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ISAT-200 Installation Manual

1. DOC0334 Restricted Proprietary and Confidential Information Document Rev 01 019 Page 29 of 48 SkyTrac Systems Ltd Table 22 RS 232 Port 2 Descriptions ISAT 200R Description and recommended usage Bay A Pin General purpose data port 28 TX Data out of ISAT 200 27 RX Data into ISAT 200 22 Serial data ground reference Note RS 485 Port 2 shares some circuits with RS 232 Port 2 Only one of these ports can operate at the same time The functional port is selected via SkyWeb 4 2 6 Ethernet Port Table 23 Ethernet Port Descriptions This is the Ethernet wire set used to transmit data to and from auxiliary devices DE Description and recommended usage 57 Ethernet transmit port OUT 70 Ethernet transmit port OUT 31 Ethernet transmit port IN 44 Ethernet transmit port IN 4 2 7 Analogue Inputs Table 24 Analogue Input Descriptions ISAT 200R Pin Description and recommended usage Bay A Bay B 30 Analogue Input Channel 1 67 Analogue Input Channel 2 Reserved Do not use 68 Analogue Input Channel 3 Reserved Do not use 69 Analogue Input Channel 4 80 Analogue Input Channel 5 Analogue inputs 1 4 and 5 can be configured as voltage seeking digital inputs Analogue input 1 is the recommended alternate input for Engines On Off toggle switch if a voltage seeking input is required Doc
2. 10 2 Display The ISAT 200 includes an 8 character display for assistance during configuration and troubleshooting 10 3 LED The LED on the ISAT 200 will indicate power and alert status A steady green LED indicates the ISAT 200 has power and is operating normally An amber LED indicates an Alert or error message is waiting to be viewed on the display 10 4 Button The black button on the ISAT 200 is used for scrolling through the menu and accessing different configuration options and error messages A single push press and release of the button will scroll through the menu one item at a time while pressing and holding the button will select a menu item 10 5 Ambient Light Sensor Beside the display is an Ambient Light Sensor which will automatically detect the ambient light level 10 6 USB Programming Port The USB programming port is used for updating the ISAT 200 firmware directly from a computer running Windows XP or later 10 7 SD Card Slot The SD Card slot is used for updating the ISAT 200 firmware when a computer is not available Document Rev 01 019 DOC0334 Page 42 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 11 APPENDICES 11 1 Appendix A Causes of RF Interference Some subscribers have contacted Iridium regarding the loss of signal quality when they operate their equipment near active INMARSAT terminals The power with which INMARSAT units transmit can overpower the I
3. Configuration of the ISAT 200 This section contains instructions on how to configure and set up the ISAT 200 system Section 6 Post Installation Tests This section contains instructions for tests to be performed after installation to confirm that the system has been installed correctly Section 7 Airworthiness Limitations This section describes the installation and operational limitations of the ISAT 200 system Section 8 Maintenance and Continued Airworthiness This section describes the steps required for the continued airworthiness of the ISAT 200 system Document Rev 01 019 DOC0334 Page 7 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd Section 9 Firmware Updates This section indicates the methods available to update the ISAT 200 and where to find the required instructions Section 10 ISAT 200 Human Machine Interface This section provides a brief description of the ISAT 200 human machine interface components Section 11 Appendices 1 2 1 Audience This manual is intended for qualified aircraft avionics installation technicians referred to as installers lt assumes that the installer is familiar with the tools materials and techniques of wiring and metal work required for installing radios antennas and related components into aircraft 1 2 2 References More detailed information about the ISAT 200 system can be found in the SkyWeb documentation section of the
4. IS MS OO cs om E 1 Charge Voltage The maximum voltage is 4 2 V x the number of cells connected in series 2 Charge Current We recommend 0 7 CmA When the voltage per cell is 2 9V or less charge using a charge current of 0 1CmA or less Contact Panasonic for information regarding pulse charging 3 Charge Temperature The batteries should be charged at temperatures between OG and 45 4 Reverse polarity Charging Verify the polarity of the batteries before charging to ensure that they are never charged with the polarity reversed 2 Discharging the Batteries 1 Discharge Current The current should be maintained at 1 0 CmA or less Consult Panasonic if you plan to discharge the batteries with a current in excess of 1 0 CmA 2 Discharge Temperature The batteries should be discharged at a temperature between 20 and 60 Consult Panasonic if you plan to discharge the batteries at temperatures less than 10T 3 Discharge Termination Voltage Avoid discharging at voltages less than 3 0 V per cell Over discharge can damage the performance of the battery Equip the unit with a mechanism to prevent over discharge especially in situations where the user may forget to turn the equipment off This information is generally descriptive only and is not intended to make or imply any representation guarantee or warranty with respect to any cells and batteries Cell and battery designs specifications are subject to modification
5. ISAT 200 DIO GND is isolated from the system ground DIO GND must be connected to aircraft ground for the digital inputs to function correctly 5 40 56 The status of the digital inputs can be checked from the ISAT 200 Menu Please refer to the ISAT 200 User Guide for help navigating the menu 4 2 3 Digital Voltage Seeking Inputs Table 18 Digital Voltage Seeking Input Descriptions ISAT 200R Pin Description and recommended usage Bay A Bay B 4 Asserted when 28V is applied Recommended to be used as a mission event toggle switch Note All Digital Inputs are referenced to the ISAT 200 DIO GND ISAT 200 DIO_GND is isolated from the system ground DIO_GND must be connected to aircraft ground for the digital inputs to function correctly The status of the digital inputs can be checked from the ISAT 200 Menu Please refer to the ISAT 200 User Guide for help navigating the menu If more voltage seeking inputs are required some of the analogue inputs can be configured as voltage seeking inputs See section 4 2 7 Analogue Inputs Document Rev 01 019 DOC0334 Page 28 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 4 2 4 RS 485 Data ports These are the RS 485 two wire half duplex multipoint serial communication channels used to transfer data to and from auxiliary devices These lines are used to communicate with the peripheral
6. James 01 015 397 Changed purchase to shipment in warranty statement Added note about cable conversion needing additional approval to 3 8 2 Jan 28 2011 J James 01 016 439 Corrected DO 160 strings in section 2 6 Added row for Section 26 0 to Table 12 Removed approval column from Rev History June 1 2011 M Hubert 01 017 434 Changed battery pack capacity rating to 2 25Ah Added CGR18650CG datasheet June 27 2011 J James 01 018 462 Removed EMTEQ A45240 1 Updated antenna note to include pigtail Added CDU 250 to list of supported peripheral devices Changed battery PN references to STS PN Apr 18 2012 J James 01 019 544 Updated warranty information Corrected battery connector reference Added STS0061 to battery references Updated battery specifications Corrected battery cable tie tension Removed battery data sheets Removed unit conversions Added step to apply mod status when replacing battery Jul 27 2012 J James Document Rev 01 019 DOC0334 Restricted Proprietary and Confidential Information Page 2 of 48 SkyTrac Systems Ltd Caution The ISAT 200 contains static sensitive circuitry that could be damaged from large electro static discharges directly into the ARINC 404 connector pins Use care when handling the ISAT 200 not to touch the connector pins unless properly grounded Wa
7. RS485_B1 RS485 port 1 inverted line 25 RS232_RX1 Serial 1 receiver 26 RS232_TX1 Serial 1 transmitter 27 RS232_RX2 Serial 2 receiver 28 RS232_TX2 Serial 2 transmitter 29 RS485_GND1 RS485 port 1 ground reference 30 ADC1 Analogue input 1 A1 IRIDIUM ANT Iridium antenna cable A2 GPS ANT GPS antenna cable CM Configuration Module The configuration module comes pre wired DIO_GND must be connected to aircraft ground for the digital inputs to function correctly RS 485_GND1 is isolated within the ISAT 200 system RS 485_GND1 needs to be connected to aircraft ground for reliable operation of the RS 485 databus Document Rev 01 019 DOC0334 Page 27 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 4 2 2 Digital Ground Seeking Inputs Ground seeking pins indicate a logical TRUE to the microcontroller if the input is grounded Table 17 Digital Ground Seeking Input Descriptions ISAT 200R Pin Description and recommended usage Bay A Bay B 11 Asserted when ground is applied 6 Asserted when ground is applied Recommended to be used for external emergency toggle switch Asserted when ground is applied Recommended to be used with flight event as a toggle switch Asserted when ground is applied Recommended for general use Asserted when ground is applied Recommended to be used as Engines On Off toggle switch Note All Digital Inputs are referenced to the ISAT 200 DIO GND
8. SkyTrac Website www skytrac ca Document Rev 01 019 DOC0334 Page 8 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 1 3 ISAT 200 System Components The following paragraphs describe the components of the ISAT 200 system 1 3 1 ISAT 200 The ISAT 200 is the primary component of the ISAT 200 System The system is comprised of a GPS Global Positioning System receiver an L Band transceiver specifically designed to communicate with the Iridium satellite system a Lithium ion battery which enables communications with the satellite system after airframe power shutdown and a battery charging system Control and interfacing are provided with a low power single board computer The ISAT 200 provides position reporting and messaging with global coverage in near real time ANTENNA DVI ISAT 200 7m Ei AIRCRAFT Ics lr e Figure 1 ISAT 200 System Block Diagram The ISAT 200 is the primary hardware component of a system designed to provide full duplex sat phone communication automatic message reporting 2 way messaging and other data transfers Data can be sent between an aircraft and any point in the world with internet access via the Iridium Low Earth Orbit LEO satellites Position reports and text messages from the aircraft can be displayed on any computer with internet access and SkyTrac software Position reporting intervals are user defined Base software displays current and hist
9. Summary The following table summarizes RTCA DO 160 Environmental Testing for the SkyTrac ISAT 200 Airborne Position Data Communicator and for the ITRAY 200 Table 12 Environmental Testing Summary ISAT 200 Part Numbers 101 200 01 101 200 03 ITRAY 200 Part Numbers 102 200 01 DO 160 Revision Mee seng Section Test Name 4 0 Temperature amp Altitude F1 F1 4 5 4 In Flight Loss of Cooling 5 0 Temperature Variation B B 6 0 Humidity A A 7 0 Operational Shock amp Crash Safety B B 8 0 Vibration SBM UG SBM UG 9 0 Explosion Proofness X X 10 0 Water Proofness A A 11 0 Fluids Susceptibility X X 12 0 Sand and Dust X X 13 0 Fungus Resistance A X 14 0 Salt Spray X X 15 0 Magnetic Effect Z Z 16 0 Power Input B BX 17 0 Voltage Spike B B 18 0 AF Susceptibility X X 19 0 Induced Signal Susceptibility X X 20 0 RF Susceptibility X X 21 0 RF Emissions L M 22 0 Lightning Induced Transient Susceptibility A A 23 0 Lightning Direct Effects A A 24 0 Icing A X 25 0 Electrostatic Discharge X X 26 0 Fire Flammability X X Document Rev 01 019 DOC0334 Restricted Proprietary and Confidential Information Page 17 of 48 SkyTrac Systems Ltd 2 7 Emissions Compliance The following table summarizes the ISAT 200 system s compliance for emissions Table 13 Emissions Compliance Entity Document Title US
10. These batteries however do contain recyclable materials and are accepted for recycling by your local battery recycling agency Please call 1 800 8 BATTERY for information on recycling your used Lithium ion battery or go to the RBRC website at www rbrc org for additional information Document Rev 01 019 DOC0334 Page 40 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 9 FIRMWARE UPDATES The ISAT 200 is equipped with a USB interface and a SD Card slot to enable firmware updates to the device Detailed instructions on how to update the firmware are included in the ISAT 200 User s Guide Refer to SkyTrac s website at www skytrac ca for a list of firmware updates available or contact SkyTrac Client Services IMPORTANT NOTE Depending on the time period between shipping of your unit and the physical installation at your location firmware upgrades may become available It is recommended that you check with SkyTrac Systems Client Services to confirm if any upgrades are available for your unit as part of the installation process Document Rev 01 019 DOC0334 Page 41 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 10 ISAT 200 HUMAN MACHINE INTERFACE 10 1 General This section provides a brief description of each of the ISAT 200 human machine interface components For more detailed information on each of these components refer to the ISAT 200 User s Guide
11. battery connector from the ISAT 200 4 Cut the cable ties securing the battery to the ISAT 200 battery cover begin careful not to damage the old battery case Recycle or safely dispose of the old battery 5 Mount the new battery lining up the battery ends with the battery mounting foam Make sure that the bump on the battery is not in contact with the cable ties and is parallel to the battery cover or it won t fit in the enclosure well 6 Install provided cable ties or equivalent to secure the battery to the mounting brackets Tighten the cable ties to 28 4in lbs 7 Visually inspect the battery installed to ensure secure installation 8 Connect the battery connector to the ISAT 200 9 Install the battery cover 10 If replacing STS0044 with STS0061 circle mod status D on the ISAT 200 serial number label with a permanent marker 11 Install the ISAT 200 in the ITRAY 200 12 Power up the ISAT 200 by applying aircraft power to the unit and wait 1 minute 13 Disconnect aircraft power from the ISAT 200 14 Verify that the battery operates Acceptable methods for doing this include verifying a Mains OFF report is received by the base station or observing the ISAT 200 display and verifying that the display operates briefly after the ISAT 200 main power is removed 15 All Panasonic Lithium ion batteries are classified by the federal government as non hazardous waste and are safe for disposal in the normal municipal waste stream
12. car s cigarette lighter e Do not place the batteries in or near fire or into direct sunlight When the battery becomes hot the built in safety equipment is activated preventing the battery from charging further and heating the battery can destroy the safety equipment and can cause additional heating breaking or ignition of the battery Do not continue charging the battery if it does not recharge within the specified charging time Doing so may cause the battery to become hot rupture or ignite This information is generally descriptive only and is not intended to make or imply any representation guarantee or warranty with respect to any cells and batteries Cell and battery designs specifications are subject to modification without notice Contact Panasonic for the latest information Panasonic JANUARY 2007 SAFETY PRECAUTIONS FOR LITHIUM ION BATTERY PACKS CONTINUED I CAUTION 3 The temperature range over which the battery can be charged is OG to 45 Charging the battery at temperatures outside of this range may cause the battery to become hot or to break Charging the battery outside of this temperature range may also harm the performance of the battery or reduce the battery s life expectancy 3 When Discharging the Battery WARNING 1 Do not discharge the battery using any device except for the specified device When the battery is used in devices aside from the specified device it ma
13. devices such as the CDU 300 Table 19 RS 485 Port 1 Descriptions ISAT 200R Description and recommended usage Bay A Pin Recommended port for connection to STS peripherals 23 RS 485 A Non Inverted Input Output Line 24 RS 485 B Inverted Input Output Line 29 RS 485 ground reference Table 20 RS 485 Port 2 Descriptions ISAT 200R Description and recommended usage Bay B Pin General purpose data port 43 RS 485 A Non Inverted Input Output Line 29 RS 485 B Inverted Input Output Line 81 RS 485 Y Non inverted Output 4 wire mode 82 RS 485 Z Inverted Output 4 wire mode 42 RS 485 ground reference Note RS 485 Port 2 shares some circuits with RS 232 Port 2 Only one of these ports can operate at the same time The functional port is selected via SkyWeb Note RS 485 4 wire mode is only available on ISAT 200R P N 101 200 03 Note RS 485 GND is isolated within the ISAT 200 system RS 485 GND needs to be connected to aircraft ground for reliable operation of the RS 485 databus 4 2 5 RS 232 Data ports These are the RS 232 ports used for sending and receiving serial binary data signals to and from peripheral devices Table 21 RS 232 Port 1 Descriptions ISAT 200R Description and recommended usage Bay A Pin Recommended port for connection to STS peripherals 26 TX Data out of ISAT 200 25 RX Data into ISAT 200 21 Serial data ground reference
14. electrolyte and damaged or discoloured PVC covering of the battery e If the ISAT 200 is not installed in an actively flying aircraft for a period of time that is greater than 3 months the battery must be electrically disconnected from the ISAT 200 unit and stored following the battery cell manufacturer s recommendations It is not recommended that the battery be stored for more than one year or loss of capacity will result e If the battery is completely depleted due to continued operation of the ISAT 200 unit out of the charge operational temperature range the battery should be fully charged within the correct temperature range This can be done by powering up the ISAT 200 unit within the battery charge operational temperature range for six hours or by using an approved desktop charger CAUTION If the battery has leaked electrolytes gets hot during charging or emits odours do not use the battery Contact SkyTrac Systems Ltd if this should occur 8 2 Maintenance Instructions The ISAT 200 Li ion battery capacity will decrease as the battery undergoes normal usage and aging The rate of capacity reduction depends greatly on the usage characteristics and operational temperature For this reason the battery must be monitored for replacement If the battery charge becomes critically low a battery alert message will be sent to the base station a low battery alert will be displayed on the ISAT 200 If the battery is installed in an ac
15. minutes High Temperature 70 C Operating Altitude Max Operating 55 000 ft H 5 0 in Size ISAT 200 W 3 6 in D 8 0 in H 4 41 in Size ITRAY 200 W 3 91 in D 11 8 in H 5 25 in Size ISAT 200 mounted in ITRAY 200 W 3 91 in D 12 1 in Weight ISAT 200 3 8 lb Weight ITRAY 200 1 0 Ib Weight ISAT 200 mounted in ITRAY 200 4 8lb Mounting Orientation The ISAT 200 mounts into the ITRAY 200 The ITRAY 200 can be mounted in any orientation Note 1 Refer to the Operation Limitations section of this document for information regarding battery operating limits Table 8 GPS Receiver Specifications Receiving Method 12 Channel continuous tracking receiver Acquisition time 39 4 seconds after power up cold start 2 seconds for re acquisition Position accuracy Less than 5 m 90 of the time Note 1 Resolution reported in position packets may be less to save transmission costs Table 9 Satellite Transceiver Specifications Operating frequency 1616 MHz to 1626 5 MHz RF Power Transmit max 7W Input Output Impedance 50 Q Duplexing Method TDD Multiplexing Method TDMA FDMA The ISAT 200 is not classified as Equipment known to have a high potential for interference in accordance with FAA Policy No ASW 2001 01 dated April 25 2002 Separate FADEC testing is not required for this installation Document Rev 01 019 DOC0334 Page 14 o
16. previous menu Document Rev 01 019 DOC0334 Page 33 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd To set the ring tone volume go to System gt Audio gt Ring Vol Select this item toggle through the choices Go Back 1 2 etc Selecting any number will set the Ringer Volume to that level Start by selecting 4 Go back and try to select a Ringtone If the selected ringtone is not heard increase the ringtone volume and try again Only nominal audio output impedance microphone bias microphone input range and ring tone need to be selected by the installer the rest can be configured by the user Audio configuration includes configuring the audio volume microphone gain side tone volume microphone bias microphone input range nominal audio output impedance and ring tone 5 3 System Configuration System configuration includes setting the registration number in the ITRAY 200 configuring position reporting information input operation and other parameters This configuration is performed within SkyTrac s Hardware Management section in SkyWeb Please refer to SkyWeb documentation available on the SkyTrac Website at www skytrac ca for more information on how to configure the unit Once the unit is configured use SkyWeb as instructed to verify correct configuration Document Rev 01 019 DOC0334 Page 34 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems L
17. the ITRAY 200R with the Configuration Module and ARINC connectors already installed the contacts and back shell Follow installation instructions as per sections 3 7 and 3 8 3 7 Installing ITRAY 200 The ISAT 200 is to be installed in an ITRAY 200 for operation Operation of the ISAT 200 outside the ITRAY 200 is not supported Note that the configuration module comes already installed on the ITRAY 200 1 Select a convenient location for installing the tray The tray can be mounted in any orientation Allow sufficient space at the rear of the tray for cable and connector routing 2 Attach the tray to the surface using four AN3 type bolts with lock nuts 3 Attach the cables to the ITRAY 200 as per an approved wiring diagram 3 8 Installing TSO Combination Antenna 3 8 1 General Notes The Iridium satellite serving a Short Burst Data call can literally be anywhere in orbit at a given moment in time For this reason it is imperative that the antenna be mounted outside as high as possible in a horizontal position on the aircraft attempting to achieve a 360 degree view of the sky with minimal obstructions The ISAT 200 uses the STS ISAT ANT combination active L1 GPS Passive Iridium low profile molded radome antenna This recommended system antenna is only available directly from SkyTrac Systems Ltd and is permanently installed on the outside of the aircraft If required please contact SkyTrac Systems to discuss the feasibility o
18. without notice Contact Panasonic for the latest information Panasonic JANUARY 2007 NOTES AND PRECAUTIONS CONTINUED 3 Equipment Design 1 Installing Battery Packs in the Equipment To avoid damage to the battery pack make sure that the battery pack is positioned away from heat sources in the equipment or in the battery charger 2 Mechanisms to Prevent Dropping Be sure to use a battery pack lock mechanism to prevent the battery pack from being ejected when the equipment is dropped or receives a sudden impact 3 Preventing Short Circuits and Reversed Connections Use a terminal structure that makes it unlikely that the terminals will be shorted by metallic necklaces clips hairpins etc Structure the battery and the terminals to the battery in sub ta way that the battery pack cannot be put in backwards when installed in the charger or the equipment 4 Inclusion in Other Equipment If the battery is built into other equipment use caution to strictly avoid designing airtight battery compartments 5 Terminal Materials in the External Equipment Use materials that are highly resistant to corrosion such as nickel or nickel coated copper If contact resistance is an issue we recommend that you use contact plating such as gold plating on the terminals 4 Storing the Batteries The batteries should be stored at room temperature charged to about 30 to 50 of capacity We recommend that batteries be charged about once per year
19. your battery please follow the instructions below 1 Remove the eight screws on the side panel of the ISAT 200 and then remove the battery cover panel as shown in Figure 2 below 2 Connect the battery to the power board Insert the 4 pin battery cable connector into the battery connector J2 for 101 200 03 J1 for 101 200 01 and push until it is securely in place 3 Reinstall the battery cover panel with the eight screws that were previously removed Figure 2 ISAT 200 Side Panel Detail For battery replacement and maintenance refer to section 8 Maintenance and Continued Airworthiness CAUTION Use only an approved STS battery Using an unapproved battery will damage your ISAT 200 and void the warranty 3 10 Installing ISAT 200 into ITRAY 200 1 Slide the ISAT 200 into the tray from the front until it is Snug 2 Fasten the front hold down tab using the provided socket head cap screws lock washers and washers Tighten the bolts until the split ring is compressed and then tighten at least another Lo turn Document Rev 01 019 DOC0334 Page 23 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 4 ELECTRICAL INSTALLATION 4 1 General This section contains the information required to complete the electrical connections in an ISAT 200 system installation including diagrams and tables that call out and list the contact locations of the connectors used in the ins
20. 02 101 200 04 and ITRAY 200S 102 200 02 have been discontinued Table 2 ISAT 200 System Components Type Part Num Description Compatibility d STS0044 or 101 200 01 Li ion 7 2V STS0061 2 Cell Li lon Battery Pack 101 200 03 Mii 101 200 01 STS ISAT ANT STS ISAT ANT SkyTrac TSO Iridium GPS Antenna 101 200 03 Document Rev 01 019 DOC0334 Page 11 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 1 3 6 ISAT 200 Supported Peripheral Devices The ISAT 200 supports the following SkyTrac Systems control head product series DVI 250C and DVI 250A CDP 250G and CDP 250C Combination of the CDP 250 and DVI 250 DVI 300C and DVI 300A CDP 300G and CDP 300C Combination of the CDP 300 and DVI 300 It is recommended that a DVI 300 and CDP 300 be used in conjunction to make full use of the ISAT 200 features Additional peripherals may become available from time to time Please go to www skytrac ca or contact SkyTrac Client Services for more information Table 3 ISAT 200 Supported Peripherals Type Part Number Description Compatibility DVI 250C Mod A STS0009 DVI 250 NVIS Friendly DVI 250A Mod A STS0010 DVI 250 NVIS Compatible DVI 250CP Mod A STS0022 DVI 250 NVIS Friendly Push Button DVI 250AP Mod A STS0023 DVI 250 NVIS Compatible Push Button CDP 250G Mod A STS0014 CDP 250 Commercial CDP 250C Mod A STS0015 CDP 250 NVIS Friendly All CDU
21. 250s are comprised of a combination of the CDU 250 above DVI 250 and CDP 250 models 101 200 01 DVI 300C 105 300 01 DVI 300 NVIS Friendly 101 200 03 DVI 300A 105 300 02 DVI 300 NVIS Compatible DVI 300CP 105 300 03 DVI 300 NVIS Friendly Push Button DVI 300AP 105 300 04 DVI 300 NVIS Compatible Push Button CDP 300G 104 300 01 CDP 300 Commercial CDP 300C 104 300 02 CDP 300 NVIS Friendly CDU 300 All CDU 300s are comprised of a combination of the above DVI 300 and CDP 300 models Note Please refer to the latest version of the List of Approved Embedded Software DOC0444 for software version requirements for peripherals This document can be obtained at www skytrac ca or your program manager Note The CDP 250 and DVI 250 require a special version of firmware to communicate with the ISAT 200 Contact SkyTrac Client Services for more information Document Rev 01 019 DOC0334 Page 12 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 2 SYSTEM SPECIFICATIONS 2 1 General This section contains tables that list the physical and electrical requirements and specifications of each component in the ISAT 200 system 2 2 Power Requirements for the ISAT 200 System Table 4 Power Requirements Component Power Requirements ISAT 200 Input Voltage 10 to 32 VDC 28 VDC nominal Average Power 14 W typical 25
22. CDP 300 CDU 300 to configure the system If using a peripheral please refer to the peripheral installation manual for more details Please follow the below instructions if using the ISAT 200 menu for audio configuration 5 2 1 Installer Audio Configuration ltems Audio Input Level The audio input level can be selected to a low range designed to connect to microphones or to a high range designed to accept up to 1 4V RMS To select the audio input level use the ISAT 200 menu System gt Audio gt Audio In Select Lo Level for low input range for microphones or Hi Level for high input range up to 1 4VRMS Microphone DC Bias Microphone DC Bias can be selected as either ON or OFF via the ISAT 200 Menu Use the System gt Audio gt Mic Bias to toggle the DC Bias ON or No Bias OFF Setting Microphone Gain Setup To set the amount of gain on the microphone input selection use the ISAT 200 menu System gt Audio gt Mic Gain and select either 6db or 18db Ring Tone One of five ring tones can be selected via menus on either the ISAT or the peripheral Connect your headset to the ISAT so that you can listen to the tones To select a ring tone go to the System gt Audio gt Ringtone menu Toggling through the choices will display 1 then 2 etc As each number is displayed the associated Ring Tone will sound for one second in the headset Select the desired ring tone Select Go Back to return to the
23. Check all ISAT 200 digital inputs that are required and verify that each input gives the expected result The digital inputs can be checked from the ISAT 200 Menu as follows a Scroll to System gt Test gt Dig I P b A six digit binary number is displayed for example 001001 The left most digit represents digital input 1 while the right most digit represents digital input 6 c Activate one of the digital inputs and check that the appropriate digit is changed from O to 1 De activate the input and check that the same digit changed from 1 to 0 Note that the logic may be inverted from the intended function This can be handled during the remote configuration of the ISAT 200 d Repeat step c for each digital input used in the ISAT 200 installation Check all ISAT 200 digital outputs that are required and verify that each output gives the expected result The digital outpus can be checked from the ISAT 200 menu as follows a Scroll to System gt Test gt Output b The menu will scroll through each digital output and toggle the value from deactivated to activated and back to deactivated c Verify that activating the digital output has the desired result Document Rev 01 019 DOC0334 Page 35 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 7 Check all ISAT 200 analog inputs that are required and verify that each input gives the expected result The analog inputs can be checked from the
24. FCC 47 Code of Federal Regulations Part 25 FCC ID Q639522B US FCC Federal Regulations Part 15 ETSI EN 301 489 The 9522B Iridium modem is designed to comply with the standards for Radio Emissions Compliance Electromagnetic Compatibility and AC Safety in the United States European Union and Canada IMPORTANT To comply with FCC RF exposure requirements a minimum separation of 20 cm is required between the antenna and all persons Document Rev 01 019 DOC0334 Page 18 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 3 MECHANICAL INSTALLATION 3 1 General This section contains procedures for the mechanical installation of the ISAT 200 system components It includes unpacking instructions a table listing the weight of each component and instructions for completing the physical installation of the ISAT 200 the ITRAY 200 and the TSO Combination Antenna The ISAT 200 installation package contains a combination GPS Iridium antenna The antenna must be placed in a location that has a clear view of the sky The ISAT 200 must receive GPS signals via the antenna to enable the determination of its present position and communicate send transmit with the Iridium LEO satellite system In order to view position data a Windows based PC is required at the base location Please see www skytrac ca for software options 3 2 Unpacking and Inspecting the System Components 1 Check the it
25. GPS Passive Iridium antenna Note Consider maximum antenna coax lengths and minimum distance between existing GPS antennas and the ISAT 200 antenna when determining an install location Note If ISAT 200 is to be installed near an active INMARSAT terminal or if the aircraft that the ISAT 200 is installed in operates near an active INMARSAT terminal please see Appendix A Install and secure the ITRAY 200 Install the TSO combination antenna PN STS ISAT ANT Route the coax cables for Iridium and GPS antenna signals to the ISAT 200 combination antenna Install and or connect the battery in the ISAT 200 Install and secure the ISAT 200 into the ITRAY 200 IMPORTANT NOTICE All system interconnect cables must be connected before power is applied to the system 3 5 ISAT 200 Component Weights The following table gives the weight for each component of the ISAT 200 system Table 14 Component Weights Component Weight ISAT 200R 3 8 Ib ITRAY 200R 1 0 Ib Installation Materials 0 2 lb TSO Combination Antenna PN STS ISAT ANT 0 5 lb 2 Cell Li lon Battery Pack STS0044 0 215 lb STS0061 0 22 Ib Document Rev 01 019 DOC0334 Page 20 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 3 6 Installation Materials 3 6 1 PN 102 200 01 Installation Kit for the ISAT 200R The ISAT 200R is installed using the Installation Kit PN 102 200 01 the kit contains
26. ISAT 200 menu as follows a Scroll to System gt Test gt Ana UP b The menu will scroll through each analog input and display the input voltage c Change one of the analog inputs and check that the analog input value increases or decreases appropriately d Repeat step c for each analog input used in the ISAT 200 installation 8 If an audio interface is installed place and receive a phone call and ensure that all audio is clear and of an appropriate volume lt is recommended that this step be performed with the engines on so that a typical level of background noise is present 9 Check that any installed peripheral devices are able to detect and communicate with the ISAT 200 Refer to the peripherals installation manual and user guide for instructions specific to the device 6 3 EMI Test Please refer to ISAT 200 System EMI RFI Test Template DOC0478 latest revision for testing procedures The purpose of the EMI test report is to verify that the operation of the ISAT 200 does not interfere with basic aircraft systems and avionics Most of the EMI tests can be accomplished on the ground however in some cases flight testing is required If the aircraft is approved for IFR operations then it is mandatory that interference between the ISAT 200 and the approach aids be checked in flight The EMI test includes the following steps and system checks e Operate the unit until at least 10 position reports are sent e The existin
27. OS eo VW SKYTRAC YOUR SATCOM TECHNOLOGY PARTNER ISAT 200 Installation Manual DOC0334 Document Revision 01 019 Applies to PN 101 200 01 101 200 03 ISAT 200 102 200 01 ITRAY 200 July 27 2012 SkyTrac Systems Ltd 200 170 Rutland Road North Kelowna BC Canada Tel 1 250 765 2393 Fax 1 250 765 3767 Web www skytrac ca Email support Qskytrac ca Copyright O 2012 SkyTrac Systems Ltd All rights reserved SkyTrac Systems Ltd Document Revision History Rev ECO Description Date Author 01 000 164 Initial Release Feb 10 2009 P Bennett T Ratch 001 168 Updates for initial production release May 4 2009 A Parker 01 002 181 Corrected unit weight June 25 2009 T Ratch 01 003 182 Post conformity updates June 29 2009 J Van 01 004 187 Changed DO 160E category July 17 2009 A Parker 01 005 188 Correct CDP 300 Part number table removed ISAT vertical install spec July 21 2009 D McMahon 01 006 189 Changed operational temperature spec Made updates to Audio Config Items July 23 2009 A Parker 01 007 234 Update warranty statement to exclude the battery shipped with the ISAT 200 added note about checking digital input status and notes about alternate coax connector Nov 4 2009 A Parker 01 008 253 Added installation f
28. SAT 200 System Components coccccccccococcnonoccnonncononcnnnnn nano cnn nc crac anna n nan nnna cnn 9 A E EE 9 A MAA eee SE 10 1 3 3 AM A a meet renee er reer A A reeree errr 10 1 3 4 ISAT 200 Installation Componente eee eeeeaeeeeneeceeeeeceaeeeeaaeseeneeseaeeesaeeeeaeeseeeeeeaas 10 AE EE En Mee 11 1 3 6 ISAT 200 Supported Peripheral Devices ooonoocinncccnncconnccnnncnnncncnncccnnnn cnn n cnn nn cnn nc aran nnnn nn nnnncnns 12 2 System Specifications miii iii 13 2 1 A RRA 13 2 2 Power Requirements for the ISAT 200 Gvstem nnet 13 2 3 Audioteca 13 2 4 Digital and Analogue e cnn ties 13 2 5 Physical Sp cifeatidns i passet uden feiende rad aras 14 2 6 Safety Compliance arras ude mumier navel cantzeuses mmndedeinidkardaspesepet ine aiian 16 2 6 1 Environmental Test Summary c oooonccinncccnncccnonnnnnnonnnnnnccnncn conca rare 17 2 7 Emissions Compliance scooter dada 18 3 Mechanical Installation srernnannvennnnnnvennnnnnvennnnnnvnnnnnnnnennnnnnnennnnnnnnnnnnnnnennnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 19 3 1 General uland AA ER TN TA 19 3 2 Unpacking and Inspecting the System Component ooocccnccccnocccononananncononcnnonn cnn non nnannc cnn can arrancan 19 3 3 Installation LIMITAIONS ua AA A E eee ee id 19 3 4 Main Installation RRE 20 3 5 ISAT 200 Component Weights AA 20 3 6 Installation Materials ooo Did 21 3 6 1 PN 102 200 01 Installation Kit for the ISAT 200R oooocccccccononononononenoneninininininininininananananano
29. W maximum 2 3 Audio Interface Table 5 Audio Interface Specifications Audio Output 150 mW minimum into 600 or 300 ohm Side Tone Software Enabled Microphone Carbon or Equivalent Microphone Input 0 007 Vrms to 1 4 Vrms maximum Microphone Input Impedance 1Kohms Microphone Excitation Software Enabled Bias 10 VDC maximum Protection Audio output short circuit protected 2 4 Digital and Analogue l Os Table 6 Digital and Analog I Os Ground Seeking Digital Inputs 100 Ohms max for ground state Maximum 35 VDC Voltage Seeking Digital Input gt 5 Volts for logic high Maximum 40 VDC Analogue Inputs Maximum 40 VDC Current Sinking Outputs Maximum 36 VDC 200 mA Aux Power Output 6 Volts 0 8 A output RS 232 Ports Meets requirements of TIA ElA 232 F standard TX maximum 13 2 V RX maximum 25V RS 485 Ports Meets requirements of TIA ElA 485 A standard Extended Common Mode 20V to 25 V Fail safe receiver Open circuit short circuit bus idle Document Rev 01 019 DOC0334 Page 13 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 2 5 Physical Specifications Table 7 ISAT 200 and ITRAY 200 Physical Specifications Operating Temperature 20 C to 55 C Short Term 30 minutes Low Temperature 40 C Short Term 30
30. ards of airworthiness for the system in question For example it is permissible for a VER certified GPS to lose navigation capability under certain conditions providing that it recovers properly and promptly but it is not permissible for an IFR Approach certified GPS to be affected in the same way A complete discussion of all the standards of airworthiness to be applied in assessing EMI effects is beyond the scope of this document Document Rev 01 019 DOC0334 Page 37 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 7 AIRWORTHINESS LIMITATIONS 7 1 Installation Limitations As per FAA Policy No ASW 2001 01 dated April 25 2002 the antenna must not be installed 0 5 meters or less from a FADEC system 7 2 Operation Limitations GPS information provided by the ISAT 200 is not intended for navigational purposes Operating the battery pack below 10 results in reduced performance The ISAT 200 field replaceable Li ion battery has a charging temperature range from 0 degrees Celsius to 45 degrees Celsius A unique user notification will be sent to the ground user when the ISAT 200 battery voltage becomes low If the battery is not charged the ISAT 200 will not be able to perform its battery only power requirements please see the SkyWeb Administrator s Guide for details Use only the ISAT 200 or chargers approved by SkyTrac Systems to charge the battery pack Use of other chargers may damage the batter
31. ble 21 RS 232 Port 1 DescriptiOnS rmsrrnnnnvnnnnnnnnnnvnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 29 Table 22 RS 232 Port 2 DescriptiOnS mmsernnnavnnnnnvnnnnvnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 30 Table 23 Ethernet Port Descriptions rnnnnnvnnnnnnnvnnnnnnnvnnnnnnnvnnennnnnnnnnnnnvnnennnnnnnennnnnnnnnnnnnnnnnnnnnnnennnnnnnnnnnnnnnnenr 30 Table 24 Analogue Input Descriptions n ssrernnnnnnvvnnnnnnvnnnnnnnvvnnnnnnvnnennnnnnennnnvnnennnnnnnnennnnnnnnnnnnnnnnnnnnnnnennnnnnnenn 30 Table 25 Auxiliary Power Description rrnnssvnnnnnnnvnnnnnnnvnnnnnnnvnnnnnnnvnnnnnnnvnnnnnnnennnnnnnennnnnnnvennnnnnennnnnnnvennnnnneenennn 31 Table 26 External Power Input Description nrsasvernnnnnvennnnnnvnnnnnnnvnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnennnnnnnennnnnnnnnnnnnnenr 31 Table 27 Audio Line DescriptiOn r rrsseernnnnnvennnnnnvnnnnnnnvnnnnnnnvnnnnnnnvnnnnnnnnnnnnnnnnnnennnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennn 31 Table 28 ITRAY 200 Communication Line Description rrssvrnnnvvnnnnvnnnnnvnnnnnnnnnvnnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnn 31 List of Figures Figure 1 ISAT 200 System Block Diagram rrrvrnnnnvnnnnnnnnnvvnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennnnnnnnnnnnnnn 9 Figure 2 ISAT 200 Side Panel Detail rrnnrnnnnnnnnnnvennnnvnnnnnnnnnnvnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnne
32. ems in the shipment against those listed on the shipping invoice to ensure that all items have been received H any items are missing contact SkyTrac Client Services 2 Carefully remove each item from its individual packaging 3 Inspect each item for damage that may have been incurred during shipping In case it is necessary to submit a damage claim save the shipping container to help verify the claim 4 After all items have been unpacked it is suggested that you save the containers and packaging materials in case H becomes necessary to reship an item Verify and record the IMEI and the serial number of the ISAT 200 3 3 Installation Limitations The following installation regulations must be adhered to e The ISAT 200 must be installed using an ITRAY 200 P N 102 200 01 mounted securely CAUTION As per FAA Policy No ASW 2001 01 dated April 25 2002 The antenna must not be installed 0 5 meters or less from a FADEC system Document Rev 01 019 DOC0334 Page 19 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 3 4 Main Installation Tasks The main tasks for this installation are listed below 1 Unpack and inspect the system components Check the contents of the installation kit against the parts list on the Installation Kit Package and verify that all components are included and were not damaged during shipping Determine the approximate location of the ISAT 200 and combination
33. ennnnnnvnnnnnnnneenr 15 Table 11 LI ION Battery Specifications rrnarnnnnvnnnnvvnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 15 Table 12 Environmental Testing Summary rsssnnnnvnnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 17 Table 13 Emissions ComplianCe nsssnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 18 Table 14 Component Weights nce 0iccctc cceciece sensi ce ecectsccteevec seenecedceccedteed eeetaeenteuseoceee stad ceccurtonesdecbvesaserteseceeole 20 Table 15 ARINC 404 Bay B pin descriptions rrravvnnnnvnnnnnvnnnnvnnnnvennnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 26 Table 16 ARINC 404 Bay A pin descriptions rrrsvrnnnnvnnnnnvnnnnvnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 27 Table 17 Digital Ground Seeking Input Descriptions rrsarnnnnvnnnnvennnnnnnnnnnnnnvnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 28 Table 18 Digital Voltage Seeking Input Descriptions rrssrnnnnvnnnnvvnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnn 28 Table 19 RS 485 Port 1 DescriptiOnS rrarrnnnnvnnnnnvnnnnvnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 29 Table 20 RS 485 Port 2 DescriptiOnS rmsernnnavnnnnnvnnnnvnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 29 Ta
34. ent Rev 01 019 DOC0334 Page 31 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 4 3 Example Installation drawings and BOM Approved installation drawings from the appropriate STC should be used for installation of the ISAT 200 System Please refer to the ISAT 200 System Installation Reference Drawings DOC0461 for reference when an STC is not applicable 4 3 1 ISAT 200 Installation Wiring Diagram Notes The following notes pertain in general to the ISAT 200 Installation Wiring Diagram Illustrations IMPORTANT NOTICE All system interconnect cables must be connected before power is applied to the system All signal and power shield continuity must be individually maintained through bulkhead disconnects Please refer to the ISAT 200 System Installation Reference Drawings or STC drawings for additional installation notes Document Rev 01 019 DOC0334 Page 32 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 5 CONFIGURATION OF THE ISAT 200 5 1 General This section contains instructions for configuring the ISAT 200 5 2 Installation Configuration A number of audio configuration items need to be done These are divided into two sections those that need to be done by the installer and those than can be done by the user This section needs to be completed if audio installation is to be done The installer can use the ISAT 200 menu system or the DVI 300
35. f 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd Table 10 TSO Combination Antenna Specifications PN STS ISAT ANT Description Active L1 GPS Passive Iridium Antenna low profile moulded radome Height 0 721 in Length 5 026 in Width 2 0 in Weight 8 0 oz Voltage 2 8 to 28 0 VDC 50 mA max Gain GPS antenna 32 dB min Table 11 Li ion Battery Specifications STS0061 STS0044 Description 2 cell Li ion battery pack with built in 2 cell Li ion battery pack with built in protection circuitry protection circuitry Capacity 7 2V nominal 2700 mAh 7 2V nominal 2250 mAh Operation 10C to 60T 200 to 60T Charging OG to 45 0 OG to 450 Storage 20 to 600C 20 to 60 Dimensions 5 2 in x 0 90 in x 0 75 in 5 2 in x 0 90 in x 0 75 in Weight 0 22 Ib 0 215 lb Connector MOLEX 43025 0400 MOLEX 43025 0400 Over Discharge Protection 2 32 Volts cell 2 2 Volts cell Over Charge Protection 4 325 Volts cell 4 375 Volts cell Over Current Protection 6 5A max 7A max Over Temperature Protection Built in thermal protection circuit disables cell in case of overheating Built in thermal protection circuit disables cell in case of overheating Note 1 Operating the battery pack below 10 C results in reduced performance Operating the battery pack above 60 C may cause reduced life and capacit
36. f performance and a shortened life expectancy I CAUTION If the device is to be used by small children the caregiver should explain the contents of the user s manual to the children The caregiver should provide adequate supervision to ensure that the device is being used as explained in the user s manual When the battery is worn out insulate the terminals with adhesive tape or similar materials before disposal Immediately discontinue use of the battery if while using charging or storing the battery the battery emits an unusual smell feels hot changes color changes shape or appears abnormal in any other way Contact your sales location or Panasonic if any of these problems are observed Do not place the batteries in microwave ovens high pressure containers or on induction cookware In the event that the battery leaks and the fluid gets into one s eye do not rub the eye Rinse well with water and immediately seek medical care If left untreated the battery fluid could cause damage to the eye 2 While Charging WARNING Be sure to follow the rules listed below while charging the battery Failure to do so may cause the battery to become hot rupture or ignite and cause serious injury e When charging the battery either use a specified battery charger or otherwise ensure that the battery charging conditions specified by Panasonic are met e Do not attach the batteries to a power supply plug or directly to a
37. f using an alternate antenna Document Rev 01 019 DOC0334 Page 21 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 3 8 2 Antenna Installation Instructions The combination antenna must be installed at least three feet away from any other GPS antenna lt is imperative that the antenna be mounted outside as high as possible in a horizontal position on the aircraft attempting to achieve a 360 degree view of the sky with minimal obstructions IMPORTANT NOTE This antenna uses an SMA connector for the GPS jack and TNC connectors for the L Band or Iridium jack Immediate damage will occur to the ISAT 200 if either cable is connected to the wrong coax pin on the ITRAY 200 connector The use of RG 400 low loss coaxial cable restricts the maximum length of the cable to 18 ft If a longer run is required use lower loss coax cable such as EMTEQ PFLX240 500 recommended or ECS 311501 and refer to manufacturer s specifications for attenuation at 1 6 GHz Attenuation of equal to or less than 3 dB is required The bond between the airframe and the antenna needs to be 10 milliohms or less Prepare the mounting location by drilling holes in the aircraft skin or through a mounting plate Use a doubler plate of 4 x 6 inches if the antenna is installed on a non metallic aircraft surface to create a ground plane The plate must have an electrical connection to the antenna ground Installation of an antenna on the a
38. g on board GPS should be operational and navigating with at least the minimum complement of satellites e The VHF Comm should be set to commonly used frequencies with the squelch open e VOR DME receivers should be selected for display e f possible set up a DME ramp test set on the frequencies indicated and adjust the output until the flags are out of view e The transponder and encoder should be monitored with ramp test equipment e Set the output of the transponder test set to 3 db above the output necessary to achieve 90 reply e f possible set the ADF to a nearby navigation station List the power plant fuel and other electric instruments on the EMI RFI Test Report and note any anomalies that occur while transmitting Assess the results If the aircraft is equipped with an autopilot or stability augmentation system then test fly the aircraft and verify that operation of the ISAT 200 unit does not have adverse effects on these systems After checking for gross effects at a safe altitude fly an approach with each of the different navigation systems coupled to the autopilot ILS GPS ETC and look for any anomalies Document Rev 01 019 DOC0334 Page 36 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd If the installed system passes all of the applicable EMI tests then no further action is required If interference is observed then the interference must be assessed against the appropriate stand
39. ircraft should be performed only as defined by the aircraft manufacturer or in accordance with TC or FAA approved engineering data Special caution must be observed when installing antennae in pressurized aircraft Note The combination antenna includes a rubber seal that must be properly installed into the groove on the underside of the antenna prior to mounting the antenna This seal acts as an environmental seal from the outside atmosphere Any connections that are not protected from the outside atmosphere by the rubber antenna seal should have an environmental seal applied to them during installation Note The ARINC connectors supplied on the ITRAY 200R use size 5 coax contacts The contacts supplied in the installation kit are for RG400 type cable SkyTrac Systems recommends the use of Emteq PFLX240 500 coax cable with a short pigtail using BNC connectors and RG400 coax cable for longer runs If using another cable type then an adaptor cable may need to be built Additional regulatory approval will be required if the cable or connectors used are not specified in the applicable STC Document Rev 01 019 DOC0334 Page 22 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 3 9 Connecting the Battery to the ISAT 200 The ISAT 200 is shipped with the battery mounted but not connected to the power board This is to prevent the battery from being depleted before the ISAT 200 is installed in an aircraft To connect
40. n 23 Figure 3 ARINC404 Bay B 106 pin out drawing rnnavnnnnnnnnnvvnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnenn 25 Figure 4 ARINC404 Bay A 30 pin out drawing rrssvvnnnavnnnnvvnnnvnnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnner 25 Document Rev 01 019 DOC0334 Page 6 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 1 GENERAL 1 1 Introduction This manual contains information and instructions required to install the ISAT 200 Position Data Communicator System and more specifically its primary component the ISAT 200 Transceiver 1 2 Contents This manual contains procedures and other information for installing the ISAT 200 system It is divided into the following sections Section 1 General This section contains a product overview and an overview of the contents of this manual It also lists the ISAT 200 system components for which installation procedures are included Section 2 System Specifications This section contains tables that list the power requirements and electrical specifications for the components of the ISAT 200 system Section 3 Mechanical Installation This section contains the procedures for the physical installation of the ISAT 200 system components Section 4 Electrical Installation This section contains the information needed to complete the electrical connections in an ISAT 200 system Section 5
41. n Items sense caaeeesaaeseeeeeseaeeesaeeeeeeeeeeees 33 5 3 System Configuration asii deci 34 6 Post Installation TESTS cena 35 6 1 General iaa ad 35 6 2 Function Pesticidas ee aint AAA A ne es 35 6 3 EMIL TOS Eo A A AA AA nd AA 36 7 Airworthiness Limitations snnnnnnnvennnnnnvnnnnnnnvvnnnnnnvnnnnnnnvnnnnnnnvennnnnnvennnnnnvennnnnnvennnnnnvennnnnneennnnnneennnnnneenennn 38 7 1 fe Elei Ru EE 38 7 2 Operation LIMITA NEE 38 8 Maintenance and Continued Airworthiness rrnsvrnnnvnnnnnvnnnnnnnnnvnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 39 8 1 elle Bil eu kateb kdvst ude dvd bad 39 8 2 Maintenance INStructiOns sneinen anaidi aaa tai danda aaike i aeeiiaii iiaii 39 8 2 1 Battery Replacement Instructions ooonnocononccccnonoccccnononccinnanccnonnnnnncnnnoncnn canon nn cnn nn nc cnn nn cc cnn nnccnnns 40 9 A ENEE aa aaa a a aR aa 41 10 ISAT 200 Human Machine Interface rnarnnnnvnnnnvnnnnnvnnnnnnnnnnvnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 42 10 1 Generali ai a da geet ia io at 42 10 27 Piep EE 42 WOES 4 BED snr AN eine 42 dr EN Cut WEE 42 10 5 Ambient Light SENSO cuco ds 42 10 6 USB Progranmiming Port otiiia beer ets dade 42 VOLT SD C rdSlok ananas um draget dar a 42 11 APPENDICES aia 43 11 1 Appendix A Causes of RF Interference oooonccccnccononcconocanonoccnoncnnnonn nano cnn ncc narran rre 43 11 2 Appendix B Battery PrecautiONS comcoccnnnnncccnnnnncccnnoncccn
42. nananess 21 3 7 Installing ITRAY200 ET 21 3 8 Installing TSO Combination Antenna ccccccecceceeeeeeceeeeeceeeeeeaaeeeeaeeseeeeceaeeesaaeeseeeeseaeeesaeeeeneeeeenees 21 3 81 General NOTES ar aaan SENAT d se E 21 3 8 2 Antenna Installation Instructions coerenta Ea EEE AEEA EEE ORRA 22 3 9 Connecting the Battery to fhelGhf 200 nn nano nn nan crac narra narran 23 3 10 Installing MT ME HL Bit BH TUTE 23 4 ElectricalInstallation 20 dai incre 24 4 1 A E NN 24 4 2 ECA aa cano Sa 24 2231 IECH ege ege eege Eed Eder tios 25 4 2 2 Digital Ground Seeking Inputs nn n naar cnn rca 28 4 2 3 Digital Voltage Seeking Inputs ooocnnccnnnnccnnnncnnnocnnncccnnccnnnrnnn anna nn cnn nr 28 4 2 4 RS 485 Data POMS it tas A det ae en A 29 4 25 RS 232 Data poms a cet ain ea aries da a enn 29 e E El EE 20 e ue te CHE 20 4 2 8 Auxiliary ower Oufpo0t ugeet da N EN 4 29 NR EH Power Input A WEE 31 4 2 10 Le e NEE 31 4 2 11 ITRAY 200 Communication Lines 31 4 3 Example Installation drawings and BOMM nnet 32 4 3 1 ISAT 200 Installation Wiring Diagram Notes 32 Document Rev 01 019 DOC0334 Page 4 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 5 Configuration of the ISAT 200 rrrsvvrnnnvnnnnnvnnnnnnnnnvnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnenn 33 5 1 General A E NN 33 5 2 Installation Configuration wwe naa a rai 33 5 2 1 Installer Audio Configuratio
43. nnnnncnnnnnnecnn canse cnn E EOE cnn E 44 Document Rev 01 019 DOC0334 Page 5 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd List of Tables Table 1 ISAT 200 Models E 11 Table 2 ISAT 200 System Components rrnnnnvnnnnnnnnnvnnnnnvnnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennnnnnnnnnnnnnnnnnnnn 11 Table 3 ISAT 200 Supported PeripheralS rrrassvnnnnvnnnnvnnnnnvnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 12 Table 4 Power Requirements s errnnnnvvnennnnvnnnnnnnvnnnnnnnvnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennnnnnnen 13 Table 5 Audio Interface Specifications rrnsrnnnnvnnnnvvnnnnvnnnnnnnnnnnnnnnvennnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennnnnn 13 Table 6 Digital and Analog OS errassvrnnnvnnnnnvnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnennnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 13 Table 7 ISAT 200 and ITRAY 200 Physical SpecificatiOnsS rrrsvrnnnnvnnnnnvnnnnvnnnnvnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 14 Table 8 GPS Receiver SpecificatiOnS rrrssrrnnnnnnnvvnnnnvnnnnnnnnnnvnnnnvennnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennnnnnnnnnnnnnnnnnnnn 14 Table 9 Satellite Transceiver Specifications rrrnvrnnnnvnnnnnnnnnnvnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn 14 Table 10 TSO Combination Antenna Specifications PN STS ISAT ANT ererrnnvvvnnnnnvnv
44. onnect 80 ADC5 Analogue Input 5 81 RS 485_Y2 RS485 port 2 non inverted line 4 wire mode 82 RS 485_Z2 RS485 port 2 inverted line 4 wire mode 83 106 RESERVED Reserved do not connect RS485 4 Wire Mode is only available on ISAT 200R P N 101 200 03 RS 485_GND2 is isolated within the ISAT 200 system RS 485 GND2 needs to be connected to aircraft ground for reliable operation of the RS 485 databus Document Rev 01 019 DOC0334 Restricted Proprietary and Confidential Information Page 26 of 48 SkyTrac Systems Ltd Table 16 ARINC 404 Bay A pin descriptions ARINC Pin Pin Names Description 1 SPI MISO Reserved for CM do not connect 2 GND Reserved for CM do not connect 3 3V3SW Reserved for CM do not connect 4 DI4 Digital Input 4 5 DI2 Digital Input 2 6 DI1 Digital Input 1 7 TRAY MOSI Reserved for CM do not connect 8 TRAY SCLK Reserved for CM do not connect 9 SPI TRAY CS Reserved for CM do not connect 10 DIO GND Digital I O Ground 11 DI6 Digital Input 12 DO1 Digital Output 1 13 AUX PWR Auxiliary Power Output 14 AUX GND Auxiliary GND 15 PWR External Power Input 28V 16 GND 28V return ground 17 CH GND Chassis Ground 18 CH GND Chassis Ground 19 CH GND Chassis Ground 20 CH GND Chassis Ground 21 S1 GND Serial 1 Ground 22 52 GND Serial 2 Ground 23 RS485 ATI RS485 port 1 non inverted line 24
45. orical position data including latitude longitude GPS time relative position to a known way point ground speed altitude and heading in tabular format and on a map Airtime flight time ETA distance traveled time elapsed and other flight data is also displayed for instant viewing Flight reports can also be generated by unit and time frame i e airtime flight time per day week month Document Rev 01 019 DOC0334 Page 9 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd Operationally the ISAT system can compliment flight following requirements for commercial operators and provide vital position data and messaging services to those operators conducting flight activities in remote areas The unit may be reprogrammed via the USB port or the SD Card Interface in order to provide new feature sets as they become available The eight character display and user friendly menu system is provided to enable troubleshooting with minimal reference to the manual required The unit supports up to two RS 232 serial ports up to two RS 485 ports Ethernet three analog inputs and six digital inputs The ISAT 200 supports sat phone integration into aircraft standard audio equipment 1 3 2 ITRAY 200 The ISAT 200 is mounted in an ITRAY 200 quick disconnect chassis The ITRAY 200 makes for easier replacement and maintenance of the ISAT 200 The ITRAY 200 onboard Configuration Module retains the configuration info
46. ridium unit s ability to properly maintain a quality connection with the Iridium satellite constellation INMARSAT terminals are often found in the same locations as Iridium subscribers generally airports and harbors especially aboard naval vessels In relation to the Iridium unit s antenna the location of the INMARSAT units antenna plays a significant role in determining the degree of signal degradation an Iridium subscriber will experience All Iridium units are susceptible to this interference regardless of the type of antenna being used Susceptibility to interference from an INMARSAT terminal applies to all Iridium end user products 9500 and 9505 equipment including the L Band Transceiver LBT which is contained in products developed by SkyTrac Systems Generally speaking an Iridium unit located within 15 to 45 meters 50 to 150 feet respectively of an operating INMARSAT mini M or Standard C terminal will likely experience interruption in the unit s performance Other sources of RF interference such as Globalstar units radar devices and broadcast stations can cause interference for Iridium units but usually are not encountered as frequently as INMARSAT terminals Mitigation of RF Interference Degradation of service due to RF interference to the Iridium unit can be significantly improved by performing either or both of the following actions a Increasing the distance and moving the Iridium an
47. rmation related to the airframe so that if the ISAT 200 is replaced the new unit will be easily reconfigured If an ISAT 200 is moved from one ITRAY 200 to another the ISAT 200 will automatically use the configuration contained in the new ITRAY 200 Note If an ISAT 200R Mod None is installed in an ITRAY 200R Mod A then the ISAT 200 MB software must be upgraded to a version greater than 00 11 13 1 3 3 Antenna The SkyTrac combination antenna combines both an Iridium antenna and a GPS antenna into a single package with a small footprint The antenna is qualified to TSO C144 This simplifies aircraft installation It is recommended that only the SkyTrac combination antenna be used with the ISAT 200 system If you wish to use an antenna other than the one provided please contact SkyTrac Systems for assistance 1 3 4 ISAT 200 Installation Components The necessary pins required to populate the ITRAY 200 connectors are included with the ITRAY 200 as well as the connectors required to install the SkyTrac combination antenna Document Rev 01 019 DOC0334 Page 10 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 1 3 5 ISAT 200 Models Table 1 ISAT 200 Models Type Part Number Description Compatibility ISAT 200R 101 200 01 GE EN 102 200 01 ISAT 200R 101 200 03 Ge e D 102 200 01 ITRAY 200R 102 200 01 ITRAY Installation Kit for ISAT 200R WEE Note ISAT 200S 101 200
48. rning Changes or modifications not expressly approved by SkyTrac Systems Ltd STS could void the user s authority to operate the equipment Warranty Information SkyTrac Systems Ltd warrants this product to be free of defects in materials and workmanship and that the product meets or exceeds approved factory acceptance test requirements STS reserves the right to replace any warranted product at its sole discretion during the warranty period The ISAT 200 Airborne Data Position Communicator except for the Li ion battery P N STS0044 or STS0061 and ITRAY 200 Installation Kit are under warranty for one year from date of shipment from SkyTrac Systems For failed units caused by defective parts or workmanship contact SkyTrac Systems for an RMA Once an RMA has been obtained the unit should be returned to SkyTrac Systems Ltd 200 170 Rutland Road North Kelowna B C Canada V1X 3B2 Proprietary Notice The information contained in this document is proprietary and confidential to SkyTrac Systems Ltd No part of this document may be reproduced or transmitted in any form or by any means electronic or mechancial without express written permission from SkyTrac Systems Ltd Document Rev 01 019 DOC0334 Page 3 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd Table Of Contents 1 A AS A ne ee 7 1 1 IMtFOGUCTION ster See A A A ARA ae 7 1 2 A A O O O 7 12 A O 8 122 ROTOS cunado lia 8 1 3 I
49. tallation This section also includes system wiring diagrams with installation notes When installing the ISAT 200 the installer shall have a working knowledge of aircraft electronics installation and be a holder of either an FAA Repairman s Certificate or a Transport Canada equivalent All installations should meet the requirements of FAA advisory circular AC43 13 1B IMPORTANT NOTICE All system interconnect cables must be connected before power is applied to the system 4 2 Line Functions This section describes the contact layout of the ARINC404 ITRAY 200R for completion of electrical installation purposes only Included for the product is a drawing of the connector and a list of pin outs with a detailed description of each connector pin out group Document Rev 01 019 DOC0334 Page 24 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 4 2 1 ITRAY 200R Pin out Note In the following figures Bay B refers to the upper bay connector with 106 pins and Bay A refers to the lower bay connector with 30 pins The following figures illustrate the ARINC 404 pin callouts using drawings pin names and pin descriptions O Y 9 E OG OC o ao O E O O E O OG t 1 ols 20 Gi OO Gi DP ee oS SS ER E Ges sea SS E Si We GEG SS ES ET SR ceo Y OG 90 eS Er Er VP Oe 094 740 810000003 0000 e 20 Y G Y Si Y Y E e Or 90 160 Y O 0 E Y Y 120 ez YU Er a Figure 3 ARINC404 Bay B 106 pin out dra
50. td 6 POST INSTALLATION TESTS 6 1 General This section contains instructions for the tests to be performed after installation in order to confirm that the system has been installed correctly Post installation tests are mandatory for all ISAT 200 installations 6 2 Function Test The avionics installer must perform this test immediately after installation 1 2 6 Move aircraft to a location with unrestricted visibility of the sky Power on unit on by turning on mains power Use the ISAT 200 menu system to check the status of the Iridium Signal and the GPS signal A single push press and release of the button will scroll through the menu one item at a time while pressing and holding the button will select a menu item The status of the GPS and Iridium signals can be checked under the Info menu A GPS sat count of 4 or better and GPS Lock confirms correct installation of the GPS portion A MDM Sig strength of 2 or better confirms correct installation of the Iridium portion Test proper position reporting at the default interval setting 1 minute An acceptable method for testing position reporting is to use STS flight following software to check if a valid position and GPS time is reported for the installed ISAT 200 Inform the local SkyTrac Program Manager to change the default position interval via SkyWeb to another interval if required Failure to do so will result in position report charges at one minute intervals
51. tenna off axis from the source of the interference or b Using an external band pass filter and an external antenna In determining the optimal location for mounting an external Iridium antenna in a location where INMARSAT antennae are also located be certain that the Iridium antenna is mounted to the side or behind the INMARSAT antenna as well as above or below it Also note that the length of the feed line the cable running from the Iridium unit to the antenna plays an important role in the performance of the unit Document Rev 01 019 DOC0334 Page 43 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 11 2 Appendix B Battery Precautions Document Rev 01 019 DOC0334 Page 44 of 48 Restricted Proprietary and Confidential Information NOTES AND PRECAUTIONS Safety Precautions for the Lithium lon Battery Pack Use of Lithium lon Batteries and the Design of Equipment That Uses These Batteries In general lithium ion batteries are used in battery packs that contain both lithium ion batteries and battery protection circuits Both items are sealed in a container made of a material such as resin so that the battery pack cannot be easily disassembled 1 Charging the Batteries The constant voltage constant current method is used to charge lithium on batteries See Figure below Scharrate d agrarr o cha charging process asaurring a a ngk call Conan velaga con can Curran ieee AS
52. tice Contact Panasonic for the latest information Panasonic JANUARY 2007 SAFETY PRECAUTIONS FOR LITHIUM ION BATTERY PACKS e Safety Warnings 1 When Using the Battery WARNING 1 Misusing the battery may cause the battery to get hot rupture or ignite and cause serious injury Be sure to follow the safety rules listed below e Do not place the battery in fire or heat the battery e Do not install the battery backwards so that the polarity is reversed e Do not connect the positive terminal and the negative terminal of the battery to each other with any metal object Such as wire e Do not carry or store the batteries together with necklaces hairpins or other metal objects e Do not pierce the battery with nails strike the battery with a hammer step on the battery or otherwise subject it to strong impacts or shocks e Do not solder directly onto the battery e Do not expose the battery to water or salt water or allow the battery to get wet Do not disassemble or modify the battery The battery contains safety and protection devices which if damaged may cause the battery to generate heat rupture or ignite Do not place the battery on or near fires stoves or other high temperature locations Do not place the battery in direct sunshine or use or store the battery inside cars in hot weather Doing so may cause the battery to generate heat rupture or ignite Using the battery in this manner may also result in a loss o
53. tively flying aircraft in above 0 degrees Celsius and battery low warning is issued the battery may need to be replaced A low battery warning on consecutive flights within the battery operational temperature range indicates that the battery is no longer successfully retaining its charge and the battery should be replaced If the ISAT 200 is not transmitting it s mains off report the battery needs to be replaced Periodic inspection is also required as per the Continued Airworthiness Section The Li ion Battery Pack PN STS0044 or STS0061 must be replaced under the following conditions e The battery no longer maintains a satisfactory charge e The battery will not charge e The battery gets hot during charging or emits an odour contact SkyTrac Systems should this occur Document Rev 01 019 DOC0334 Page 39 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 8 2 1 Battery Replacement Instructions Replace the ISAT 200 battery only with an approved STS ISAT 200 battery or damage to the ISAT 200 and or the battery may result Use of another battery may present a risk of fire or explosion CAUTION Battery May Explode If Mistreated Do Not Disassemble Or Dispose Of In Fire Do not install STS0044 in an ISAT 200 with mod status D To replace the battery follow the instructions below 1 Remove the ISAT 200 from the ITRAY 200 2 Remove the battery cover from the ISAT 200 3 Disconnect the
54. to prevent overdischarge 5 Use of the Batteries See the section on Safety Precautions for the Lithium lon Battery Pack 6 Other The Chemical Reaction Because batteries utilize a chemical reaction battery performance will deteriorate over time even if stored for a long period of time without being used In addition if the various usage conditions such as charge discharge ambient temperature etc are not maintained within the specified ranges the life expectancy of the battery may be shortened or the device in which the battery is used may be damaged by electrolyte leakage If the batteries cannot maintain a charge for long periods of time even when they are charged correctly this may indicate it is time to change the battery 7 Please Note The performance and life expectancy of batteries depends heavily on how the batteries are used In order to ensure safety be sure to consult with Panasonic in advance regarding battery charging and discharging specifications and equipment structures when designing equipment that includes these batteries Please Note Panasonic assumes no liability for problems that occur when the Notes and Precautions for use listed above are not followed This information is generally descriptive only and is not intended to make or imply any representation guarantee or warranty with respect to any cells and batteries Cell and battery designs specifications are subject to modification without no
55. ument Rev 01 019 DOC0334 Page 30 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 4 2 8 Auxiliary Power Output Table 25 Auxiliary Power Description ISAT 200R SC Bay A Pin Description and recommended usage 13 6 VDC 0 8 A short circuit protected thermal shutdown protected 14 Auxiliary Output Ground IMPORTANT NOTICE The auxiliary power output does not operate when the ISAT is operating under internal battery power 4 2 9 External Power Input 28V Table 26 External Power Input Description Et Description and recommended usage 15 This pin connects to the aircraft power systems and supply power to the ISAT 200 16 Power Ground 28VDC Return 4 2 10 Audio Lines Table 27 Audio Line Description ZE Description and recommended usage 1 Microphone ground 2 Microphone positive input 13 Microphone negative input 26 Speaker negative 27 Speaker positive 600 ohm output 28 Speaker positive 300 ohm output 4 2 11 ITRAY 200 Communication Lines The ISAT 200 has several pins which communicate with the Configuration Module on the ITRAY 200 These pins are pre wired at the factory and are not for use by the aircraft installer Table 28 TRAY 200 Communication Line Description ISAT 200R Description and recommended usage Bay A Pin 1 2 3 7 8 9 Power supply and data bus to ITRAY 200 Docum
56. unctional test Instructions added new ISAT 200R CatM and ISAT 200S CatM This release is not TC approved Feb 11 2010 G Ross 01 009 270 Updated Table 7 with operation temperature short term operational temperature and ITRAY 200 mounted physical characteristics Removed STS ISAT ANT from Table 4 Corrected the voltage rating for STS ISAT ANT on Table 10 Added ITRAY 200 installation orientation to section 3 7 Added a GND connection note to section 4 2 5 Added the qualification of the ITRAY 200 to Table 12 Added installation materials to Table 14 Corrected the weight of the ISAT 200 Mar 04 2010 M Hubert G Ross 01 010 340 Labeled analog pins 2 and 3 as Reserved Do not use Section 4 2 8 now says analogue inputs 1 4 5 can be configured and analogue input 1 is preferred for engine status Section 1 3 1 references three analogue inputs now Jul 21 2010 G Ross 01 011 357 All references to ISAT 200S and ITRAY 200S deleted Added note to Section 1 3 5 that ISAT 200S and ITRAY 200S have been discontinued Sep 10 2010 Y Liu 01 012 372 Added note to section 1 3 2 Nov 15 2010 D McMahon 01 013 384 Added ESD Caution Statement Fixed Formatting Dec 15 2010 M Hubert 01 014 390 Added ITRAY 200 to warranty statement Added from SkyTrac Systems to date of purchase in warranty statement Jan 5 2011 J
57. wing Figure 4 ARINC404 Bay A 30 pin out drawing Document Rev 01 019 DOC0334 Page 25 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd Table 15 ARINC 404 Bay B pin descriptions ARINC Pin Pin Names Description 1 RESERVED Microphone Ground 2 MIC_IN Microphone In positive line 3 RESERVED Microphone Ground 4 CH_GND Chassis Ground 13 MIC_IN Microphone In negative line 14 RESERVED Reserved do no connect 15 GND Analogue Ground 16 CH_GND Chassis Ground 26 SPKR_GND Speaker Ground 27 SPKR_600 Speaker 600 28 SPKR_300 Speaker 300 29 RS 485_B2 RS485 port 2 inverted line 30 CH_GND Chassis Ground Ethernet 31 ETH IN Ethernet negative receive port 32 39 RESERVED Reserved do not connect 40 DI3 Digital Input 3 41 DIO_GND Digital I O Ground 42 RS485 GND2 RS485 port 2 ground reference 43 RS 485 A2 RS485 port 2 non inverted line 44 ETH IN Ethernet positive receive port 45 52 RESERVED Reserved do not connect 53 DO4 Digital Output 4 54 DO2 Digital Output 2 55 DO3 Digital Output 3 56 DI5 Digital Input 5 57 ETH OUT Ethernet negative transmit port 58 66 RESERVED Reserved do not connect 67 ADC2 Analogue Input 2 Reserved Do not use 68 ADC3 Analogue Input 3 Reserved Do not use 69 ADC4 Analogue Input 4 70 ETH OUT Ethernet positive transmit port 71 79 RESERVED Reserved do not c
58. y damage the performance of the battery or reduce its life expectancy and if the device causes an abnormal current to flow it may cause the battery to become hot rupture or ignite and cause serious injury I CAUTION 2 The temperature range over which the battery can be discharged is 20 to 60 C Use of the battery outside of this temperature range may damage the performance of the battery or may reduce its life expectancy To ensure the safe use of this battery contact Panasonic when designing a device that uses this battery This information is generally descriptive only and is not intended to make or imply any representation guarantee or warranty with respect to any cells and batteries Cell and battery designs specifications are subject to modification without notice Contact Panasonic for the latest information Panasonic JANUARY 2007
59. y of the battery Note 2 The ISAT 200 has a built in protection circuit to prevent charging outside of the battery charging operational range Note 3 Store batteries at room temperature at 30 50 of capacity for maximum battery life Please refer to Appendix B Battery Precautions for additional information on operating conditions Document Rev 01 019 DOC0334 Page 15 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 2 6 Safety Compliance The ISAT 200 and ITRAY 200 have been tested to meet the following RTCA DO 160 categories Part Number 101 200 01 ISAT 200R has been tested to the RTCA DO 160E environmental categories as follows DO 160E Env Cat F1 BAB SBM UG XXXXXXZBBXXXLXXXXX Part Numbers 101 200 03 ISAT 200R and 102 200 01 ITRAY 200R have been tested to the RTCA DO 160F environmental categories as follows DO 160F Env Cat F1 BAB SBM UG XXXXXXZ BX BXXXMXXXXX The tests demonstrated that the ISAT 200 and ITRAY 200 do not exhibit any unsafe performance when exposed to the specified environmental test conditions and that installation of the ISAT 200 and ITRAY 200 in accordance with the installation instructions in this Manual will not pose a hazard to the continued safe flight and landing of the aircraft Document Rev 01 019 DOC0334 Page 16 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 2 6 1 Environmental Test
60. y pack and increase the risk of heat explosion or fire STS is not responsible for the damage caused to the Li ion battery pack by mishandling The pack refers to the ISAT 200 Li ion battery pack PN STS0044 or STS0061 e Do not short circuit the pack Do not pierce or strike with a hammer step on or otherwise subject to a strong impact Do not dispose of the pack in a fire or heat it intentionally Do not use the battery in reverse polarity Do not allow the pack to be immersed in water Do not disassemble or modify the pack There is a safety mechanism incorporated into every pack cell to prevent damage to the pack or the ISAT 200 A damaged safety mechanism or mishandling of the battery pack may cause heat explosion or fire CAUTION Do not operate or store the battery pack above 60 degrees Celsius ambient temperature Refer to the battery datasheet in Appendix B for more information Document Rev 01 019 DOC0334 Page 38 of 48 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 8 MAINTENANCE AND CONTINUED AIRWORTHINESS 8 1 Continued Airworthiness Periodic inspection is required as follows e Operator is to inspect the Mains Power breaker once every six months to verify proper operation of the breaker e Operator is to inspect the ISAT 200 battery once every year to verify the battery is in good working condition Open the battery compartment and visually inspect the battery Inspect for leaked

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