Sky Connect Aviation Series Installation Manual TRACKER

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Sky Connect Aviation SeriesInstallation ManualTRACKERRevision # 1.4Dated: January 13, 2009Part Number 1616-964-12Jan. 13, 2009iRevision 1.4

Aviation Certification IssuesCERTIFICATION – Sky Connect has rights to several Supplemental Type Certificates. Use ofthis information is provided with purchase of the equipment. Assistance in certification efforts tothe installers is offered at no charge to the customer or installer. Assistance is provided on SkyConnect’s scheduling.Please plan your certification issues with the following in mind; Phone assistance is provided8am to 5pm Central Time U.S. based on our available time and work load for the day.Certification teams maybe required to perform work on a deadline basis, there will be a fee forsuch work at the rate of 150 US per hour. Please contact Sky Connect Technical Services forassistance.Jan. 13, 2009iiRevision 1.4

TABLE of CONTENTSLIST OF REVISIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vINDEX OF ACRONYMS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . viGENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 1INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 1SYSTEM DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 1TECHNICAL SPECIFICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 3INSTALLATION PROCESS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 11WIRING DIAGRAM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 11SIM CARD ACTIVATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 11ANTENNA PLACEMENT PLAN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 11INFORMATION NEEDED FOR CONFIGURATION . . . . . . . . . . . . . . . . . . . . . . 2 - 12TRACKER MAPPING SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 12WIRING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 12CONFIGURATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 12TRACKER RULES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 12INSTALLATION - GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 1A DISCUSSION ON SIM CARDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 1ITEMS REQUIRED BUT NOT SUPPLIED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 2GENERAL SYSTEM COMPONENTS THAT APPLY TO ALL SYSTEMS . . . . . . 3 - 4SYSTEM COMPONENTS THAT APPLY ONLY TO TRACKER . . . . . . . . . . . . . 3 - 4GENERAL INSTALLATION INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 6TRACKER SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 1TRACKER SYSTEM COMPONENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 1Jan. 13, 2009iiiRevision 1.4

TRANSCEIVER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 1CONFIGURATION MODULE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 1CONFIGURATION/SIM MODULE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 2TRACKER SOP DIALER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 3MMU/II (Mission Management Unit) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 3TRACKER-SOP STRUCTURAL MOUNTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 5TRACKER WIRING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 5POST INSTALLATION TESTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 8TRACKER SETUP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 11TRACKER TESTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 11OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 14APPENDIX A Troubleshooting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 - 1Jan. 13, 2009ivRevision 1.4

LIST OF REVISIONSRevision #Description of ChangeDateApproval1.0Removed all POTS unit information andcreated a new manual part number forTracker only.3/24/2007MLF1.1Added Combo antenna, corrected note onICSM, revised pin out chart to remove the400 series references.3/20/2008MLF1.2Typos corrected, revised MMU/MMU IIrecommended installation wiring drawing10/3/2008MLF1.3Added spec and part numbers for MMU II12/15/2008MLF1.4Added configuration details on MMU II andCombo antenna drawing1/13/2009MLFJan. 13, 2009vRevision 1.4

INDEX OF ACRONYMSFOIField Of Interest (a position)GISGeographic Information SystemIDTIcarus Dial ToneIMEIInternational Mobile Equipment IdentifierLBTL Band TransceiverPBXPrivate Branch eXchangePOTSPlain Old Telephone SystemPUKPersonal Unblocking CodeSBDShort Burst DataSIMSubscriber Identity ModuleSMSShort Message ServiceFor a complete definition of terms see http://www.telestial.com/glossary.htm on the Web.Jan. 13, 2009viRevision 1.4

1GENERAL INFORMATION1.1INTRODUCTIONThis manual contains information relative to the physical, mechanical, and electricalinstallation of the Sky Connect Systems. Operating procedures are also included.1.2SYSTEM DESCRIPTIONThe Sky Connect series satellite communications device consists of a transceiver, anL-band antenna, and a dialing/audio/data interface device. The remote mountedtransceiver is the heart of the system, and contains the Iridium satellite LBT (L-BandTransceiver). The LBT can be thought of as the “phone” in the satellite phone system andthe modem in the data system, as it is the connection used to gain access to the Iridiumnetwork. The LBT allows the two way transfer of voice and data.The LBT is the same in every transceiver of the Sky Connect System though differentmodules are added to define the function of the transceiver as a whole. Each SkyConnect telephone system also has the ability for data transfer at rates up to 10 Kbps(with compression), allowing the user to interface a laptop for in-flight email capability.The Tracker system offers an optional internal 12 channel G.P.S. module. Tracker usesthe short burst data transfer portions of the Sky Connect suite, though it can be coupledwith any of the phone systems. Any system can exist alone, or co-exist with another, andupgrades can be done to any system at any time without incurring additional costpenalties.The Iridium system can only be occupied by one “call” at a time, whether it is voice, data,or Short Burst Data. These systems exist simultaneously, but can not be usedsimultaneously. Multiple transceivers and antennas are required for multiple channels ofcommunication. For clarity, two users may be on separate handsets on the same call, buttwo users can not be on separate handsets on different calls without a secondtransceiver/antenna. Similarly, when a phone call is in progress, Tracker will be unableto send SBD packets, though as soon as the line is clear, it will send its stored messages.Jan. 13, 20091-1Revision 1.4

Figure 1Tracker & Communication Concept DrawingJan. 13, 20091-2Revision 1.4

1.3TECHNICAL SPECIFICATIONS1.3.1TRANSCEIVERSPart Numbers 1616-XX0-0X all Transceivers are the same with the exceptions listed inthe below table.ITEMSPECRegulatory Compliance:DO-160D, FAA STC on Part 25, 27, and 29 aircraft. FAA-PM ATemperature Range:Section 4 Cat D2 (-20C to 55C)Altitude Range:Section 4 Cat D2 (50,000 feet)Vibration:Section 8 Cat RTemp Variation:Section 5 Cat CPower Input:Section 16 Cat BDC Spike:Section 17 Cat BConducted EmissionsSection 21 Cat BRadiated EmissionsSection 21 Cat BW eight4.05 lbs.Add Tracker:.05 lbs.Add G.P.S.10 lbsAdd Messenger:.05 lbs.Physical Dimensions:Length10.0 Inches(W idth)2.5 Inches(Height)4.5 InchesPower Requirements (Voltage):11-32VdcPower Requirements (Current) : 1 Amp @ 28VdcTransmit Power Average:1.5 wattsMounting:Quick release tray, 4-#6 holes, any configurationTransmission rate:2.4Kbps voice and data (10Kbps with compression)Operating Frequency:1.616-1.6265 GHzJan. 13, 20091-3Revision 1.4

ITEMSPECInputs/Outputs:POTS (Plain Old Telephone Service), RS232, DSC, dclevel. 8 discrete inputs Lo 1.2 Hi 1.3Connectors:TNC female (Iridium), BNC female G.P.S.,62 pin High Density D-sub connector1.3.5.2 SOP DIAL PAD SIX POSITION 1616-051-01/03SOP 6 Dialer has been dropped.1.3.5.3 SOP DIALER ELEVEN POSITION 1616-052-00/02ITEMSPECW eight8 oz.Physical Dimensions:(Depth)3.375 Inches(W idth)5.75 Inches(Height)1.12 InchesPower Requirements (Voltage):6 to 28 volt dimmer connected to two separate bussesPower Requirements (Current) :100 ma Max.Inputs:2 lamp inputsOutputs:7 switch grounded outputsConnectors:DB-15 maleMounting:Dzus rail1.3.5.4 MISSION MANAGEMENT UNIT 1616-055-00/10/12ITEMSPECRegulatory Compliance:FAA STC on Part 27, and 29 aircraft. (MMU II only part 29) FAAPM AW eight:15 oz.Jan. 13, 20091-4Revision 1.4

Physical Dimensions:(Depth)3.375 Inches(MMU) 5.65 (MMU II)(W idth)5.75 Inches(Height)1.875 InchesPower Requirements (Voltage):10-33 VDCPower Requirements (Current) :250 ma max.Inputs:RS-232Outputs:RS-232, four discrete outputs 100ma sinked to groundConnectors:DB-25 maleMounting:Dzus rail1.3.5.5 SWITCH PANEL1616-053-00Switch panel has been dropped1.3.5.6 CONFIGURATION MODULE1616-905-01ITEMSPECRegulatory Compliance:FAA STC on Part 27, and 29 aircraft. FAA-PM AW eight: 8 oz.Physical Dimensions:(Length)2.5 inches (without mating connectors)(W idth)1.25 inches(Height).625 inchesPower Requirements (Voltage):12VDC (supplied by transceiver)Inputs:Serial BussOutputs:Serial BussConnectors:2 DE-9 connectors one male one femaleJan. 13, 20091-5Revision 1.4

1.3.5.7 CONFIGURATION/SIM MODULE 1616-905-02ITEMSPECRegulatory Compliance:FAA STC on Part 27, and 29 aircraft. FAA-PM AW eight:16 oz.Physical Dimensions:(Length)2.5 inches (without mating connectors)(W idth)2.125 inches(Height).625 inchesPower Requirements (Voltage):12VDC (supplied by transceiver)Inputs:Serial Buss and DPL BussOutputs:Serial Buss and DPL BussConnectors:One DE9 female and one DB25 male1.3.6ANTENNAS1.3.6.1 IRIDIUM LOW PROFILE ANTENNA 1616-880-01 AeroAntenna AT2775-XXXITEMSPECRegulatory Compliance:TSO C-144, DO-160DOperating Temp:-55 Deg to 85 Deg CW eight:.5 Lbs Max.Physical Dimensions:3.5 inches in diameterFrequency:1595 /- 30 MhzConnectors:TNCFAltitude:70,000 feetImpedance:50 OhmsJan. 13, 20091-6Revision 1.4

1.3.6.2 IRIDIUM BLADE ANTENNA 1616-880-00 Dayton Grander # L10-780ITEMSPECRegulatory Compliance:FAA STC on Part 27, and 29 aircraftW eight.7 Lbs Max.Physical Dimensions:Length5.49 InchesW idth3.09 InchesHeight3.11 InchesSpeed:600 Kts.Impedance:50 Ohms1.3.6.3 SENSOR G.P.S. ANTENNA 1616-880-04ITEMSPECRegulatory Compliance:TSO C-144, DO-160DOperating Temp:-67 Deg F to 185 Deg FW eight5 Oz.Physical Dimensions:3.5 inches in diameter X .57 Inches HighFrequency:1575.42 MHzConnectors:TNCFAltitude:55,000 feetImpedance:50 OhmsVoltage:4 – 24 VDC1.3.6.4ANTCOM COMBO IRIDIUM/GPS ANTENNA 1616-880-10ITEMSPECRegulatory Compliance:TSO C-144, DO-160D, DO-228, MIL-C-5541Operating Temp:-67 Deg F to 185 Deg FW eight7.84 Oz.Jan. 13, 20092-7Revision 1.4

ITEMSPECPhysical Dimensions:L 5.026" W 2.2" H .71"Frequency:Iridium 1610 to 1626.5MHz GPS 1575.42 /- 13 MHzConnectors:TNC both GPS and IridiumAltitude:70,000 feetImpedance:50 OhmsVoltage:2.8 to 28VDC (GPS)Jan. 13, 20091-1Revision 1.4

2INSTALLATION PROCESSINSTALLATION PROCESS OUTLINENote: Make a plan to cover the follow items in depth in this manual.2.1W IRING DIAGRAM2.1.1G.P.S. interface, or use of an internal G.P.S.2.1.2Event switches, optional2.1.3Diagnostic port, must be installed for configuration2.1.4Configuration/SIM module, optional2.1.5Selection of Dialers optional2.2SIM CARD ACTIVATIONCheck to make sure the card is activated, call Sky ConnectYou will need to know the following information;2.2.1The IM EI # of your unit2.2.2Model #2.2.3Serial #2.2.4Credit Card or billing information for monthly service2.2.5Aircraft type and registration number2.2.6Complete contact information for customer using the product2.2.7Send in activation form to turn on the unit with satellite system, please fill out the form as accurately aspossible to make the process as smooth as possible2.2.8The form may be filled out on the web at http://www.skyconnect.aero/1086.xml2.3ANTENNA PLACEMENT PLAN2.3.1Pay close attention to the length of coax from the antenna to RT2.3.2Follow manual instructions on placement near other Sat COM and Comm antennas2.4Notebook computer with “tracker setup” program, CD included with RTJan. 13, 20092 - 11Revision 1.4

2.5INFORMATION NEEDED FOR CONFIGURATION2.5.1How the event switches were wired2.5.2W hat type of switches, MOM, ALT, Press2.5.3W hat phone numbers need to be entered (optional)2.6TRACKER MAPPING SYSTEMDecide what mapping system is to be used for tracking the aircraft.Setup an account with that provider and secure ID and passwords.Make sure this installation is added to the account that handles the mapping.It is the responsibility of the owner to add aircraft to the mapping system, Sky Connectcan NOT do that for you unless it is the Sky Connect W ebmap you are using.2.7W IRING2.7.1W ire system as drawn, you the installer are responsible to the FAA for methods and practices used duringthe installation.2.7.2Continuity checks.2.7.3Power polarity checks.2.8CONFIGURATION2.8.1Configure RT to work with event switches as connected in wiring2.8.2Configure external G.P.S. to talk to Sky Connect RT, Aviation or NMEA RS232 format data2.8.3Enter phone numbers (optional)2.9TRACKER RULESBefore the tracker can be used to display data on a map, the rules of operation must be understood. Thefollowing will outline those rules.2.9.1The transceiver must send data.Jan. 13, 20091.In order to send data the transceiver must have an active LBT sending SBD. This is donefrom the activation form.2.The transceiver must have an active SIM card.2 - 12Revision 1.4

3.The transceiver must have been configured for the aircraft type.4.Helicopters may use collective or squat switches.5.Airplanes may use squat switches.6.The transceiver must have the report intervals set.7.The aircraft must be outside and have a clear view of the sky.8.The aircraft antenna system must be installed I.A.W. our instructions.9.To display a complete flight, the aircraft must send Departure, Scheduled reports, and anArrival message to define a complete flight. This is done through the proper setting of thesquat switch, and or software settings from the tracker setup configuration software.Our server must be set to pass the data on to the proper map program.Our server must have been set up for the customer (activation form completed and sent in to our office).The map program must be set to receive the data from our server.The map program must have a profile setup to display the aircraft correctly.If email notification is desired we must have the email addresses (activation form).Jan. 13, 20092 - 13Revision 1.4

This page intentionally left blankJan. 13, 20092 - 14Revision 1.4

3INSTALLATION - GENERALPRIOR TO INSTALLATIONPerform a visual inspection of the equipment for evidence of damage incurred duringshipment.3.1A DISCUSSION ON SIM CARDSIt is Sky Connect policy to ship all units with a deactivated SIM card. The unit is tested with a DEMOcard before leaving our facility.W ith that in mind, please be aware of the following paragraphs.No testing can occur until a activated SIM card is installed in the transceiver or CONFIG/SIM Module.The account has to be activated with an Iridium service provider. Systems are generally shipped with aSIM card installed, with the PIN code disabled, and the service deactivated. The customer is responsiblefor this activation as the customer receives the bills for the phone use. This process can take minutes, andshould be done in advance of the installation/testing.In the event that the customer provides a SIM card, or desires to provide the card it must be de-pinned, orthe system will get blocked. Contact the manufacturer if you intend to change SIM cards. Sky Connectrecommends against customer replacement of SIM cards as it affects unit serviceability.Until the Iridium L-Band Transceiver has been registered on the network, there is very little you can do totest its operation. A de-pinned activated SIM is required before this can happen. The SIM card is theidentity of the user, and thus must travel with the user. In this case, the user’s SIM card is installed in theSky Connect transceiver.This process should only need to be accomplished at initial installation. After useractivation, the system will function. Should the unit need to be replaced, or transferred to another party,or in the event that a SIM card requires replacement, return unit to SkyConnect or a qualified avionics shop to have the SIM card replaced in order to keep the SIM card accountmatched with the user.Jan. 13, 20093-1Revision 1.4

3.2ITEMS REQUIRED BUT NOT SUPPLIED;Table 1QTYITEM SUSE1Daniels Manufacturing Crimper P/N M22520/2-01P11Daniels Manufacturing Crimper Positioner P/N K41P11Daniels Manufacturing Crimper Positioner P/N K1SAll M24308 connectorsCrimping tools for use on coax connectorsAll coax connectorsCoax connectors for antenna cable if locally madeContact insertion/removal toolM81969/1-4 (metal) orM81969/14-01 (plastic)Misc. installations supplies such as; wire ties, Adel clamps, Etc.If installing a Tracker without the control head (ieFlightDeck system with a Tracker) and panel mountedswitches are desired, we offer the following manufacturerpart numbers with and without LEDs with and withoutNVIS, non NVIS part numbers are not shown call VivisunVivisun# LED-42-15-KB-36185 (2LA EMER; 3S0 ////)Emergency SwitchVivisun# LED-40-18-KB-36189 (2LA CODE; 3J0 ////)Code SwitchVivisun# LED-42-12-KB-36187 (2LA POSN; 3J0 ////)Position SwitchVivisun# LED-42-12-KB-36188 (2LA DIAL; 3J0 ////)Dial SwitchVivisun# LED-40-18-KB-36190 (2JA CALL; 3JA TEXT)Call/Text - AnnunciatorVivisun# 95-42-15-K6-70878 (2LA EMER; 3S0 ////)Emergency SwitchVivisun# 95-40-18-K6-70956 (2LA CODE; 3J0 ////)Code SwitchVivisun# 95-42-12-K6-70880 (2LA POSN; 3J0 ////)Position SwitchVivisun# 95-42-12-K6-70881 (2LA DIAL; 3J0 ////)Dial SwitchVivisun# 95-40-18-K6-70957 (2JA CALL; 3JA TEXT)Call/Text - AnnunciatorJan. 13, 20093-2Revision 1.4

3.3Suggestions for coax connectors and tools (customer supplied);Table 2ConnectorCoaxToolNewark#Industrial#BNC maleRG400/RG142CTL-189F289131-4427BNC male 90 DegRG400/RG142CTL-139F144331-334TNC femaleRG400/RG142220045-296F7801225551-6TNC female bulkheadRG400/RG142220045-297F8562225557-6TNC maleRG400/RG142CTL-192B064731-4452TNC male 90degRG400/RG142220045-290B4658225554-6Jan. 13, 20093-3Revision 1.4

3.4GENERAL SYSTEM COM PONENTS THAT APPLY TO ALL SYSTEM STable 3ProductPart NumberDescription1616-700-01Inmarsat Filter1616-900-99Sky Connect Series CD ROM1616-950-XXAviation Installation Manual, current revision1616-901-XXQuick Start User Manual, current revision1616-050-80SBD Message Traffic1616-104-013 year warrantyS67-1575-109Low Profile Iridium Antenna1616-429-01ARINC 429 Converter for con

(with compression), allowing the user to interface a laptop for in-flight email capability. The Tracker system offers an optional internal 12 channel G.P.S. module. Tracker uses the short burst data transfer portions of the Sky Connect suite, though it can b

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