ambient light level as measured
by the photocell on the 500 Series unit.

14V DC

Backlight level tracks a 14 volt DC aircraft lighting bus.

28V DC

Backlight level tracks a 28 volt DC aircraft lighting bus.

5V DC

Backlight level tracks a 5 volt DC aircraft lighting bus.

5V AC

Backlight level tracks a 5 volt AC aircraft lighting bus.

NOTE

If a lighting bus (any selection other than

PHOTO

) is selected, and the lighting bus

control is turned to its minimum (daytime) setting, the display 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 responds to the input level (bus voltage or ambient light) changes.
The higher the number the slower the display responds. This field has a range of 3 to 7, and is set to 4 at
the factory.

MIN -

(Minimum)

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

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Summary of Contents for GNS 530

Page 1: ...rnational 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 express permission of Garmin ...

Page 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 REVISIONS Revision Revision Date Description ECO A 2 10 00 Initial Release 12684 B 3 6 00 Add new installation accessory kits 12845 C 9 22 00 Add unit versions with 14 28 volt transmitter Update config...

Page 3: ...ation 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 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 i...

Page 4: ...EMOVAL 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 SWITCHES 4 10 4 6 SERIAL DATA 4 13 4 7 COM VOR ILS AUDIO GNS 530 ONLY 4 17 4 8 VOR ILS INDICATOR GNS 530 ONLY 4 19 4 9 RMI OBI 4 21 4 10 DME TUNING GNS 530 ONLY 4 22 4 11 TERRAIN AWARNESS AND WARNING...

Page 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 FIGURE F 8 GNS 530 A TYPICAL INSTALLATION F 17 FIGURE F 9 GPS 500 TYPICAL INSTALLATION F 19 FIGURE F 10 POWER LIGHTING AND ANTENNAS INTERCONNECT F 21 FIGURE F 11 ALTIMETER INTERCONNECT F 23 FIGURE F 12 ...

Page 6: ...armin 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 0101 2 16 01 Remote COM transfer 3 0111 7 9 01 Improves VLOC Morse code ident 4 0203 Rev B 8 12 02 Improve receiver audio compressor performance 5 0207 4 2 02 Remove excess solder from COM board 6 0...

Page 7: ...ludes 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 are TAWS or TERRAIN upgradeable GPS signals are received by Garmin s low profile GA 56 antenna P N 010 10040 0X CAUTION The 500 Series product lens is coated with a special anti reflective coating whi...

Page 8: ...18 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 Humidity 95 non condensing Altitude Range 1 500 ft to 50 000 ft Input Voltage Range GPS 500 011 00562 00 10 GNS 530 011 00550 10 30 11 to 33 Vdc Input Voltage Range GNS 530 011 00550 00 22 to 33 Vdc Input...

Page 9: ...s 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 than 6 dB when the RF level is 2 PV hard modulated 30 at 1000 Hz at rated audio Squelch 2 Pv r6 dB for 25 kHz channels 3 Pv r6 dB for 8 33 kHz channels Selectivity 6 dB BW is greater than r8 kHz for 25...

Page 10: ...e 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 of standard deflection AGC Characteristics From 99 dBm to 13 dBm input of a Standard VOR Audio Test Signal audio output levels shall not vary more than 3 dB Spurious Response Greater than 80 dB VOR ...

Page 11: ...aracteristics 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 the reference AGC voltage shall not vary more than 6 dB over the input signal frequency range of 9 kHz from the assigned channel frequency Skirt Bandwidth The input signal level required to produce ref...

Page 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 shall be 78 mV 7 8 mV b With a standard deflection FLY UP condition 150 Hz dominant the output shall be 78 mV 7 8 mV Flag The unit Flags a When the level of a standard deviation test signal produces 50 o...

Page 13: ...rature 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 certified for IFR enroute terminal and non precision approaches The 500 Series initial certification was accomplished via STC s by Garmin in a Piper PA32 See Appendix B for copies of the STC s The 500 ...

Page 14: ...R 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 SPECIFIC LEGAL RIGHTS WHICH MAY VARY FROM STATE TO STATE IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL SPECIAL INDIRECT OR CONSEQUENTIAL DAMAGES WHETHER RESULTING FROM THE USE MISUSE OR INABILIT...

Page 15: ...y 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 transmitter DME Transponder and Radar For rotorcraft locate the GA 56 Antenna as far as possible from the main rotor hub This reduces the percentage of time the blades block the antenna Also mount it as f...

Page 16: ...cate 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 a 1 57542 GHz notch filter is installed on the COM transceiver antenna output x Locate the 500 Series unit as far as possible from all COM antennas Figure 2 1 GPS Antenna Installation Considerations...

Page 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 forced air fan be installed of the indicated rating to cool this equipment Units tightly packed in the avionics stack heat each other through radiation convection and sometimes by direct conduction ...

Page 18: ...rproofness 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 Operating Frequency 1575 42 2 00 MHz LNA Gain 20 dB Maximum 12dB Minimum LNA Noise Figure 3 0 dB Maximum LNA Output VSWR 50 2 1 Maximum LNA Input power at 1 dB Gain Compression 6 dB Minimum LNA Bandwidt...

Page 19: ...010 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 14 or 28 V 2 10 W 3 1 2 GNS 530 TAWS Upgraded Originally non TAWS units that have been upgraded to include TAWS CATALOG P N UNIT P N GNS 530A ACCESSORIES 1 COLOR OPERATING VOLTAGE MINIMUM XMIT PWR 010...

Page 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 BLACK N 010 00291 10 011 00863 10 Y N GRAY Y 010 00291 11 011 00863 10 Y Y GRAY Y 3 1 4 GPS 500 TAWS Upgraded Originally non TAWS units that have been upgraded to include TAWS CATALOG P N UNIT P N A...

Page 21: ...SSEMBLY 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 00 P5050 CONNECTOR KIT 011 00558 00 GPS 500 PILOT S GUIDE 190 00181 60 GPS 500 QUICK REFERENCE GUIDE 190 00181 61 GPS 500 SAMPLE AIRPLANE FLIGHT MANUAL SUPPLEMENT 190 00181 64 GNS 530 PILOT S GUIDE 1...

Page 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 DC VERTICAL NO 013 00079 60 14V DC 14V DC VERTICAL YES 013 00079 61 14V DC 14V DC VERTICAL NO 013 00079 70 28V DC 5V DC VERTICAL YES 013 00079 71 28V DC 5V DC VERTICAL NO 3 4 INSTALLATION ACCESSORIE...

Page 23: ...na 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 as outlined in AC 43 13 2A 3 Seal the antenna and gasket to the fuselage using a good quality electrical grade sealant Use caution to insure that the antenna connector is not contaminated with sealan...

Page 24: ...TION 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 aircraft wiring harness The following tables list contact part numbers for reference and recommended crimp tools Table 3 1 Pin Contact Part Numbers 78 pin conn P5001 5050 44 pin conn P5006 25 pin con...

Page 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 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 ...

Page 26: ...the 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 the access hole and rotate the mechanism 90 counterclockwise to insure correct position prior to placing the unit in the rack The 500 Series unit is installed in the rack by sliding it straight in unt...

Page 27: ...3 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 POWER 1 In 20 AIRCRAFT POWER 1 In 21 MAIN LEFT Out 22 MAIN RIGHT 2 5V COMMON Out 23 MAIN LATERAL FLAG Out 24 MAIN LATERAL FLAG 2 5V COMMON Out 25 MAIN TO Out 26 MAIN FROM 2 5V COMMON Out 27 MAIN UP Out...

Page 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 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 AIRCR...

Page 29: ...DIO 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 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 RS232_OUT_5 Out 61 RS232_IN_5 ...

Page 30: ...SERVED 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 14 TRANSMIT INTERLOCK In 15 COM REMOTE TRANSFER In 16 SPARE 17 INTERCOM MIC LO In 18 COM MIC AUDIO LO In 19 500 COM AUDIO LO Out 20 RESERVED 21 AIRCRAFT GROUND 22 AIRCRAFT GROUND 23 RESERVED 24 RESERV...

Page 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 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 I...

Page 32: ...8 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 circuit breaker P5002 11 and P5002 12 supply power to the COM transmitter The other power input pins P5001 19 P5001 20 and P5006 44 accept 11 33 Vdc GNS 530 P N 011 00550 10 and 011 00550 30 accepts ...

Page 33: ...001 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 inactive if the voltage to ground is 11 33 Vdc NOTE Some transponders and other altitude encoding receivers do not have internal isolation diodes to prevent the unit from pulling the encoder lines to...

Page 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 Deviation output is capable of driving up to three 1000 meter loads with r150 mVdc r10 for full scale deflection The drive circuit provides for more than full scale deflection with a maximum course ...

Page 35: ...IN 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 4 3 Main Indicator Configuration Refer to...

Page 36: ...4 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 pin performs the same function as pressing the CDI key on the GNS 530 bezel 4 5 1 4 VLOC ANNUNCIATE GNS 530 Only This VLOC Annunciator output is driven when the unit is configured with a single CDI H...

Page 37: ...henever 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 loss of GPS signal system failure out of the area of coverage etc x All TAWS annunciators are illuminated simultaneously during a TAWS system test The TAWS TERR INHB discrete input may be used to toggl...

Page 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 Calibration and Checkout Refer to section 5 2 8 for the annunciators switches checkout 4 5 5 Annunciators Switches Interconnect Refer to Figure F 15 on page F 31 for the annunciators switches intercon...

Page 39: ...osition 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 receive pressure altitude air data and fuel data from certain systems on the GPS RS 232 IN 1 port The 500 Series unit can communicate with a Ryan TCAD 9900B system using the GPS RS 232 OUT 2 and GPS RS 232...

Page 40: ...25 Greenwich Mean Time BCD Ɣ Ɣ Ɣ Ɣ 147G Magnetic Variation Ɣ Ɣ Ɣ 251 Distance to Go Ɣ 251G Distance to Go Ɣ Ɣ Ɣ 252 Time to Go Ɣ Ɣ Ɣ Ɣ 260G Date BCD Ɣ Ɣ Ɣ 261G GPS Discrete Word 1 Ɣ Ɣ Ɣ 275G LRN Status Word Ɣ Ɣ Ɣ 300G Station Declination Type and Class Ɣ Ɣ Ɣ 303 Message Length Type Number Ɣ Ɣ Ɣ 304G Message Characters 1 3 Ɣ Ɣ Ɣ 305G Message Characters 4 6 Ɣ Ɣ Ɣ 306G NAV Waypoint Airport Latitude Ɣ...

Page 41: ... order to display 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 OUT 2 P5001 58 Out GPS RS 232 IN 2 P5001 59 In GPS RS 232 OUT 3 P5001 41 Out GPS RS 232 IN 3 P5001 42 In GPS RS 232 OUT 4 P5001 54 Out GPS RS 232 IN 4 P5001 55 In RS 232 OUT 5 P5050 6...

Page 42: ...ut 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 and 5 2 18 for the TCAD checkout 4 6 5 Serial Data Interconnect Refer to Figure F 16 on page F 33 for the RS 232 serial data interconnect Refer to Figure F 17 on page F 35 for the ARINC 429 Bendix Ki...

Page 43: ...IT 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 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 7 2 COM V...

Page 44: ...RCOM 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 active if either the voltage to ground is 1 9 V or the resistance to ground is 375 These inputs are considered inactive if the voltage to ground is 11 33 Vdc COM REMOTE TRANSFER and VLOC REMOTE TRANSFE...

Page 45: ...cy 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 Flag 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 outp...

Page 46: ...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 k load With a Standard Localizer Centering Test Signal ap...

Page 47: ...in 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 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 d...

Page 48: ...kage 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 either the voltage to ground is 1 9 V or the resistance to ground is 375 These inputs are considered inactive if the voltage to ground is 11 33 Vdc 4 10 2 2 King Serial DME Tuning Pin Name Connector Pi...

Page 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 Figure F 32 on page F 65 for the parallel BCD Slip Code DME tuning interconnect NOTE For the GNS 530 to tune a Narco DME 890 or IDME 891 or an ARC Cessna RTA 476A using parallel 2 of 5 unique wiring and ...

Page 50: ...ce 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 PDA Yes Yes No Excessive Rates of Descent Alert Ground Proximity Warning System GPWS Alerting sub function Yes No No Negative Climb Rate Altitude Loss After Takeoff Ground Proximity Warning System GP...

Page 51: ...ries 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 priority TAWS AUDIO ACTIVE OUT allows the TAWS system to announce that it is playing audio This can be connected to the audio inhibit in lines of other units whose audio is of less priority than TAWS 4...

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

Page 53: ...tware 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 ARINC 429 CONFIG Page Select the MAIN ARINC 429 CONFIG Page see Figure 5 1 This page configures the GPS ARINC 429 output port and the two GPS ARINC 429 input ports The two input ports can each be con...

Page 54: ...on 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 waypoint information from the following EFIS systems Honeywell Primus 1000 INS IRU Heading information from the following Inertial systems Bendix King KAH 460 Collins AHC 85 Honeywell Laseref Litef ...

Page 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 graphical representation of flight plan procedures GAMA 429 Pro Line 21 ARINC 429 data as defined by the GAMA General Aviation Subset 2nd Edition The output data includes navigation and flight plan inf...

Page 56: ...tion 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 information from a BF Goodrich WX 500 Stormscope CHANNEL OUTPUTS Selection Description Off No unit s connected to output of this channel Aviation Serial position altitude velocity and navigation data to th...

Page 57: ...able 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 ...

Page 58: ...de 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 that the 500 Series unit is communicating properly with other instruments Compare on screen indications with the information depicted on connected instruments such as the CDI HSI RMI and or external ...

Page 59: ...isplay 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 responds to the input level bus voltage or ambient light changes The higher the number the slower the display responds This field has a range of 3 to 7 and is set to 4 at the factory MIN Minimum Sets th...

Page 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 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 rang...

Page 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 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 s...

Page 62: ...The 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 to 150 and a Calibrate to 150 field appears Selecting this field calibrates the 500 Series unit to match the input source Verify OBS operation by checking that the course displayed on the 500 Series ...

Page 63: ...hed 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 229 or KNI 582 RMI pointer independently from the GNS 530 CDI button Track CDI The MAIN King Serial OBI outputs are GPS or VOR and switchable by the GNS 530 CDI button This is useful if it is desired...

Page 64: ...sed The higher the SQ 250 number the more signal is required to break squelch SQ 833 Sets the squelch threshold for 8 33 kHz channel spacing operation May be set to any value between 0 zero and 63 The higher the number the more signal is required to break squelch SIDETN Sets the sidetone audio output level May be set to any value between 0 zero and 63 NOTE The sidetone audio output level is indepe...

Page 65: ...lect 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 only apply to installations where a CDI HSI is connected to the VOR LOC GLIDESLOPE pins on connector P5006 CDI LAT VERT Selection Verify That Max left up The CDI is pegged to the left up Full left u...

Page 66: ...ection 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 Decimal parallel DME tuning not operational for MAIN software versions 2 02 and lower Parallel slip Slip code parallel DME tuning not operational for MAIN software versions 2 02 and lower Narco 890 891 2 o...

Page 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 are green When a 500 Series unit is used with a WX 500 Stormscope the Synchro or Serial heading formats may be used If another heading format is used lightning strike information is visible on the Wea...

Page 68: ...kywatch 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 imposed LIM A and LIM B 5 Heading and barometric BARO and radio RAD altitude status For BFG Skywatch see Figure 5 19 verify that the 500 Series unit can change the Skywatch operating mode STBY or OPER In s...

Page 69: ...0 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 please refer to Section 5 of the GAD 42 Installation Manual P N 190 00159 00 5 2 20 MONITORING THE DATA LINK The Data Link is monitored on the Data Link Page There are four main page groups in the 500 Se...

Page 70: ...cription 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 100 volume right side The default value is 60 of the maximum value The TAWS volume needs to be set so as to ensure that aural alerts are audible under all anticipated noise environmental conditions ...

Page 71: ...t 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 Clearance FTLA Reduced Required Terrain Clearance RTC cautionary alert to the specified text Default Terrain Ahead 2x Sets the Forward Looking Terrain Clearance FTLA Reduced Required Terrain Clearance RTC ca...

Page 72: ...ified 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 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 73: ... 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 ARINC 429 output may vary in how and where annunciations are displayed Generally it is not required to verify every data field with an ARINC 429 interface Correct display of a subset of the data without not...

Page 74: ...d 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 the correct times 5 3 4 2 EHSI Deviation Scaling Only if HSI CDI is driven by the 500 Series unit via serial data With the 500 Series unit locked onto a GPS fix activate an OBS waypoint about 20 naut...

Page 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 the communications capability on both the high and low ends of the VHF COM band It may be required by the governing regulatory agency to verify operation of the COM transmitter and receiver at the exte...

Page 76: ...conditions 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 audio volume by moving the cursor to the VOLUME field and rotating small right knob Turn the knob to the right to increase the volume and to the left to decrease the volume 5 3 11 TAWS System Check Fo...

Page 77: ...are 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 annunciator are NOT illuminated If any external TAWS annunciators are illuminated a fault exists 2 Select TER CAUT in the DISCRETE TOGGLE field on the MAIN DISCRETE I O page of the 500 Series unit x Ver...

Page 78: ...rs 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 unit x Verify that when the TER N A discrete toggle is selected on the 500 Series unit the TER N A box is filled in on the 500 Series unit and the amber TERR N A lamp is illuminated on the external TAW...

Page 79: ...is 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 TER TEST terrain annunciator message is removed and x If a 3d GPS signal is present verify the terrain annunciator message is replaced with a black empty square and a red yellow terrain map is displaye...

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

Page 81: ...This 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 installation of the Garmin 500 Series unit Definitions and Abbreviations None N A Precautions None N A Units of Measurement None N A Referenced Publications Garmin 500 Series Installation Manual P N...

Page 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 local FSDO with a copy of the revised FAA Form 337 and revised ICA The FAA inspector accepts the change by signing Block 3 and including the following statement The attached revised new Instructions f...

Page 83: ...ctly 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 www garmin com A 3 GA 56 Environmental Qualification Form It is the responsibility of the installing agency to obtain the latest revision of the GA 56 Environmental Qualification Form This form is a...

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

Page 85: ...t 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 other location on the pilot s panel within the field of view at a height suitable for normal viewing from the pilot s seated position This includes loss of integrity monitoring RAIM waypoint sequencing ...

Page 86: ...Page B 2 500 SERIES INSTALLATION MANUAL Rev Q 190 00181 02 ...

Page 87: ...500 SERIES INSTALLATION MANUAL Page B 3 190 00181 02 Rev Q ...

Page 88: ...Page B 4 500 SERIES INSTALLATION MANUAL Rev Q 190 00181 02 ...

Page 89: ...500 SERIES INSTALLATION MANUAL Page B 5 190 00181 02 Rev Q ...

Page 90: ...Page B 6 500 SERIES INSTALLATION MANUAL Rev Q 190 00181 02 ...

Page 91: ...500 SERIES INSTALLATION MANUAL Page B 7 190 00181 02 Rev Q ...

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Page 93: ...500 SERIES INSTALLATION MANUAL Page B 9 190 00181 02 Rev Q ...

Page 94: ...Page B 10 500 SERIES INSTALLATION MANUAL Rev Q 190 00181 02 ...

Page 95: ...escription 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 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 shall be output by the 500 Series unit approximately ...

Page 96: ...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 97: ...I 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 approximately once every second If no route is being navigated by the 500 Series unit i e the active route is empty the following Type 2 sentence is output approximately once every second id item designat...

Page 98: ...er 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 s x x x x x x...

Page 99: ...n 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 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 D 3 ICARUS A...

Page 100: ...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 ranging from 0 0x30 0x30 0x30 to 255 0x32 0x35 0x35 D 5 ARNAV EI FUEL FLOW SENTENCE The Garmin 500 Series units shall be capable of receiving the following 13 byte message from the ARNAV or Electronics...

Page 101: ...n 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 cha...

Page 102: ...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 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 103: ...uel 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 CR LF SQ ASCII characters 345 represents error log reason indicator SR67890 CR LF SR ASCII characters 67890 represents fuel remaining tenths gallons SS123 CR LF SS ASCII character 123 represents grou...

Page 104: ...icator 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 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 ...

Page 105: ...in 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 Icarus Instruments ARNAV JP Instrument s Shadin Miniflo L Altitude Serializer or 8800T 3000 FC 10 EDM 700 91204XT 38 D Fuel Air Data 9000T FT 10 9200T Function Shadin Digiflo L Shadin Digidata Shadin...

Page 106: ...075 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 206 KI 208 A KI 209 A KI 525A KPI 522 B KPI 553 A B Function Bendix King BF Goodrich Ryan Garmin Weather Traffic KTA 870 SKY497 Skywatch 9900B BX GTX 330 and Terrain KMH 880 SKY899 Skywatch HP WX 50...

Page 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 Indicator Interconnect Figure F 14 KI 208A Main Indicator Interconnect Figure F 15 Annunciators Switches Interconnect Figure F 16 RS 232 Serial Data Interconnect Figure F 17 ARINC 429 EFIS Interconnect Figu...

Page 108: ...81 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 DME Tuning Interconnect Figure F 33 TAWS Interconnect ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

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

Page 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 ...

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

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

Page 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 ...

Page 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 ...

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

Page 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 ...

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

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

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

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

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

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

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

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

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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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