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Garmin GPS 165, Руководство по установке

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Содержание GPS 165

Страница 1: ...Av Kit Install Manual 190 00066 02 Rev J Page 1 GPS 165 INSTALLATION MANUAL GARMIN INTERNATIONAL INC PART NUMBER 190 00066 02 1200 E 151st STREET REVISION J 27 MARCH 1998 OLATHE KANSAS 66062 3426 ...

Страница 2: ...160 Rev B 01 Jun 1994 Add Crimp Extract Tools Access List Misc 3405 Rev C 12 Sept 1994 Add Electronics International fuel flow interface selection update output unit list Fig 1 3 installation requirements and wiring diagram 4841 Rev D 09 Nov 1995 Add Mid Continent as option 5219 Rev E 29 Jan 1996 Add MCI options JST connector details misc 5827 Rev F 28 June 1996 Chg to barrel type crimp connectors...

Страница 3: ...E 2 2 UNIT ACCESSIBILITY 2 3 CABLING AND WIRING 2 4 COOLING AIR 2 5 EXTERNAL ALTITUDE INPUT 2 6 MINIMUM INSTALLATION REQUIREMENTS SECTION 3 INSTALLATION PROCEDURE 3 1 INSTALLATION ACCESSORIES 3 2 ANTENNA INSTALLATION 3 3 CABLE INSTALLATION 3 4 GPS 165 INSTALLATION AND REMOVAL SECTION 4 POST INSTALLATION CONFIGURATION AND CHECKOUT PROCEDURE 4 1 TEST MODE OPERATIONS 4 2 INSTALLATION CONFIGURATION 4 ...

Страница 4: ...TEST 4 3 7 POWER TEST 4 3 8 SIGNAL ACQUISITION TEST 4 3 9 VHF COMM INTERFERENCE CHECK SECTION 5 CERTIFICATION SECTION 6 CONTINUED AIRWORTHINESS APPENDIX A CERTIFICATION DOCUMENTS APPENDIX B CONNECTOR CHANGES APPENDIX C REFERENCE DISCRETE SWITCH ANNUNCIATOR INSTALLATION APPENDIX D STC PERMISSION ...

Страница 5: ...DEFINITION 26 PIN HD DSUB 1 3 INTERCONNECT SCHEMATIC 2 1 ANTENNA INSTALLATION CONSIDERATIONS 2 2 GPS INSTALLATION CONSIDERATIONS 3 1 REMOTE BATTERY PACK ASSEMBLY 3 2 GA 56 ANTENNA INSTALLATION 3 3 FLANGE MOUNT GA 56 ANTENNA INSTALLATION 3 4 COAX CABLE INSTALLATION 3 5 GPS 165 FACE DIMENSIONS 3 6 AVIATION RACK INSTALLATION ...

Страница 6: ... 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 1 2 1 PHYSICAL CHARACTERISTICS Width 5 75 inches Height 2 25 inches Depth 5 00 inches GPS 165 Weight 2 0 lbs Low Profile Antenna Weight 4 oz Max Air Speed Subsonic Structural rating for ...

Страница 7: ...es an unread message is available for viewing RS232 chan 1 output data Output capable of driving devices as listed in Section Pin 24 4 Conforms to the EIA specification EIA 232C RS232 chan 2 output data Output capable of driving devices as listed in Section Pin 19 4 Conforms to the EIA specification EIA 232C RS232 chan 1 input data Input capable of receiving data from devices as listed Pin 17 in S...

Страница 8: ...tion of the suggestions in this section are required to achieve the desired performance and reliability from the GPS 165 2 1 ANTENNA CONSIDERATIONS 2 1 1 SATELLITE VISIBILITY The GARMIN GA 56 Low Profile GPS Antenna must be mounted on top of the aircraft For best performance select a location with an unobstructed view of the sky above the aircraft when in level flight Figure 2 1 illustrates a typi...

Страница 9: ... is adequate depth for the unit and connectors in the instrument panel A location away from heating vents or other sources of heat generation is optimal In order to minimize accumulation of dirt and residues on the face of the unit it is best to mount the unit with its face vertically positioned Figure 2 2 illustrates a typical aviation rack installation 2 3 CABLING AND WIRING The recommended ante...

Страница 10: ...ormation can come from an analog resolver or from an EFIS via the ARINC 429 bus or RS 422 bus HSI CDI Device This device displays Nav Flag Left Right and To From This can be displayed on an EFIS or HSI External Annunciators and Switches NAV GPS Switch Annunciator GPS Sequence Switch Annunciator Approach Switch Annunciator not required for A2 Message Annunciator Arrival Annunciator The installer is...

Страница 11: ... 013 00029 00 MD41 428 INTEGRATED SW ANN UNIT HOR 28V 013 00029 01 MD41 424 INTEGRATED SW ANN UNIT HOR 14V 013 00029 02 MD41 428 5V INTEGRATED SW ANN UNIT HOR 28V 5V LIGHTING 013 00029 05 MD41 438 INTEGRATED SW ANN UNIT VERT 28V 013 00029 06 MD41 434 INTEGRATED SW ANN UNIT VERT 14V 013 00029 07 MD41 438 5V INTEGRATED SW ANN UNIT VERT 28V 5V LIGHTING MISC OPTIONS 190 00066 00 GPS 165 PILOT S GUIDE ...

Страница 12: ...d the recommendations of Section 2 Secure the cable in accordance with good aviation practice B Trim the coaxial cable to the desired length and install the BNC connector 330 00087 00 per the cabling instructions on Figure 3 4 If the connector is provided by the installer follow the connector manufacturer s instructions for cable preparation C Contacts for the 37 and 26 pin connectors must be crim...

Страница 13: ...OST INSTALLATION CONFIGURATION CHECKOUT PROCEDURE Before starting the below operations unit initialization must occur Do this by first removing any data cards and then turning the unit on Press enter in response to Select operating mode Normal ok Press enter in response to No Jeppesen database rte prx limited to user wpts ok After the Satellite Status Page is displayed for 5 seconds the unit may b...

Страница 14: ...alt Serial altitude received from Shadin 9000T Serializer System Non TSO d Shadin 9200T Series Serializer System Non TSO d Shadin 8800T Series Encoder System TSO d shadin fuel Fuel information received from Shadin 91204XT Digital Fuel Management System TSO d Shadin 91053XT Digital Fuel Management System TSO d arnav ei fuel Fuel information received from Arnav Model FC 10 Fuel Computer TSO d Arnav ...

Страница 15: ...d equipment The available options are Input Field Description off No units connected to ARINC 429 input Selected Course Any ARINC 429 compatible unit that transmits the Selected Course word label 100 Course heading Any ARINC 429 compatible unit that transmits the Selected Course word label 100 and at least one headinglabel trueheading label314 magneticheading label 320 Heading Any ARINC 429 compat...

Страница 16: ... heading 147 Magnetic variation 261 GPS navigation mode 275 Navigation status 326 Lateral scale factor 351 Distance to destination 352 Time to destination Flight plan data Label octal Description 074 Flight plan header 075 Active from to waypoints 113 Message checksum 300 Station magnetic variation type class 303 Message length type number 304 Waypoint identifier characters 1 3 305 Waypoint identi...

Страница 17: ...lies Lnav 1 Only data marked for Lnav 1 is used Lnav 2 Only data marked for Lnav 2 is used common Data marked for either Lnav 1 or Lnav 2 is used For ARINC 429 input data the following applies Lnav 1 Only data with SDI 0 or SDI 1 is used Lnav 2 Only data with SDI 0 or SDI 2 is used common Only data with SDI 0 is used NOTE SDI 0 is an all call Fuel av gas Using Aviation gas 5 8 lbs gal jet A Using ...

Страница 18: ...3 standard 4 3 GROUND TEST The GPS 165 ground test procedure incorporates a series of six 6 display pages to test CDI flag OBI annunciator external switches altitude inputs and power functions of the unit 4 3 1 CDI AND FLAG TEST With power applied to the aviation rack and the GPS 165 unit off depress and hold the ENT key and turn the unit on release the ENT key when the display activates Rotate th...

Страница 19: ...This page displays the results of communication loop back tests Four channels are tested RS232 channel 1 and 2 RS422 and ARINC 429 Results of the test are either OPEN or OK Open means the channel s transmitter and receiver are not connected or the test failed The tests are performed continuously while on this page except for RS232 channel 2 This channel is only tested at power on and the results d...

Страница 20: ...OWER Memory Batt OK Intrnl Batt OK If the installation includes optional remote mount battery backup accessory NOTE Depending on the power source for the unit Aircraft wall charger or internal battery and the status of battery charging the top line may read Battery Power Charger Trickle Chrg Ext Pwr Rapid Charge Ext Pwr Maint Charge Ext Pwr No Charge Turn the GPS 165 off in preparation for a signa...

Страница 21: ...t h If the NAV flag comes into view the comm transmitter used may require additional RF shielding to control the excessive radiation Refer to Section 2 1 4 for suggested modifications SECTION 5 CERTIFICATION The GPS 165 has been certified for IFR enroute terminal and non precision approaches by GARMIN in a Mooney M20J See Appendix D for a copy of the STC All installations must be certified For mor...

Страница 22: ...Av KitInstall Manual 190 00066 02 Rev J Page22 FIGURE 1 1 PINOUT DEFINITION 37 PIN DSUB ...

Страница 23: ...Av Kit Install Manual 190 00066 02 Rev J Page 23 FIGURE 1 2 PINOUT DEFINITION 26 PIN HD DSUB ...

Страница 24: ...Av KitInstall Manual 190 00066 02 Rev J Page24 FIGURE 1 3A INTERCONNECT SCHEMATIC ...

Страница 25: ...Av Kit Install Manual 190 00066 02 Rev J Page 25 FIGURE 1 3B INTERCONNECT SCHEMATIC ...

Страница 26: ...Av KitInstall Manual 190 00066 02 Rev J Page26 FIGURE 1 3C INTERCONNECT SCHEMATIC ...

Страница 27: ...6 02 Rev J Page 27 FIG 2 1 ANTENNA INSTALLATION CONSIDERATIONS Antenna masked by vertical fin T tail or dorsal fin Antenna must be on top of aircraft OK Maintain 6 16 cm compass safe distance FIG 2 2 GPS INSTALLATION CONSIDERATIONS ...

Страница 28: ...Av KitInstall Manual 190 00066 02 Rev J Page28 FIGURE 3 1 REMOTE BATTERY PACK ASSEMBLY ...

Страница 29: ...Av Kit Install Manual 190 00066 02 Rev J Page 29 FIGURE 3 2 GA 56 ANTENNA INSTALLATION ...

Страница 30: ...Av KitInstall Manual 190 00066 02 Rev J Page30 FIGURE 3 3 FLANGE MOUNT GA 56 ANTENNA INSTALLATION ...

Страница 31: ...Av Kit Install Manual 190 00066 02 Rev J Page 31 FIGURE 3 4 COAX CABLE INSTALLATION ...

Страница 32: ...Av KitInstall Manual 190 00066 02 Rev J Page32 FIGURE 3 5 GPS 165 FACE DIMENSIONS ...

Страница 33: ...Av Kit Install Manual 190 00066 02 Rev J Page 33 FIGURE 3 6 AVIATION RACK INSTALLATION ...

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Страница 38: ...me contacts are pins as shown while others are the socket type The type used will vary with the installation When working with the stamped crimp type contacts the following tools should be used Tools 37 position connectors 26 position connector supplier Crimp Tool Extraction Tool Crimp Tool Extraction Tool Amp 58448 2 91067 22 90430 1 91285 1 ITT Cannon 995 2000 000 980 0008 124 995 2000 022 980 0...

Страница 39: ...FIGURE C 1 INTERCONNECT SCHEMATIC APPENDIX C REFERENCE DISCRETE SWITCH ANNUNCIATOR INSTALLATION Av Kit Install Manual 190 00066 02 Rev J Page 39 ...

Страница 40: ...FIGURE C 2 INTERCONNECT SCHEMATIC Av Kit Install Manual 190 00066 02 Rev J Page 40 ...

Страница 41: ...FIGURE C 3 SWITCH ANNUNCIATOR LAYOUT Av Kit Install Manual 190 00066 02 Rev J Page 41 ...

Страница 42: ... Manual 190 00066 02 Rev J Page 42 APPENDIX D STC PERMISSION Consistent with N8110 69 or Order 8110 4 Aviation Authority approved installers are hereby granted permission to use STC SA00155WI data to modify aircraft ...

Страница 43: ...Av Kit Install Manual 190 00066 02 Rev J Page 43 ...

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