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500 SERIES INSTALLATION MANUAL

Page 1-1

P/N 190-00181-02

Page Rev. B

1. GENERAL DESCRIPTION

1.1 INTRODUCTION

This manual describes the physical, mechanical, and electrical characteristics and the installation
requirements for the 500 Series (GPS 500, GNC 520, and GNS 530) Panel-mounted units. After
installation of the 500 Series system, FAA Form 337 must be completed by an appropriately certificated
agency to return the aircraft to service.

1.2 EQUIPMENT DESCRIPTION

The 500 Series units are mark width (6.25” wide) units, and 4.60” high. The display is a 320 by 234 pixel
color LCD. The units include two removable data cards, one with a Jeppesen database, and the second
being an optional custom data card.

The GPS 500 is a GPS receiver certifiable for IFR en route, terminal, and non-precision approach
operations.

The GNC 520 includes all the features of the GPS 500, and also includes an IFR certified airborne VHF
communications transceiver.

The GNS 530 includes all the features of the GNC 520, and also includes IFR certified airborne
VOR/Localizer and Glideslope receivers.

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 which is very sensitive to skin
oils, waxes and abrasive cleaners. It is very important to clean the lens using an eyeglass lens cleaner which
is specified as safe for anti-reflective coatings (one suitable product is Wal-Mart

®

Lens Cleaner) and a

clean, lint-free cloth.

1.3 TECHNICAL SPECIFICATIONS

The conditions and tests required for TSO approval of the 500 Series are minimum performance standards.
It is the responsibility of those desiring to install this article either on or within a specific type or class of
aircraft to determine that the aircraft installation conditions are within the TSO standards. The article may
be installed only if further evaluation by the applicant documents an acceptable installation and is approved
by the administrator. For TSO Compliance, see Appendix A.

1.3.1 Physical Characteristics

Width

Front Bezel: 6.25 inches, Rack: 6.32 inches

Height

Front Bezel: 4.58 inches, Rack: 4.60 inches

Depth Behind Panel

11.00 inches (including connectors)

GPS 500 Weight

5.5 lbs. (unit); 1.35 lbs. (rack w/connectors)

GNC 520 Weight

6.2 lbs. (unit); 1.55 lbs. (rack w/connectors)

GNS 530 Weight

6.8 lbs. (unit); 1.65 lbs. (rack w/connectors)

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Содержание GPSMAP 500 Series

Страница 1: ... GNS 530 Shown GARMIN International Inc 1200 E 151st Street Olathe KS 66062 USA 190 00181 02 Revision B March 2000 6 5 6 167 7 21 0 18 36 1 DQG 16 ...

Страница 2: ...IN International Inc 1200 E 151 st Street Olathe KS 66062 USA Telephone 913 397 8200 Dealer Line 1 800 800 1420 Web Site Address www garmin com RECORD OF REVISIONS Revision Revision Date Description ECO Insertion Date By A 2 10 00 Initial Release 12684 B 3 6 00 Add new installation accessory kits 12845 LIST OF EFFECTIVE PAGES Page Revision A B i B ii B 1 1 B 1 2 B 1 3 B 1 4 B 1 5 B 1 6 B 2 1 B 2 2...

Страница 3: ...NA INSTALLATION DRAWING 3 7 3 11 MOUNTING RACK DIMENSIONS 3 9 3 12 MOUNTING RACK INSTALLATION 3 15 4 SYSTEM INTERCONNECTS 4 1 PIN FUNCTION LIST 4 1 4 2 POWER LIGHTING AND ANTENNAS 4 5 4 3 ALTIMETER 4 6 4 4 MAIN INDICATOR 4 7 4 5 ANNUNCIATORS SWITCHES 4 9 4 6 SERIAL DATA 4 11 4 7 COM VOR ILS AUDIO GNC 520 AND GNS 530 ONLY 4 14 4 8 VOR ILS INDICATOR GNS 530 ONLY 4 16 4 9 RMI OBI 4 18 4 10 DME TUNING...

Страница 4: ...HSI INTERCONNECT 2 GNS 530 1 SANDEL SN3308 4 47 FIGURE 4 15 ARINC 429 SANDEL EHSI INTERCONNECT 2 GNS 530 2 SANDEL SN3308 4 49 FIGURE 4 16 ARINC 429 AIR DATA IRU AHRS INTERCONNECT 4 51 FIGURE 4 17 ARINC 429 FLIGHT CONTROL INTERCONNECT 4 53 FIGURE 4 18 WEATHER AND TRAFFIC INTERCONNECT 4 55 FIGURE 4 19 AUDIO PANEL INTERCONNECT 4 57 FIGURE 4 20 VOR ILS INDICATOR INTERCONNECT 4 59 FIGURE 4 21 RMI OBI I...

Страница 5: ...eceived 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 which is very sensitive to skin oils waxes and abrasive cleaners It is very important to clean the lens using an eyeglass lens cleaner which is specified as safe for anti reflective coatings one suitable product is Wal Mart Lens Cleaner and a clean lin...

Страница 6: ...0 mA 27 5 VDC not transmitting 3 0 A 27 5 VDC transmitting Superflag Power Requirements 500 mA max per superflag output 27 5 VDC 1 0 A max 27 5 VDC on P5001 Main Superflags 1 0 A max 27 5 VDC on P5006 VOR LOC G S Superflags Software RTCA DO 178B level C Environmental Testing RTCA DO 160C For more details see Environmental Qualification Forms 1 3 3 GPS Specifications Regulatory Compliance TSO C129a...

Страница 7: ...lch 2 µv 6 dB for 25 kHz channels 3 µv 6 dB for 8 33 kHz channels Selectivity 6 dB BW is greater than 8 kHz for 25 kHz channeling 60 dB BW is less than 25 kHz for 25 kHz channeling 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 Transmitter Duty Cycle Recommende...

Страница 8: ...e 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 OBS Bearing Accuracy The bearing information as presented to the pilot shall not have an error in excess of 2 7 as specified by RT...

Страница 9: ...ncy at 36 kHz from the assigned channel frequency Spurious Response Greater than 80 dB Centering Accuracy Typical 0 3 mV Max error 9 9 mV per RTCA DO 195 Audio Output A minimum 100 mW into a 500 Ω load Audio Response Less than 6 dB of Variation between 350 and 2500 Hz Except the 1020 Hz Ident Tone will be at least 20 dB down in voice mode Audio Distortion The distortion in the receiver audio outpu...

Страница 10: ... was accomplished via STC s by GARMIN in a Piper PA32 See Appendix B for copies of the STC s 1 6 LIMITED WARRANTY GARMIN Corporation warrants this product to be free from defects in materials and manufacture for one year from the date of purchase GARMIN will at its sole option repair or replace any components that fail in normal use Such repairs or replacement will be made at no charge to the cust...

Страница 11: ... 500 Series and its GPS antenna 2 2 3 VOR LOC ANTENNA LOCATION The GNS 530 VOR LOC antenna should be well removed from all projections engines and propellers It should have a clear line of sight if possible The antenna must be mounted along the centerline of the aircraft minimizing the lateral offset 2 2 4 GLIDESLOPE ANTENNA LOCATION The GNS 530 Glideslope antenna should be well removed from all p...

Страница 12: ...r the GNC 520 and GNS 530 transmitters If a COM is found to be radiating the following can be done 1 Replace or clean VHF COM rack connector to ensure good coax ground 2 Place a grounding brace between the 500 Series unit VHF COM and ground 3 Shield the VHF COM wiring harness 2 2 8 COM VOR LOC and Glideslope Antenna Installation Instructions Install the COM VOR LOC and Glideslope antennas accordin...

Страница 13: ...AIR The 500 Series units meet all TSO requirements without external cooling However external cooling is strongly recommended Recommended airflow rating is 1 CFM cubic foot per minute at a pressure equivalent to 0 1 inches of water Location of the 500 Series unit in a stack of other power dissipating equipment can produce unacceptably high ambient air temperatures around the unit Temperatures above...

Страница 14: ...Waterproofness 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 Ω 2 1 Maximum LNA Input power at 1 dB Gain Compression 6 dB Minimum LNA Ba...

Страница 15: ...K00 00060 00 010 00182 01 The following installation accessories are available 1 GPS Antenna Options GA 56 Antenna Kit without cable Mod 1 or later GARMIN P N 010 10040 01 This kit contains the following items ITEM GARMIN P N QTY GA 56 ANTENNA SUB ASSEMBLY 011 00134 00 1 BACKING PLATE 115 00031 00 1 NUT SELF LOCKING 8 32 210 10004 09 4 ANTENNA GASKET 253 00002 00 1 GA 56 Flange Mount Antenna Kit M...

Страница 16: ...re is required for installation of the mounting rack but is not provided 6 32 Flat Head Screw 6 ea 6 32 Self locking Nut 6 ea 3 2 DATA BASE OPTIONS ITEM GARMIN P N DATA CARD WORLD WIDE 010 10201 00 DATA CARD AMERICAS 010 10201 01 DATA CARD INTERNATIONAL 010 10201 02 3 3 MISCELLANEOUS OPTIONS ITEM GARMIN P N CONNECTOR BNC MALE CLAMP 330 00087 00 LOW LOSS AVIATION ANTENNA EXTENSION CABLE WITH RIGHT ...

Страница 17: ...of this section applies to the GPS antenna The GA 56 antenna outline and footprint dimensions are shown in Figure 3 2 page 3 5 1 Using the backing plate as a template mark the location of the mounting holes and the through hole for coaxial cable Drill or punch the holes 2 The antenna installation must provide adequate support for the antenna considering a maximum drag load of 5 lbs For the GA 56 a...

Страница 18: ...late CAUTION 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 5008 44 pin conn P5006 25...

Страница 19: ...o P N 616245 or ITT Cannon P N 980 0005 722 4 For the card edge connector pin contacts use AMP part number 90272 1 or equivalent crimping tool 3 7 RACK INSTALLATION 1 The back plate of the rack may optionally be removed for ease of mounting in the aircraft panel To do so remove the two 4 40 screws tilt the back plate away from the tray and then slide the back plate to the side 2 Figure 3 3 page 3 ...

Страница 20: ... until the unit is firmly seated in the rack To remove the unit from the rack insert the hex drive tool into the access hole on the unit face and rotate counterclockwise until the unit is forced out about 3 8 and can be freely pulled from the rack Be sure not to over tighten the unit into the rack The application of hex drive tool torque exceeding 15 in lbs can damage the locking mechanism 3 9 COM...

Страница 21: ...500 SERIES INSTALLATION MANUAL Page 3 7 Page 3 8 blank P N 190 00181 02 Page Rev B 3 10 GA 56 Antenna Installation Drawing Figure 3 2 GA 56 Antenna Installation Drawing ...

Страница 22: ...500 SERIES INSTALLATION MANUAL Page 3 9 Page 3 10 blank P N 190 00181 02 Page Rev B 3 11 Mounting Rack Dimensions Figure 3 3 GNS 530 Mounting Rack Dimensions ...

Страница 23: ...500 SERIES INSTALLATION MANUAL Page 3 11 Page 3 12 blank P N 190 00181 02 Page Rev B Not available at time of release Figure 3 4 GNC 520 Mounting Rack Dimensions ...

Страница 24: ...500 SERIES INSTALLATION MANUAL Page 3 13 Page 3 14 blank P N 190 00181 02 Page Rev B Not available at time of release Figure 3 5 GPS 500 Mounting Rack Dimensions ...

Страница 25: ...500 SERIES INSTALLATION MANUAL Page 3 15 Page 3 16 blank P N 190 00181 02 Page Rev B 3 12 Mounting Rack Installation Figure 3 6 GNS 530 Mounting Rack Installation ...

Страница 26: ...500 SERIES INSTALLATION MANUAL Page 3 17 Page 3 18 blank P N 190 00181 02 Page Rev B Not available at time of release Figure 3 7 GNC 520 Mounting Rack Installation ...

Страница 27: ...500 SERIES INSTALLATION MANUAL Page 3 19 Page 3 20 blank P N 190 00181 02 Page Rev B Not available at time of release Figure 3 8 GPS 500 Mounting Rack Installation ...

Страница 28: ... INTEGRITY ANNUNCIATE Out 10 ANNUNCIATE D Out 11 ANNUNCIATE E Out 12 ALTITUDE ALARM ANNUNCIATE Not implemented at time of publication Out 13 ANNUNCIATE F Not implemented at time of publication Out 14 ILS GPS APPROACH Out 15 RESERVED 16 TIME MARK OUT Out 17 MAIN LATERAL SUPERFLAG Out 18 MAIN VERTICAL SUPERFLAG Out 19 AIRCRAFT POWER In 20 AIRCRAFT POWER In 21 MAIN LEFT Out 22 MAIN RIGHT 2 5V COMMON ...

Страница 29: ...ARINC 429 OUT B Out 48 GPS ARINC 429 IN 1 A In 49 GPS ARINC 429 IN 1 B In 50 GPS ARINC 429 IN 2 A In 51 GPS ARINC 429 IN 2 B In 52 RESERVED 53 RESERVED 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 ALTIT...

Страница 30: ...T 6 Not implemented at time of publication Out 63 GPS RS 232 IN 6 Not implemented at time of publication In 64 78 SPARES 4 1 3 P5002 GNC 520 and GNS 530 Only View of J5002 connector from back of unit 13 12 11 10 9 8 7 6 5 4 3 2 1 25 24 23 22 21 20 19 18 17 16 15 14 Pin Pin Name I O 1 RESERVED 2 RESERVED 3 RESERVED 4 COM MIC KEY In 5 INTERCOM MIC HI In 6 COM MIC AUDIO HI In 7 500Ω COM AUDIO HI Out ...

Страница 31: ... In 14 PARALLEL DME 8MHZ Out 15 VOR LOC SUPERFLAG Out 16 500Ω VOR ILS AUDIO HI Out 17 500Ω VOR ILS AUDIO LO Out 18 SERIAL DME CLOCK Out 19 SERIAL DME DATA Out 20 SER DME CHAN REQ PAR DME 4MHZ I O 21 SER DME RNAV MODE PAR DME 2MHZ I O 22 DME COMMON In 23 VOR ILS ARINC 429 OUT B Out 24 VOR ILS ARINC 429 OUT A Out 25 VOR OBI CLOCK Out 26 VOR OBI SYNC Out 27 VOR OBI DATA Out 28 VLOC REMOTE TRANSFER In...

Страница 32: ...s power to the COM transmitter The other power input pins P5001 19 P5001 20 and P5006 44 will accept 11 33 VDC A power connection on P5006 44 is only required if NAV SUPERFLAG and or G S SUPERFLAG is utilized 4 2 2 2 Lighting Buss Pin Name Connector Pin I O LIGHTING BUSS HI P5001 39 In LIGHTING BUSS LO P5001 40 In The 500 Series unit can be configured to track 28 VDC 14 VDC 5 VDC or 5 VAC lighting...

Страница 33: ...hese inputs are considered inactive if either the voltage to ground is 18 5 V or the resistance to ground is 100 kΩ NOTE Some transponders and other altitude encoder receivers do not have internal isolation diodes to prevent the unit from pulling the encoder lines to ground when the unit is off These units will require a diode to be added to the installation harness for each encoder line The anode...

Страница 34: ...4 4 2 Main 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 Ω meter loads with 150 mVDC 10 for full scale deflection The drive circuit provides for more than full scale deflection with a maxim...

Страница 35: ...S 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 sect...

Страница 36: ...tor flashes 4 5 1 3 CDI SOURCE SELECT GNS 530 Only This discrete input may be used to toggle between display of GPS and VOR LOC Glideslope information on the MAIN external CDI HSI A momentary low on this pin performs the same function as pressing the CDI key on the GNS 530 bezel 4 5 1 4 VLOC ANNUNCIATE GNS 530 Only This annunciator output is driven when the unit is configured with a single CDI HSI...

Страница 37: ...P5001 1 Out GPS ANNUNCIATE P5001 2 Out WAYPOINT ANNUNCIATE P5001 3 Out TERMINAL ANNUNCIATE P5001 4 Out APPROACH ANNUNCIATE P5001 5 Out MESSAGE ANNUNCIATE P5001 6 Out OBS ANNUNCIATE P5001 7 Out INTEGRITY ANNUNCIATE P5001 9 Out ILS GPS APPROACH P5001 14 Out All outputs sink up to 500 mA when activated 4 5 2 2 Switch Inputs Pin Name Connector Pin I O OBS MODE SELECT P5001 71 In CDI SOURCE SELECT P500...

Страница 38: ...an 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 IN 2 lines to display traffic information on the 500 Series unit If two 400 or 500 Series units are installed in an aircraft the GPS RS 232 OUT 3 and GPS RS 232 IN 3 lines may be cross connec...

Страница 39: ... Longitude 312 Ground Speed 313 Track Angle True 314 True Heading 315 Wind Speed 316 Wind Angle True 320 Magnetic Heading 321 Drift Angle 326G Lateral Scale Factor 330 Conic Arc Inbound Course 331 Conic Arc Radius 332 Conic Arc Course Change Angle 333 Airport Runway Azimuth 334 Airport Runway Length in Feet 335 Left Right Hand Holding Pattern Azimuth 340 Left Right Hand Procedure Turn Azimuth 351G...

Страница 40: ...R ILS ARINC 429 OUT B P5006 23 Out VOR ILS ARINC 429 IN A P5006 36 In VOR ILS ARINC 429 IN B P5006 35 In The GPS and VOR ILS ARINC 429 outputs conform to ARINC 429 electrical specifications when loaded with up to 5 standard ARINC 429 receivers 4 6 3 Serial Data Configuration Refer to section 5 2 1 for the main GPS ARINC 429 configuration Refer to sections 5 2 13 5 2 14 and 5 2 15 for the Stormscop...

Страница 41: ...ts these connections must include diode isolation or multiple radios will transmit simultaneously 4 7 2 COM VOR ILS Audio Electrical Characteristics 4 7 2 1 COM MIC KEY Pin Name Connector Pin I O COM MIC KEY P5002 4 In This input is considered active if either the voltage to ground is 1 9 V or the resistance to ground is 375 Ω This input is considered inactive if either the voltage to ground is 18...

Страница 42: ... audio 4 7 2 4 DISCRETE INPUTS Pin Name Connector Pin I O TRANSMIT INTERLOCK P5002 14 In COM REMOTE TRANSFER P5002 15 In VLOC REMOTE TRANSFER P5006 28 In These inputs are considered active if either the voltage to ground is 1 9 V or the resistance to ground is 375 Ω These inputs are considered inactive if either the voltage to ground is 18 5 V or the resistance to ground is 100 kΩ COM REMOTE TRANS...

Страница 43: ... VLOC frequency is channeled to a localizer channel 4 8 2 VOR ILS Indicator Electrical Characteristics 4 8 2 1 Superflags Pin Name Connector Pin I O VOR LOC SUPERFLAG P5006 15 Out GLIDESLOPE SUPERFLAG P5006 38 Out The output supplies not less than 500 mA on a 28 volt system and 250 mA on a 14 volt system with the output voltage not less than AIRCRAFT POWER 3 VDC when the flag is to be OUT OF VIEW ...

Страница 44: ...R 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 will be 0 5 0 1 VRMS into a 10 kΩ load With a Standard Localizer Centering Test S...

Страница 45: ...t in the data stream set to indicate that a localizer frequency is tuned which will stow 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 ou...

Страница 46: ... less than 10 µA NAV DME COMMON must be pulled low to indicate to the NAV module that it is the device channeling the DME NAV DME COMMON is considered active if either the voltage to ground is 1 9 V or the resistance to ground is 375 Ω These inputs are considered inactive if either the voltage to ground is 18 5 V or the resistance to ground is 100 kΩ 4 10 2 2 King Serial DME Tuning Pin Name Connec...

Страница 47: ...g Serial Panel DME tuning interconnect Refer to Figure 4 23 on page 4 67 for the King Serial Remote DME tuning interconnect Refer to Figure 4 24 on page 4 69 for the parallel 2 of 5 DME tuning interconnect Refer to Figure 4 25 on page 4 71 for the parallel BCD Slip Code DME tuning interconnect NOTE For the GNS 530 to tune a Narco DME 890 or IDME 891 using parallel 2 of 5 unique wiring and configur...

Страница 48: ...00 SERIES INSTALLATION MANUAL Page 4 21 Page 4 22 blank P N 190 00181 02 Page Rev B 4 11 500 SERIES INTERCONNECTS 4 11 1 500 Series System Interface Diagram Figure 4 1 500 Series System Interface Diagram ...

Страница 49: ...500 SERIES INSTALLATION MANUAL Page 4 23 Page 4 24 blank P N 190 00181 02 Page Rev B 4 11 2 500 Series Typical Installations Figure 4 2 GNS 530 Typical Installation ...

Страница 50: ...500 SERIES INSTALLATION MANUAL Page 4 25 Page 4 26 blank P N 190 00181 02 Page Rev B Figure 4 3 GNC 520 Typical Installation ...

Страница 51: ...500 SERIES INSTALLATION MANUAL Page 4 27 Page 4 28 blank P N 190 00181 02 Page Rev B Figure 4 4 GPS 500 Typical Installation ...

Страница 52: ...500 SERIES INSTALLATION MANUAL Page 4 29 Page 4 30 blank P N 190 00181 02 Page Rev B 4 11 3 Power Lighting and Antennas Interconnect Figure 4 5 Power Lighting and Antennas Interconnect ...

Страница 53: ...500 SERIES INSTALLATION MANUAL Page 4 31 Page 4 32 blank P N 190 00181 02 Page Rev B 4 11 4 Altimeter Interconnect Figure 4 6 Altimeter Interconnect ...

Страница 54: ...500 SERIES INSTALLATION MANUAL Page 4 33 Page 4 34 blank P N 190 00181 02 Page Rev B 4 11 5 Main Indicator Interconnect Figure 4 7 Main Indicator Interconnect ...

Страница 55: ...500 SERIES INSTALLATION MANUAL Page 4 35 Page 4 36 blank P N 190 00181 02 Page Rev B 4 11 6 KI 209A Main Indicator Interconnect Figure 4 8 KI 209A Main Indicator Interconnect ...

Страница 56: ...500 SERIES INSTALLATION MANUAL Page 4 37 Page 4 38 blank P N 190 00181 02 Page Rev B 4 11 7 KI 208A Main Indicator Interconnect Figure 4 9 KI 208A Main Indicator Interconnect ...

Страница 57: ...500 SERIES INSTALLATION MANUAL Page 4 39 Page 4 40 blank P N 190 00181 02 Page Rev B 4 11 8 Annunciators Switches Interconnect Figure 4 10 Annunciators Switches Interconnect ...

Страница 58: ...500 SERIES INSTALLATION MANUAL Page 4 41 Page 4 42 blank P N 190 00181 02 Page Rev B 4 11 9 RS 232 Serial Data Interconnect Figure 4 11 RS 232 Serial Data Interconnect ...

Страница 59: ...500 SERIES INSTALLATION MANUAL Page 4 43 Page 4 44 blank P N 190 00181 02 Page Rev B 4 11 10 ARINC 429 EFS 40 50 Interconnect Figure 4 12 ARINC 429 EFS 40 50 Interconnect ...

Страница 60: ...ION MANUAL Page 4 45 Page 4 46 blank P N 190 00181 02 Page Rev B 4 11 11 ARINC 429 Sandel EHSI Interconnect 1 500 Series Unit 1 Sandel SN3308 Figure 4 13 ARINC 429 Sandel EHSI Interconnect 1 500 Series Unit 1 Sandel SN3308 ...

Страница 61: ...NSTALLATION MANUAL Page 4 47 Page 4 48 blank P N 190 00181 02 Page Rev B 4 11 12 ARINC 429 Sandel EHSI Interconnect 2 GNS 530 1 Sandel SN3308 Figure 4 14 ARINC 429 Sandel EHSI Interconnect 2 GNS 530 1 Sandel SN3308 ...

Страница 62: ...NSTALLATION MANUAL Page 4 49 Page 4 50 blank P N 190 00181 02 Page Rev B 4 11 13 ARINC 429 Sandel EHSI Interconnect 2 GNS 530 2 Sandel SN3308 Figure 4 15 ARINC 429 Sandel EHSI Interconnect 2 GNS 530 2 Sandel SN3308 ...

Страница 63: ...500 SERIES INSTALLATION MANUAL Page 4 51 Page 4 52 blank P N 190 00181 02 Page Rev B 4 11 14 ARINC 429 Air Data IRU AHRS Interconnect Figure 4 16 ARINC 429 Air Data IRU AHRS Interconnect ...

Страница 64: ...500 SERIES INSTALLATION MANUAL Page 4 53 Page 4 54 blank P N 190 00181 02 Page Rev B 4 11 15 ARINC 429 Flight Control Interconnect Figure 4 17 ARINC 429 Flight Control Interconnect ...

Страница 65: ...500 SERIES INSTALLATION MANUAL Page 4 55 Page 4 56 blank P N 190 00181 02 Page Rev B 4 11 16 Weather and Traffic Interconnect Figure 4 18 Weather and Traffic Interconnect ...

Страница 66: ...500 SERIES INSTALLATION MANUAL Page 4 57 Page 4 58 blank P N 190 00181 02 Page Rev B 4 11 17 Audio Panel Interconnect Figure 4 19 Audio Panel Interconnect ...

Страница 67: ...500 SERIES INSTALLATION MANUAL Page 4 59 Page 4 60 blank P N 190 00181 02 Page Rev B 4 11 18 VOR ILS Indicator Interconnect Figure 4 20 VOR ILS Indicator Interconnect ...

Страница 68: ...500 SERIES INSTALLATION MANUAL Page 4 61 Page 4 62 blank P N 190 00181 02 Page Rev B 4 11 19 RMI OBI Interconnect Figure 4 21 RMI OBI Interconnect ...

Страница 69: ...500 SERIES INSTALLATION MANUAL Page 4 63 Page 4 64 blank P N 190 00181 02 Page Rev B 4 11 20 King Serial Panel DME Tuning Interconnect Figure 4 22 King Serial Panel DME Tuning Interconnect ...

Страница 70: ...500 SERIES INSTALLATION MANUAL Page 4 65 Page 4 66 blank P N 190 00181 02 Page Rev B 4 11 21 King Serial Remote DME Tuning Interconnect Figure 4 23 King Serial Remote DME Tuning Interconnect ...

Страница 71: ...500 SERIES INSTALLATION MANUAL Page 4 67 Page 4 68 blank P N 190 00181 02 Page Rev B 4 11 22 Parallel 2 OF 5 DME Tuning Interconnect Figure 4 24 Parallel 2 OF 5 DME Tuning Interconnect ...

Страница 72: ...500 SERIES INSTALLATION MANUAL Page 4 69 Page 4 70 blank P N 190 00181 02 Page Rev B 4 11 23 Parallel BCD Slip Code DME Tuning Interconnect Figure 4 25 Parallel BCD Slip Code DME Tuning Interconnect ...

Страница 73: ...500 SERIES INSTALLATION MANUAL Page 4 71 Page 4 72 blank P N 190 00181 02 Page Rev B 4 11 24 King Serial KA 120 Interconnect Figure 4 26 King Serial KA 120 Interconnect ...

Страница 74: ...made the desired selection press the ENT key to accept the entry 5 2 INSTALLATION CONFIGURATION PAGES The Configuration Pages described in the following sections are in the order found when rotating the right small knob clockwise starting at the MAIN ARINC 429 CONFIG page Use the procedure described in section 5 1 to get to this page NOTE All Configuration Pages shown apply to the GNS 530 but not ...

Страница 75: ...oystick waypoint information from a RADAR graphics unit Sandel EHSI Selected course and heading information from the following EHSI system Sandel SN3308 DATA OUT Selection Description Off No unit s connected to ARINC 429 output ARINC 429 Standard ARINC 429 output data non GAMA GAMA 429 ARINC 429 data as defined by the General Aviation Manufacturers Association GAMA General Aviation Subset 2nd Edit...

Страница 76: ...nformation from the following units Shadin 91204XM Digital Fuel Management System TSO d Shadin 91053XM Digital Fuel Management System JP Instruments EDM 700 or EDM 760 Engine Monitor Arnav ei fuel Serial fuel flow information from the following units ARNAV FC 10 FT 10 Electronics International FP 5L Shadin fadc Serial air data and fuel flow information from the following units Shadin 9628XX X Fuel...

Страница 77: ...l 3 input CHAN 3 OUTPUT Selection Description Off No unit s connected to channel 3 output Crossfill Serial transfer of flight plans and user waypoints between two 500 Series units CHAN 4 INPUT Selection Description Off No unit s connected to channel 4 input WX 500 Lightning strike information from a BF Goodrich WX 500 Stormscope CHAN 4 OUTPUT Selection Description Off No unit s connected to channe...

Страница 78: ...rd JOYSTICK WPT Latitude and longitude of a joystick waypoint sent by an EFIS or RADAR indicator 5 2 4 MAIN LIGHTING Page Select the MAIN LIGHTING Page see Figure 5 4 This page allows you to set display parameters that affect the display backlight and key lighting brightness The DISPLAY and KEY lighting characteristics are adjusted separately each with the following fields LIGHTING Shows the curre...

Страница 79: ...r 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 OFFSET Adjusts the lighting level up or do...

Страница 80: ...on Verify That APR The APR annunciator is active and inactive as selected on this page GPS The GPS source select annunciator is active and inactive as selected on this page INTEG The INTEG annunciator is active and inactive as selected on this page MSG The MSG annunciator is active and inactive as selected on this page OBS The OBS annunciator is active and inactive as selected on this page TERM Th...

Страница 81: ...VERT flag is hidden In view The LAT VERT flag is in view TO FROM Selection Verify That FROM The FROM flag is in view Hidden 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 will appear Selecting this field will c...

Страница 82: ...6 975 MHz can be used SPACING Selection Description 25 0 kHz Selects traditional 25 kilohertz spacing 760 channel 8 33 kHz Selects 8 33 kilohertz channel spacing which is required in some areas of the world CAUTION 8 33 kHz channels are not authorized for use in the United States SQ 250 Sets the squelch threshold for 25 kHz channel spacing operation May be set to any value between 0 zero and 63 Th...

Страница 83: ... Select the VOR DISCRETE INPUTS Page see Figure 5 9 This page allows you to verify the operation of an external VLOC transfer switch that may be present in the installation Selection Verify That REMOTE XFR The box is filled in while a remote VLOC transfer switch is pressed 5 2 11 VOR LOC GS CDI Page GNS 530 Only Select the VOR LOC GS CDI Page see Figure 5 10 This page allows you to verify and cali...

Страница 84: ... the 500 Series VOR LOC GS OBS inputs The SELECTED COURSE field should indicate near to 150 and a Calibrate to 150 field will appear Selecting this field will calibrate the 500 Series to match the input source Verify OBS operation by checking that the course displayed on the 500 Series is within 2 of the selected course Do this at 30 intervals around the OBS card DME CHNL MODE This configuration a...

Страница 85: ...ption Common Common VOR ILS receiver only 429 data with SDI 0 is used VOR ILS 1 Number 1 Pilot VOR ILS receiver Only 429 data with SDI 0 or SDI 1 is used VOR ILS 2 Number 2 Copilot VOR ILS receiver Only 429 data with SDI 0 or SDI 2 is used DME MODE Selection Description Directed freq 1 If the GNS 530 is connected to a multi channel ARINC 429 DME channel 1 of that DME will be tuned Directed freq 1 ...

Страница 86: ... TEST Page see Figure 5 13 This page shows current strike activity WX 500 status and the heading supplied by the WX 500 The WX 500 mode may be changed to Demo Noise monitor Self test Strike test or Weather Verify that the WX 500 mode can be changed Refer to the WX 500 manual for specific installation test procedures for the WX 500 using this page to view strike data change the WX 500 mode view WX ...

Страница 87: ... to the BFG Skywatch installation manual for system checkout For Ryan TCAD see Figure 5 16 this page shows the current shield mode and altitude Verify that the TCAD shield mode may be changed Ground GND Terminal TML Standard STD En Route ENR or Unrestricted UNR and that the TCAD is reporting the correct altitude Refer to the Ryan TCAD installation manual for system checkout 5 2 17 RYAN TCAD CONFIG...

Страница 88: ...ies 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 noting any discrepancies is typically adequate evidence of correct ARINC 429 operation Parameter Self test Value Course Deviation Half left deviation TO indication flag pulled Glideslope...

Страница 89: ... the following frequencies 121 175 MHz 121 200 MHz 131 250 MHz 131 275 MHz 131 300 MHz 10 Repeat steps 3 through 6 for all COM transceivers installed in the aircraft 11 If the GPS NAV flag comes into view refer to Section 2 2 7 for options to improve performance 5 3 7 VHF COM Check GNC 520 and GNS 530 Only A flight test is recommended after the installation is complete to ensure satisfactory perfo...

Страница 90: ...Page Rev B Appendix A CERTIFICATION DOCUMENTS A 1 Continued Airworthiness Maintenance of the 500 Series units is on condition only Refer to the 500 Series Maintenance Manual Garmin P N 190 00181 05 Periodic maintenance of the 500 Series units is not required ...

Страница 91: ...ategory C Humidity 6 0 Equipment tested to Category A Shock 7 0 Equipment tested per DO 160C Par 7 2 1 Operational 7 2 Crash Safety 7 3 Vibration 8 0 Equipment tested without shock mounts to Categories B M N Explosion 9 0 Equipment identified as Category X no test required Waterproofness 10 0 Equipment identified as Category X no test required Fluids Susceptibility 11 0 Equipment identified as Cat...

Страница 92: ...ck 7 0 Equipment tested per DO 160C Par 7 2 1 Operational 7 2 Crash Safety 7 3 Vibration 8 0 Equipment tested without shock mounts to Categories B M N Explosion 9 0 Equipment identified as Category X no test required Waterproofness 10 0 Equipment identified as Category X no test required Fluids Susceptibility 11 0 Equipment identified as Category X no test required Sand and Dust 12 0 Equipment ide...

Страница 93: ...perational 7 2 Crash Safety 7 3 Vibration 8 0 Equipment tested without shock mounts to Categories B M N Explosion 9 0 Equipment identified as Category X no test required Waterproofness 10 0 Equipment identified as Category X no test required Fluids Susceptibility 11 0 Equipment identified as Category X no test required Sand and Dust 12 0 Equipment identified as Category X no test required Fungus 1...

Страница 94: ...sh Safety 7 3 Not Applicable Vibration 8 0 Equipment tested without shock mounts to Categories C L M Y Explosion 9 0 Equipment identified as Category X no test required Waterproofness 10 0 Equipment tested to Category S Fluids Susceptibility 11 0 Equipment tested to Category F with Ethylene Glycol De Icing Fluid Sand and Dust 12 0 Equipment identified as Category X no test required Fungus 13 0 Equ...

Страница 95: ...Page A 6 500 SERIES INSTALLATION MANUAL Page Rev B P N 190 00181 02 This page intentionally left blank ...

Страница 96: ... MANUAL Page B 1 P N 190 00181 02 Page Rev B Appendix B STC Permission Consistent with N8110 69 or Order 8110 4 Aviation Authority approved installers are hereby granted permission to use STC 2166WI A data to modify aircraft ...

Страница 97: ...Page B 2 500 SERIES INSTALLATION MANUAL Page Rev B P N 190 00181 02 STC form not available at time of release ...

Страница 98: ...500 SERIES INSTALLATION MANUAL Page B 3 P N 190 00181 02 Page Rev B ...

Страница 99: ...Page B 4 500 SERIES INSTALLATION MANUAL Page Rev B P N 190 00181 02 ...

Страница 100: ... 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 once every second The track desired track and bearing to waypoint angles and the magnetic variation are output according to the current mode of the...

Страница 101: ...ack 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 identifier will be blank filled on right if less than 5 characters in identifier L d d d d Bearing to...

Страница 102: ...ing navigated by the GNC 500 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 will be output approximately once every second id item designator 3 ASCII characters route sequence number is 01 seq sequence number 1 binary byte last waypoint flag ...

Страница 103: ...f 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 x d 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 xxxxxxx undefined dddddddd lon...

Страница 104: ...m Shadin 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 I...

Страница 105: ...aracter 0x03 Note Checksum is calculated by adding each byte in the message 2 through 51 such that carries are discarded to give a one byte result The ASCII coded decimal representation of that byte is given ranging from 0 0x30 0x30 0x30 to 255 0x32 0x35 0x35 D 5 ARNAV EI FUEL FLOW SENTENCE The GARMIN GNC 400 shall be capable of receiving the following 13 byte message from the ARNAV or Electronics...

Страница 106: ...epresents 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 character...

Страница 107: ...Page D 4 500 SERIES INSTALLATION MANUAL Page Rev B P N 190 00181 02 This page intentionally left blank ...

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