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GWX 68 Installation Manual

Page 3-3

190-00286-01

Preliminary Revision 1

3.3.1 Shield Block Assembly Procedure

The parts for the connector and backshell assembly, GWX68 installations, are listed in Table 3-3 and
shown in Figure 3-1.

Figure 3

-

1. Shield Block Install onto Backshell Connector Assembly

Table 3

-

4. Shield Block Components

Backshell Assembly

Garmin P/N

Shield Block

Garmin P/N

011-00950-12

(25/44 Pin High Density)

011-01169-01

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Summary of Contents for 010-00299-00

Page 1: ...tion Manual 1 1 36 GWX 68 Installation Manual 5 1 5 12 05 Preliminary Release NOTES 1 DESCRIPTION Installation Documentation 2 PAGE SIZE Letter Width 8 5 inches Height 11 inches Tabloid Width 11 0 inches Height 17 0 inches 3 PAGINATION double sided letter sheets single sided tabloid sheets 4 MATERIAL 24 pound bond Approved equivalents allowed 5 COLOR Black Ink on White Paper Stock 6 BINDERY Three ...

Page 2: ...Garmin P N 190 00286 01 May 2005 Preliminary Revision 1 Preliminary GWX 68 Installation Manual ...

Page 3: ...ereto provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin International Inc 1200 E 151st Street Olathe KS 66062 USA Telephone 913 397 8200 Aviation Dealer Technical Support Line Toll Free ...

Page 4: ...0 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 is being provided in accordance with California s Propos...

Page 5: ...URE LEVEL MPEL The zone in which the radiation level exceeds the US Government standard of 1 mW cm2 is the semi circular area of at least 9 16 ft from the 10 antenna and 10 83 ft from the 12 antenna as indicated in the illustration below All personnel must remain outside of this zone The distance to the MPEL boundary is calculated upon the basis of each antenna available with the GWX 68 system rat...

Page 6: ... is not scanning the danger increases 2 The recommended safe distance which is established above should be followed The distance from any person to the radar should be greater than that distance 3 Personnel should be advised to avoid the end of an open waveguide unless the radar is turned off 4 Personnel should be advised to avoid looking into a waveguide or into the open end of a coaxial connecto...

Page 7: ...tion Materials 2 1 2 3 Installation Considerations 2 1 2 4 Cabling and Wiring 2 2 2 5 Cooling Requirements 2 2 2 6 Mounting Requirements 2 2 3 INSTALLATION PROCEDURE 3 1 3 1 Unpacking Unit 3 1 3 2 Wiring Harness Installation 3 1 3 3 Backshell Assemblies and D Subminiature Connectors 3 2 3 4 Unit Installation 3 10 3 5 Post Installation Configuration Checkout 3 10 3 6 Continued Airworthiness 3 10 4 ...

Page 8: ...utline Drawing A 1 B 1 GWX 68 Typical G1000 Interconnect Wiring Diagram B 1 B 2 GWX 68 Typical MX20 Interconnect Wiring Diagram B 3 B 3 GWX 68 Analog Stabilization Interconnect Wiring Diagram B 5 B 4 GWX 68 AHRS Stabilization Interconnect Wiring Digram B 7 LIST OF TABLES TABLE PAGE 3 1 Pin Contact Part Numbers 3 1 3 2 Recommended Crimp Tools 3 1 3 3 Backshell Assembly 3 2 3 4 Shield Block Componen...

Page 9: ...and the purpose of the modification The table is current at the time of publication of this manual see date on front cover and is subject to change without notice Authorized Garmin Sales and Service Centers are encouraged to access the most up to date bulletin and advisory information on the Garmin Dealer Resource web site at www garmin com using their Garmin provided user name and password MOD LE...

Page 10: ...aircraft while airborne is prohibited by FCC rules Due to the potential for interference with onboard systems the operation of ground based cellular communication devices while onboard an aircraft that is on the ground is subject to FAA regulations 14 CFR 91 21 FCC regulation 47 CFR 22 925 prohibits airborne operation of ground based cellular telephones installed in or carried aboard aircraft Grou...

Page 11: ...midity 95 non condensing Altitude Range 1 500 ft to 50 000 ft 1 4 4 Performance Specifications Characteristics Specifications Display Colors 4 Colors Selectable Ranges 2 5 5 10 20 40 80 160 320nm Weather Avoidance Range 305nm w 12 Ant 270nm w 10 Ant Performance Index 213dB w 12 Ant 210dB w 10 Ant Rx Sensitivity 110 dBm MDS Manual Gain 12 to 64dB Antenna Beamwidth 7 8 w 12 Ant 9 0 w 10 Ant Magnetro...

Page 12: ...ments To find out the specific details on whether a particular installation is exempt from licensing please visit the FCC web site http wireless fcc gov aviation If an aircraft license is required make application for a license on FCC form 404 Application for Aircraft Radio Station License The FCC also has a fax on demand service to provide forms by fax The GWX 68 owner accepts all responsibility ...

Page 13: ...craft The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements At the time of publication installations of this TSO approved article are only approved when installed in an aircraft as part of a Garmin G1000 system 1 6 1 TSO ETSO Compliance TSO C63c Class 7 1 7 Reference Documents The following publications are sources of additional informatio...

Page 14: ...G FROM THE USE MISUSE OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT Some states do not allow the exclusion of incidental or consequential damages so the above limitations may not apply to you Garmin retains the exclusive right to repair or replace the unit or software or offer a full refund of the purchase price at its sole discretion SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE ...

Page 15: ...Page 1 6 GWX 68 Installation Manual Preliminary Revision 1 190 00286 01 This page intentionally left blank ...

Page 16: ...a installations on pressurized cabin aircraft require FAA approved installation design and engineering substantiation data whenever such antenna installations incorporate alteration penetration of the cabin pressure vessel by connector holes and or mounting arrangements For needed engineering support pertaining to the design and approval of such pressurized aircraft antenna installations it is rec...

Page 17: ...el contacts ensure that no two contacts are mounted directly adjacent to each other This minimizes the risk of contacts touching and shorting to adjacent pins and to ground Ensure that routing of the wiring does not come in contact with sources of heat RF or EMI interference Check that there is ample space for the cabling and mating connectors Avoid sharp bends in cabling and routing near aircraft...

Page 18: ...e made through a 44 pin D subminiature connector Section 4 defines the electrical characteristics of all input and output signals Required connectors and associated hardware are supplied with the connector kit See Appendix C for examples of interconnect wiring diagrams Construct the actual harnesses in accordance with aircraft manufacturer authorized interconnect standards Table 3 1 Pin Contact Pa...

Page 19: ...ckets in place Table 3 3 lists Garmin part numbers for the GWX 68 D Sub Connectors and the Backshell Assembly Table 3 3 Backshell Assembly Figure Ref Description Garmin P N 1 Cast Housing From Garmin Backshell kit 125 00085 00 2 Shield block 117 00147 xx 3 Screw 4 40 x 250 FLHP100 SS P Nylon 211 63234 08 4 Multiple Conductor Shielded Cable See Interconnect Diagrams Appendix C As Required 5 Shield ...

Page 20: ...arts for the connector and backshell assembly GWX68 installations are listed in Table 3 3 and shown in Figure 3 1 Figure 3 1 Shield Block Install onto Backshell Connector Assembly Table 3 4 Shield Block Components Backshell Assembly Garmin P N Shield Block Garmin P N 011 00950 12 25 44 Pin High Density 011 01169 01 ...

Page 21: ... the shield See Figure 3 2 Use caution when cutting the jacket to avoid damaging the individual braids of the shield When dealing with a densely populated connector with many cables it may prove beneficial to stagger the windows throughout the Window Min to Window Max range If staggering is not needed the Ideal Window length is recommended Tools needed to Accomplish the Window Cut Coaxial Cable St...

Page 22: ...ed braid and effectively take the place of items 5 and 6 For detailed instructions on product use refer to Raychem installation procedure RCPS 100 70 Raychem Recommended Heating Tools HL1802E AA 400 Super Heater CV 1981 MiniRay IR 1759 Individual Solder Sleeves and Flat Braid Solder Sleeves Reference the following MIL Specs for general solder sleeves M83519 1 1 M83519 1 2 M83519 1 3 M83519 1 4 M83...

Page 23: ...same point so no shield is exposed Slide 0 75 minimum of Teflon heat shrinkable tubing 7 onto the cable and use a heat gun to shrink the tubing The chosen size of heat shrinkage tubing must accommodate the number of conductors present in the cable Secondary Method Leave a max 0 35 of shield extending past the jacket Fold this 0 35 of shield back over the jacket Slide a solder sleeve 7 over the end...

Page 24: ...le Flat Braid is left or if only a single Flat Braid is need for this connector a Ring terminal 8 insulated 18 22 AWG MS25036 149 can accommodate this single Flat Braid If more braids exist for this connector than two per ring terminal it is permissible to terminate three braids per ring terminal This will necessitate the use of a Ring terminal 8 insulated 10 12 AWG MS25036 156 In rare situations ...

Page 25: ...ackshell strain relief and cast housing will contact the cable bundle Note Choosing to use this tape is at the discretion of the installer 12 Place the smooth side of the backshell strain relief 14 across the cable bundle and secure using the three screws 15 Warning Placing the grooved side of the strain relief across the cable bundle may risk damage to wires 13 Attach the cover 16 to the backshel...

Page 26: ...n from each wire prior to crimping 2 Insert newly crimped pins and wires 3 4 into the appropriate connector housing 5 location shown in the figure below 3 Apply the spacer 2 by wrapping it around the PCB Board 1 making sure to insert the plastic connector mounted on the board into the hole provided in the spacer 4 Plug the four conductor wire harness 3 into the connector on the PCB Board 1 5 Inser...

Page 27: ... does not provide valid outputs until the aircraft post installation configuration procedures are completed When installed as part of the G1000 integrated cockpit system the GWX 68 must have FAA approved configuration data Configuration data is loaded to the GWX 68 from an aircraft specific G1000 Software Loader Card Settings are predetermined for a specific aircraft and are typically contained wi...

Page 28: ...RINC 453 OUT B Out 6 RESERVED 7 AIRCRAFT POWER 1 In 8 RESERVED 9 AIRCRAFT POWER 1 In 10 AIRCRAFT POWER 2 In 11 RESERVED 12 AIRCRAFT POWER 2 In 13 POWER GROUND 14 RESERVED 15 POWER GROUND 16 CONFIG MODULE DATA I O 17 CONFIG MODULE POWER Out 18 ROLL ATTITUDE HI In 19 ROLL ATTITUDE LO In 20 26 VAC GYRO REF LO In 21 26 VAC GYRO REF HI In 22 ARINC 429 IN 2 A In 23 ARINC 429 IN 2 B In 24 RESERVED 25 RES...

Page 29: ...er Pin Name Connector Pin I O AIRCRAFT POWER 1 P400 7 In AIRCRAFT POWER 1 P400 9 In AIRCRAFT POWER 2 P400 10 In AIRCRAFT POWER 2 P400 12 In POWER GROUND P400 13 POWER GROUND P400 15 Pins 7 and 9 of P400 are internally connected to form AIRCRAFT POWER 1 Pins 10 and 12 of P400 are internally connected to form AIRCRAFT POWER 2 AIRCRAFT POWER 1 and AIRCRAFT POWER 2 are diode ORed to provide power redu...

Page 30: ...ERNET OUT A P400 36 Out ETHERNET OUT B P400 37 Out The Ethernet high speed data bus HSDB meets the hardware aspects of IEEE standard 802 3 for 10 base T Ethernet communications 4 4 Configuration 4 4 1 Configuration Module Pin Name Connector Pin I O CONFIG MODULE GROUND P400 1 CONFIG MODULE DATA P400 16 I O CONFIG MODULE POWER P400 17 Out CONFIG MODULE CLOCK P400 31 Out 4 5 Auto Pilot 4 5 1 Flight ...

Page 31: ...Installation Manual Preliminary Revision 1 190 00286 01 4 5 2 26 Volt AC Reference Pin Name Connector Pin I O 26 VAC GYRO REF LO P400 20 In 26 VAC GYRO REF HI P400 21 In Expected nominal input voltage is 400 Hz 26VRMS ...

Page 32: ...ING SURFACE 6 624 168 25 3 312 84 12 6 750 171 45 3 375 85 73 10 00 254 0 4X 265 THRU 6 73 25 6 4 30 7 6 4 951 029 125 75 0 74 TILT AXIS 2 47 62 7 30 MAX TILT ANGLE R5 530 140 46 MAX SPHERICAL RADIUS 10 ANTENNA R6 548 166 32 MAX SPHERICAL RADIUS 12 ANTENNA NOTES 1 DIMENSIONS INCHES mm 2 12 ANTENNA SHOWN UP PRELIMINARY 4X 211 64214 22 1 4 28 SOCKET HEAD CAP SCREWS RIGHT ANGLE CONNECTOR Figure A 1 G...

Page 33: ...APPENDIX B INTERCONNECT DRAWINGS GWX 68 Installation Manual Page B 1 Page B 2 blank 190 00286 01 Preliminary Revision 1 Figure B 1 GWX 68 Typical G1000 Interconnect Wiring Diagram ...

Page 34: ...APPENDIX B INTERCONNECT DRAWINGS GWX 68 Installation Manual Page B 3 Page B 4 blank 190 00286 01 Preliminary Revision 1 Figure B 2 GWX 68 Typical MX20 Interconnect Wiring Diagram ...

Page 35: ...APPENDIX B INTERCONNECT DRAWINGS GWX 68 Installation Manual Page B 5 Page B 6 blank 190 00286 01 Preliminary Revision 1 Figure B 3 GWX 68 Analog Stabilization Interconnect Wiring Diagram ...

Page 36: ...APPENDIX B INTERCONNECT DRAWINGS GWX 68 Installation Manual Page B 7 Page B 8 blank 190 00286 01 Preliminary Revision 1 Figure B 4 GWX 68 AHRS Stabilization Interconnect Wiring Diagram ...

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