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SkyNode

® 

S100 Installation and Operation Manual

 

 

Page 

11

 of 

32

 

 

S100-400, R2.01

 

 

 

4.

 

Installation 

 

4.1.

 

Introduction 

 

This section provides information regarding the installation of the S100.  Close adherence to these 
suggestions will assure optimum performance of the system.  It is the responsibility of the installer to 
design the installation on or within the limits specified in this manual.  The installation approval by the 
relevant certification authority is the responsibility of the installer. 

 

4.2.

 

Unpacking 

 

Following verification of shipping documents, move the case to a clean area.  Remove packing material 
and keep ready.  Remove the unit carefully and place it on a flat clean surface.  Verify that the part and 
serial numbers on the shipping invoice matches the part and serial numbers on the unit label.  In case 
of mismatch, contact Latitude Technologies for details.  Perform a visual inspection of the unit to 
ensure that it was not damaged during shipment. If you ordered the installation kit ensure that all 
connectors are in the package. 
 

4.3.

 

Airworthiness Integrity-Design Considerations 

 

It is mandatory that, during the design of the installation airworthiness, considerations be taken into 
account as to not change the airworthiness integrity of the aircraft being modified.  Special attention 
should therefore be taken in the following areas: 

 

4.3.1.

 

Cable Routing 

 

While installing the additional wiring required for integrating the system into the aircraft it is important 
that the existing cable routing and system separation established by the aircraft OEM be respected and 
remain unchanged. 

 

4.3.2.

 

Grounding 

 

While installing the additional wiring and grounds required to integrate the system into the aircraft it is 
important to install grounding point at proper locations.  If existing grounding point are to be used 
ensure that the number of grounds on that location is not exceeded and always follow the aircraft OEM 
Maintenance Manual guide. Always attach the power ground for this system to grounds designated or 
used by the OEM as DC Grounds (as opposed to AC or shields or signal grounds). It is highly 
recommended to bring the power ground to a DC ground in close proximity to the circuit breaker that 
feeds the S100.(See Appendix A) 

 

4.3.3.

 

Wiring Integrity 

 

Ensure you follow the guidelines of this Installation Manual as to the size and quality of the wiring and 
associated components.  Any deviation may require more data and analysis from the local approval 
authority for the modifications required to install the S100. (See Appendix A). Ensure that all added 
wiring is clamped in accordance with 

FAA AC43.13-1B, Chapter 11.

 

 

Содержание SkyNode S100

Страница 1: ...YNODE S100 TRACKING SYSTEM P N S100 001 Document No S100 400 Creation Jan 24 2007 Revision 2 01 Jun 17 2014 LATITUDE TECHNOLOGIES CORPORATION 101 3375 Whittier Ave Victoria BC Canada V8Z 3R1 Tel 250 4...

Страница 2: ...ES Information in this document is subject to change without notice Latitude Technologies reserves the right to change or improve their products and to make changes in the content of this material wit...

Страница 3: ...all shipping charges duties and taxes for products returned to Latitude Technologies Corporation from outside of Canada This warranty shall not apply to damage resulting from Improper or inadequate m...

Страница 4: ...7 S100 DIMENSIONS 10 4 INSTALLATION 11 4 1 INTRODUCTION 11 4 2 UNPACKING 11 4 3 AIRWORTHINESS INTEGRITY DESIGN CONSIDERATIONS 11 4 3 1 Cable Routing 11 4 3 2 Grounding 11 4 3 3 Wiring Integrity 11 4...

Страница 5: ...igure 4 S100 Terminal Menu 18 List of Tables Table 1 Latitude Technologies KT006 Kit 9 Table 2 Latitude Technologies KT007 Kit 9 Table 3 S100 Input Interface 13 Table 4 S100 Output Interface 13 Table...

Страница 6: ...may have occurred since the printing of this document Please contact Latitude Technologies Corporation for the most recent version 1 2 Acronyms and Abbreviations CPU Computer EMI Electromagnetic Inter...

Страница 7: ...n recommendations of Section 4 and the Environmental Qualification Table of Appendix C 1 6 Safety Precautions There is no specific safety precaution as such associated with this equipment 2 Referenced...

Страница 8: ...ns Length 6 80 inches 17 3cm Width 4 00 inches 10 2cm Height 1 10 inches 2 8 cm Weight 0 94 lbs 426 g Mounting Any direction Provide access for visibility of Status Indicators for Troubleshooting Mate...

Страница 9: ...traight crimp for RG 400 cable M39012 55 4502 1 CN048 TNC straight plug for RG400 cable M39012 30 0503 1 550 0101 Ziploc bag 2 x 3 1 550 0103 Ziploc bag 4 x 6 Table 1 Latitude Technologies KT006 Kit T...

Страница 10: ...SkyNode S100 Installation and Operation Manual Page 10 of 32 S100 400 R2 01 3 7 S100 Dimensions Dimensions are provided in inches Figure 2 S100 Outline Drawing...

Страница 11: ...ge the airworthiness integrity of the aircraft being modified Special attention should therefore be taken in the following areas 4 3 1 Cable Routing While installing the additional wiring required for...

Страница 12: ...is compatible with the Environment that the S100 was qualified to See Appendix C It is also mandatory that the S100 be installed so that the side of the unit that shows the status lights can be acces...

Страница 13: ...to a squat switch Engine On Off when connected to the engine hours meter or many other possibilities Configuring discrete inputs is done remotely by Latitude Technologies Corporation for assistance ca...

Страница 14: ...or communication The main RS 232 port is P2 the DB9 9 pin serial port on the front of the device this port outputs all the debug information and can also be used with Latitude API devices This is also...

Страница 15: ...ge when the weight decreases a certain amount i e if the aircraft releases a load The analog inputs can measure DC voltage levels from 0V to 28V You may be required to change the firmware version on y...

Страница 16: ...Systems antenna 3 5 dia passive GPS antenna TNC jack white Table 8 GPS Antenna Part Numbers 4 4 4 3 Iridium Antenna Latitude P N Manufacture s P N Description MD015 S3IR16RR P XTB 1 Antcom Iridium An...

Страница 17: ...uble checked and verified whenever changes are made To determine what firmware version is currently installed and the unit s serial number power up the S100 and observe the serial port data output dis...

Страница 18: ...n is used The following sections provide a brief description of what the modifiable settings indicate 5 1 1 Edit GPS Interval The GPS Interval is the length of time between the S100 s processing and s...

Страница 19: ...messages will display all logged position messages that have not been transmitted successfully Deleting Resetting the log will clear any untransmitted position messages Deleting the log cannot be und...

Страница 20: ...at all LED s are off on the S100 Table 10 Pre Test Checklist 6 2 Functional Test No Engine This test requires a facility to monitor the availability of the aircraft on the Latitude web site Prior to p...

Страница 21: ...ngine s Turn all electrical and electronic equipment on the aircraft Landing Lights Taxi Lights Blowers XPDR ADF GPS etc While performing the tests below ensure that there is no noticeable disturbance...

Страница 22: ...D Patterns during Startup On startup the system will enter its internal system check During this time the system will cycle through the LEDs from top to bottom twice Provided that all internal system...

Страница 23: ...ata signal 15 VDC 15 RTS AUX RS232 output Auxiliary serial data signal 5 VDC 16 GND Ground Signal Ground return 0 VDC 17 GPS IN RS232 input NMEA 0183 serial data receive alternate GPS source input 15...

Страница 24: ...TS RS232 input Serial data signal 15 VDC 8 CTS RS232 output Serial data signal 5 VDC 9 RI 5V RS232 output Serial data signal 5 VDC Factory option to set P2 Pin 9 to a fixed 5V 100mA supply Table 14 S1...

Страница 25: ...SkyNode S100 Installation and Operation Manual Page 25 of 32 S100 400 R2 01 APPENDIX B INTERCONNECT INTERFACES...

Страница 26: ...COAX CONNECTOR SMA OR TNC Single Wires ALL WIRES PER AWG22 UNLESS OTHERWISE SPECIFIED M22759 41 22 9 OR EQUIVALENT Connector P1 DB25 Connector P2 DB9 GPS Antenna Connector M39012 30 0503 Straight or M...

Страница 27: ...g Connectors TNC male straight plug P N TNC male 90 plug P N 10 MIL C 17 RG400 0 195 1 00 M39012 30 0503 M39012 20 0007 12 MIL C 17 RG400 0 195 1 00 M39012 30 0503 M39012 20 0007 12 MIL C 17 RG142 0 1...

Страница 28: ...6 4502 15 MIL C 17 113 RG142 0 195 1 00 M39012 55 4502 M39012 56 4502 15 MIL C 17 128 RG400 0 195 1 00 M39012 55 4502 M39012 56 4502 20 MIL C 17 128 RG400 0 195 1 00 M39012 55 4502 M39012 56 4502 25 M...

Страница 29: ...SkyNode S100 Installation and Operation Manual Page 29 of 32 S100 400 R2 01 Figure B1 Typical Wiring Installation COMBINED GPS IRIDIUM ANTENNA GPS ANTENNA IRIDIUM ANTENNA...

Страница 30: ...Skynode S100 Installation and Operation Manual Page 30 of 32 S100 400 R2 01 APPENDIX C ENVIRONMENTAL TESTS TABLE...

Страница 31: ...temperature 85 o C Operating 60 o C 50 000 feet 8000 feet to 50000 feet 15000 feet Temperature Variation 5 0 Equipment tested to Category B 5 o C min Humidity 6 0 Equipment tested to Category A 95 RH...

Страница 32: ...ategory X no test performed Radio Frequency Susceptibility 20 0 Equipment identified as Category X no test performed Emission of Radio Frequency Energy 21 0 Equipment tested to Category B Lightning In...

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