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Sky Connect Series Installation Manual

1. 1 RS232 In HI 1 RS232 In Lo 1 GPS Data From GPS Aviation or NMEA 0183 marine Note 3 Comm Audio HI e TRY DADOS Comm Audio HI Comm Audio Lo lt Audio Lo Mic Audio H 7 Mic Audio Hi hield SKY 7A22 to Dimmer Buss Audio Enable 25 5 ne lator Panel o Pilot Headset 5 Pilot Phone Audio HT Jack 4 Pilot Mic Audio Lo Noten z 5 Pilot Mic Audio Hi Position Dialer A1 A E gt t Copilot Mic Audio Dialer A2 Copilot Mic Audio Dialer A4 4 Copilot Phone Audi Copilot Phone Audi See Code Under Fire Lite Emergency Annuciator SKY 7 Trecker Status Annuciator SKY 74422 3 Dialer Status Aux Tracker Status Lite Note 14 Squat Switch Ais wette Power SRY CSREES gone ee sky 31A22N Aux Emergency L Gnd AC on Gnd Aux Code Under Fire Lite Aux Dialer Status Lite Copilot Phone Hi Copilot Phones Lo Copilot Mic Hi Copilot Mic Lo Pilot Phones Hi Pilot Phones Lo 5 Pilot Mic Hi Event Switch 5 sak optional Switch closure A Ee OMEN mE s Pilot Mic Lo Note 2 ES P N 1616 051 XX P N 1616 S00 03 Diagnostic Conn Audio Panel P10 Pilot Mic Lo Conf guration Module ER As Pilot Mic H An A FEO j i E gt Pilot Phones Lo Conf Ig SDA era SDA Data In CORE PERE 9 Date Out 9 Data In Data Lo X t 9 Data
2. 9 1 Revision Date April 25 2005 Revision 2 02 C skyConnect Description of Problem Possible Causes Executive handset keeps repeating 3 melodic tones when I go off hook A PIN code is still on the SIM card contact tech support before any attempt to dial is made Executive handset played 3 repeating tones and my call attempts failed even though melodic I now hear a dial tone instead of the 3 melodic tones A PIN code is still on the SIM card and you have locked the phone by entering invalid codes Contact Technical Support I dial numbers hear a pause and then a repetitive sound consisting of two quick dial tones and a pause Hit a to start the call sequence on Executive Flight Deck systems I dial numbers hear call progress tones or a pause followed by a return to dial tone Your call did not complete for some reason no socket established try again Check signal strength by dialing 4 beep no signal strength 6 beeps full signal strength Classic Handset says Enter PIN A PIN code is still on the SIM card Contact tech support before any attempt to dial is made Classic Handset says BLOCKED A PIN code is still on the SIM card and you have locked the phone by entering invalid codes Contact tech support All Systems with Voice I can make calls out but not to the aircraft when calling from a land line The dialing sequence is
3. CH TB Note SKY 70ABES Note 5 PIA TS X SkY 708ees T I BS spi A 1 T cto ATE cto SKY VEREES SKY 73A22 SKY 74A22 SKY 10A22N gt SKY 7A22 Dial Annunciator Panel 28VDC Dimmer Position Dialer A1 Dialer A2 Dialer A4 Code Under Fire Emergency Tracker Status Dialer Status Aux Tracker Status Lite Aux Annuc Power Aux Emergency Lite Aux Code Under Fire Lite Aux Dialer Status Lite Gnd P N 1618 081 XX Optional Switch closure Note 2 Note 14 Squat Switch gt SKY SOA22 e SKY 91A22N Gnd A C on Gnd SKY 11A88N SKY 7B22 Dial Annunclator Panel PBVDC Dimmer Position Dialer A1 Dialer A2 Dialer A4 Code Under Fire Emergency Tracker Status Dialer Status AUX Tracker Status Lite Aux Annuc Power Aux Emergencu Lite Aux Code Under Fire Lite Aux Dialer Status Lite Gnd P N 1618 051 XX Dimmer Buss SKY COREES TY STRESS See P N ATS775 TN P N S67 1575 39 P N 1616 050 0X See Chart for dash numbers Tracker SOP System Wiring Dual Dialers Dwg 1616 900 SS2 Conf igurat Config SCL Conf 1g SDA C
4. SYSTEMS COMPONENTS DO 160D Initial Part 25 Canadian and American STC on Cessna 525 CJ2 Section 4 Cat D2 20C to 55C Section 4 Cat D2 50 000 feet Section 8 Cat R Section 5 Cat C Section 16 Cat B Section 17 Cat B Section 21 Cat B Section 21 Cat B 4 05 lbs 05 Ibs 10 Ibs 05 Ibs 10 000 Inches 2 500 Inches 4 500 Inches 11 32Vdc Amp 28Vdc 1 5 watts 2 4Kbps voice and data 10Kbps with compression 1 616 1 6265 GHz POTS Plain Old Telephone Service RS232 DSC dc level TNC female Iridium BNC female GPS 62 pin High Density D sub connector Quick release tray 4 6 holes Refer to individual system sub sections for specifications on those components specific to each system Revision Date April 25 2005 1 3 Revision 2 02 C Sky Connect 2 INSTALLATION PROCESS INSTALLATION PROCESS OUTLINE 1 INSTALLATION PLANNING Note Make a plan to cover the follow items in depth in this manual 1 1 Wiring diagram 1 1 1 GPS interface or use of an internal GPS 1 1 2 Event switches optional 1 1 3 Diagnostic port must be installed for configuration 1 1 4 Configuration module optional 1 1 5 Selection of Dialers optional 1 2 SIM card activation Check to make sure the card is activated call Sky Connect You will need to know the following information 1 2 1 The IMEI of your unit 1 2 2 Model 1 2 3 Serial 1 2 4 Credit Card or billing information for monthly
5. the Tracker will store and send position reports when the line is free Configurations will exist to give Tracker priority thus discontinuing an in progress call Alternatively separate transceivers antennae can be used for multiple systems Using ground power turn on the Aircraft master avionics master or what ever is required to fully power all elements of the installed Sky Connect components If a GPS is interfaced it must be operating and have acquired satellites The aircraft must have an unimpeded view of the sky Operating next to a hangar can cause occasional brief signal interruption of both GPS and Iridium functionality If using an internal GPS allow the unit to run for up to 15 minutes on the initial startup to allow the internal GPS to acquire almanac data Allow one minute for the system to register on the iridium network Within this registration time Tracker will generate a start up message which will be sent via the Iridium network to our switching network and then to Flight Explorer The data will be processed by Flight Explorer and sent back to the local PC running Flight Explorer Tracker Edition At this time approximately 12 seconds after the message was generated a data block will be available on your PC s display that contains all known information about your flight In this case it will know only your position Giving the GPS a destination waypoint and if possible some speed will send additional parameters to Fligh
6. the system must be powered down and the handset reconnected before power is applied No damage will be done to the handset though the system may not operate correctly until restart 6 3 Revision Date April 25 2005 Revision 2 02 C sky Connect 2 3 TROUBLESHOOTING TIPS Refer to Appendix A for troubleshooting advice 3 OPERATIONS The Sky Connect Classic system consists of the transceiver and L band antenna and uses a corded handset for dialing communicating The Classic configuration contains limited memory dialing functions When used in conjunction with FlightDeck access to the transceiver is on a first come first serve basis Ringing audio is provided through a small piezo alert which is housed in the Classic handset interface Volume of the alert is selectable via a trim pot adjustment A 28Vdc level output is available at the interface for additional external annunciator alerts A maximum of thirty feet from Transceiver to handset is permitted on the DSC buss This measurement includes path to both handsets as well as the collapsed coil length 6 4 Revision Date April 25 2005 Revision 2 02 Notes 1 Connect 22AWG spliced as shown to 18AWG 2 Optional switches require diode protection if connected to anything other than ground All audio wires are twisted pairs shield floats at one end All unused pins are reserved DO NOT connect anything to reserved pins Seng Hood PAN DI 000200 All wire numbers are examples use
7. 101 01 s LU SKY 18A22N H SKY Aces I NAT PTA12 Dialpad Audio Interface Trian N 28VDC P N ATS77S TNC Ei Audio Panel 28VDC Unswitched Audio in Hi Ring Audio Hi Lo Ring Audio Lo Unswitched Audio in cs N Com 3 Audio Hi Phone Audio Hi n ME M SKY TOAeeS P N S67 1575 39 Com 3 Audio in Lo Phone Audio Lo NN tol l b Mal D e tol tol b Com 3 Mic out Hi TI A i Mic Audio Hi 5 Mal 2 N I Llc w l 8 SKY 6A22S I I gt Pit ov Ae Com 3 Mic out Lo Mic Audio Lo P N 1616 100 01 Phone only customer supp ied Shield 1616 150 01 Phone with Tracker and GPS POTS Tip 1616 150 02 Phone with Tracker no GPS POTS Ring SKY 12A22N Gnd SKY 13A22N Gnd Note 2 P N 1616 301 01 Optional Wiring for Dialpad installation SKY 12A22N SKY CONNECT LLC File c cktcrt my schematics sky connect ech Title Sky Connect Install Dao Sheet Executive System Wiring No e Rev 1 0 Executive System Wiring Dwg e 1616 900 100 Approved Changed S MAR 2005 08 34 C Sky Connect 5 FLIGHTDECK SYSTEM 1 INSTALLATION Be sure to cover Section III as it pertains to the transceiver installation and antenna installation that applies to all systems All systems are capable of having the Tracker options installed For Tracker installation and system testing and operation see Section VII 1 1 FLIGHTDECK SYSTEM COMPONENTS Table 1 Description Components Product Requirements And
8. 4 4 TRANSCEIVER ELECTRICAL INSTALLATION 3 4 TRANSCEIVER PIN ASSIGNMENTS esee tetas tek seus atei eee Lb ee eta 3 5 4 EXECUTIVE SYSTEM tee ni prata insita 4 1 l INSTALLATION eicere SARA AAA EE EEA ET Ialia 4 1 1 1 EXECUTIVE SYSTEM COMPONENTS sess 4 1 1 2 EXECUTIVE COMPONENT SPECIFICATIONS e 4 3 1 3 EXECUTIVE STRUCTURALMOUNTING iii 4 3 14 ue eme 4 4 2 POSTINSTALLATION TESTING ii 4 4 2 1 TRANSCEIVER INDICATIONS PHONE SETTINGS AND OPERATIONS 4 4 2 3 RESETIING BASE STATION oi scessecocscassdasensanesseveendasssanecsses concsesoacvacseessesonecastdaseacenssoebonsgad S BEE 4 5 2 5 TROUBLESHOOTING TIPS aa ageet nan QQ qa haasi TA ia 4 6 3 OPERA MONS uuu yun uu tutun Sua maykamun E asnasan as 4 7 5 PLIGHIDECE SYSTEM lc aaa a nu uu AL aaa 5 1 I INSTALLATION u kam een eee 5 1 1 1 FLIGHTDECK SYSTEM COMPONENTS a ri 5 1 1 2 FLIGHTDECK COMPONENT SPECIFICATIONS USING NAT PTA12 DIALPAD 5 2 1 3 FLIGHTDECK STRUCTURALMOUNTING iii 5 2 14 PLIGHT DECK SYSTEM WIRING i iii 5 2 2 POST INSTALLATION TESTING nennen eene nnnnnnnn enne nente nnns essen nenne nasse seen rnnt nnns 5 3 2 1 TRANSCEIVER INDICATIONS AND PHONE SETTINGS iii 5 3 2 3 TROUBLESHOOTING TIPS 5 3 Se OPERATIONS ii Rn 5 4 ii
9. In Data Out 1 Copilot Mic Lo config Gnd 3 onf 19 Gnd c 3 Copilot Mic HI Config Par Par Copilot Phone Lo Shield 1 c J Copilot Phones Hi customer supplied Alternate Diagnostic Port Hiring W O Config Module Tracker Dash Number Chart 01 with C vacker no GPS with Telephony and GPS on with Telephony end no GPS P N S67 5 GPS P N ATS77S TNC E BNC gt N 1616 050 0X See Chi for dash File c cktert my schemat ics sky connect Sch Title Sky Conn Install Dag Sheet Tracker Dialer Lo Z Wiring Tracker Dialer System Lo Z Wiring Dag 1616 900 SS1 is crested mam Approved Changed G VAR POOS Sky Connect Transcelver 11 to 33 VOC 11 to 33 VOC 11 to 33 VOC Gnd Gnd 1 RS232 In 1 RS232 In Comm Audio Comm Audio Mic Audio Hi Shield Audio Enable Configuration Gnd Shield Swi 1 Switch 2 Switch 3 Switch 4 Event Swite Event Swi Annuciator Annuciator Event Switch Event Switch 6 Congif SCL Config SDA Config Deta Out Config Data In BNC J1 P1 Non ESS Buss mE A SatTalk P18 J1 so gt SKY 8A22 l GPS Date From GPS Aviation or NMEA 0183 marine r s lt Y SABEN 38 esvpc 37 DC 33 34 Comm Audio HI Audio Lo
10. Mic Audio Lo 1 Com 3 Mic out customer suppl ied Notes Shield D D D SR SOT ee b b b Note 3 POTS Tip o SKY CASES POTS Tip POTS Ring POTS Ring SKY 12A22N Gnd Shield PC Data Connector SKY 13A22N Gnd P4 SKY SAPES 9 Note 6 Ringer Drive Gnd SKY 4AceS S VDC Dimmer e8VDC Dimmer Buss SKY SABES Note 13 SKY 6AceS P N 1616 301 01 Note 7 28 VDC Dimmer P N S67 1575 39 es N Ringer Annunciator TNC Note 8 P N 1616 300 01 Phone only 1616 350 01 Phone with Tracker and GPS 1616 350 02 Phone with Tracker no GPS SKY CONNECT LLC lt 5 A A A__ ann Flight Deck Wiring Dwg 1616 900 200 Approved Changed 11 MAR 2005 11 53 C Sky Connect 6 CLASSIC SYSTEM 1 INSTALLATION Be sure to cover Section III as it pertains to the transceiver installation and antenna installation that applies to all systems All systems are capable of having the Tracker options installed For Tracker installation and system testing and operation see Section VII 1 1 CLASSIC SYSTEM COMPONENTS Table 1 Description Components Product Requirements And Part Number Classic 1616 400 01 RT for Phone system Requires selection of 1616 400 only service provider 1616 450 01 RT for Phone with Tracker and internal GPS sensor includes GPS antenna 1616 450 02 RT for Phone with Tracker no GPS 1616 900 01 Classic install kit contains Tray Connectors Iridium antenna Manu
11. QTY ITEMS USE 1 Daniels Manufacturing Crimper P N M22520 2 01 Pl 1 Daniels Manufacturing Crimper Positioner P N K41 PI 1 Daniels Manufacturing Crimper Positioner P N KIS All M24308 connectors Crimping tools for use on coax connectors All coax connectors Coax connectors for antenna cable if locally made Misc installations supplies such as wire ties Adel clamps Etc GENERAL SYSTEM COMPONENTS THAT APPLY TO ALL SYSTEMS Table 2 Product Part Number Description Items that apply 1616 700 01 Inmarsat Filter to all systems 1616 900 99 Sky Connect Series CD ROM 1616 900 95 Apollo Compression Software 1616 900 XX Aviation Installation Manual current revision 1616 901 XX Quick Start User Manual current revision 1616 050 80 SBD Message Traffic 1616 050 97 Shop Upgrade Harness 1616 050 98 Field Upgrade Harness 1616 104 01 3 year warranty S67 1575 109 Low Profile Iridium Antenna 1616 900 10 ARINC 429 Converter for converting to RS232 1616 105 02 RT Installation kit which consist of 1 AMP HDP 20 Crimp Contact Connectors P N 571 2051631 from Mouser Electronics 2 Connector Pin P N FC7520D from Positronic Industries 3 UND Cable Clamp SZ2 AMP D sub Accessories P N 571 2057301 from Mouser Electronics 4 Hardware AMP DC 0449 Kit P N 205980 1 from Mouser Electronics 3 2 Revision Date April 25 2005 Revision 2 02 C skyConnect GENERAL INSTALLATION INSTRU
12. Revision Date April 25 2005 Revision 2 02 C skyConnect 6 CLASSIC SYSTEM ananas 6 1 1 INSTALLATION D 6 1 1 1 ERR AE E RE 6 1 1 2 CLASSIC COMPONENT SPECIFICATIONS i 6 2 1 3 CLASSIC STRUCTURAL MOUNTING ei 6 2 1 4 EE e ME 6 3 2 POSTINSTALLATIONTESTING uu elia anali Ae NT eni renne 6 3 2 1 TRANSCEIVER INDICATIONS PHONE SETTINGS AND OPERATIONS 6 3 2 2 HOW TO DIAL CALLS piii iii 6 3 2 3 TROUBLESHOOTING TIPS nei iii 6 4 3 OPBRATIONS u 6 4 7 TRACKER SYSTEM ner OTT 7 1 l INSTALLATION clelia lalla 7 1 1 1 TRACKER SYSTEM COMPONENTS rei 7 1 1 2 TRACKER SOP COMPONENT SPECIFICATIONS ii 7 2 1 3 TRACKER SOP STRUCTURAL MOUNTING i 7 3 1 4 TRACKER WIRING ttr pte ap re eher ut pe than ta ves alos EC da EUR palesa 7 3 2 POSTINSTAEEAXEIION TESTING n tede eter metet tee eget PI E Eee eU ERE SEHE RR EE 7 3 2 1 E TEE 7 4 2 2 CONFIGURATION SETTINGS nazio Rieti 7 5 2 4 TRACKER EENEG ege 7 10 S OPERATION tege e n iraniani 7 12 3 1 EE EMILE 7 12 3 2 TRAGKERSOP A cicli 7 12 8 TELEPHONE INDICATIONS AND SETUP essrerrrerererererere senese nese nice nen enerenereeeenecanesinezeneseaeionecenee 8 1 L FRANSCENVERINDICATIONS iiirii einen eiee ooie eere Ea Ib Pee oo ee 8 1 2 PHONE TESTING i u ER 8 2 2 4 AIRCRAFT
13. TO GROUND iaia ii 8 2 2 2 GROUND TO AIRCRAFT ee 8 2 9 APPENDIX A TROUBLESHOOTING rsssissiririazizriciinizzionizioraoianioniceazzinisianizniniinizzani azionisti 9 1 iii Revision Date April 25 2005 Revision 2 02 C sky Connect LIST OF REVISIONS Revision Description of Change Date Approval 2 0 Manual re write 3 24 2005 MLF 2 01 Typo corrections and added info on A model LBT 4 8 2005 MLF 2 02 Change on SOP Dialer dimming 4 25 05 MLF lv Revision Date April 25 2005 Revision 2 02 C sky Connect INDEX OF ACRONYMS FOI Field Of Interest a position GIS Geographic Information System IDT Icarus Dial Tone IMEI International Mobile Equipment Identifier LBT L Band Transceiver PBX Private Branch eXchange POTS Plain Old Telephone System PUK Personal Unblocking Code SBD Short Burst Data SIM Subscriber Identity Module SMS Short Message Service For a complete definition of terms see http www telestial com glossary htm on the Web Revision Date April 25 2005 Revision 2 02 C sky Connect 1 GENERAL INFORMATION 1 GENERAL 1 1 INTRODUCTION This manual contains information relative to the physical mechanical and electrical installation of the Sky Connect Systems Operating procedures are also included 1 2 SYSTEM DESCRIPTION The Sky Connect series satellite communications
14. closure Emergency Note 2 Tracker Status Dialer Status Aux Tracker Status Lite Aux Annuc Power Aux Emergency Lite Aux Code Under Fire Lite Aux Dialer Status Lite Note 14 Squat Switch Grid P N 1618 051 XX Event Switch 6 gt SKY SOA22 SKY S1A22N Gnd A C on Gnd Diagnostic Conn P10 Configuration Module Congif SCL 2 amp iconfig SCI Data Out AC Config SDA c SDA Dete In Config Data Out Data In Data Lo Config Data In 4 9 Data Out NC Config Gnd z ont 1g Gnd NC Config Par 1 amp JConfig Par NC Shield gt NC NC NC P N 1816 905 01 ont io Module P N ATS77S P N 567 Tracker Dash Number Chart BNC O3A Tracker with Telephony and GPS 04A Tracker with Telephony end no GPS P N 1618 050 0X See Chart for dash File c cktert my schematicsNsky connect Sch Title Sky Conn Install Dag Tracker SOP A System Wiring Dual Dialers W O SatTalk Dwg 1616 900 S55 SE EE mE Engineer Created 31 JAN 2005 C Approved Changed 21 MAR 2005 EMERGENCY UNDER FIRE POSITION lam JI W A S dl n n md Mery Tracker Status Phone Number Phone Stalus Figure 12 Special OPS Dialer Voice Speed Dia gt lt Format Country C
15. dash numbers Tracker SOP System Wiring Dwg e 1616 900 SS3 Sky Connect Transce ver J1 P1 11 to 33 VDC A IS 2 11 to 33 VDC SKY TATOS ne 11 to 33 VDC Gnd Gnd Gnd Non ESS Buss NN 1 RSe3e In Hi SKYSOADES 41 RS232 In Lo GPS Data From GPS Aviation or NMEA 0183 marine D Note 3 Audio Panel Comm Audio Hi SKY CASES Com Phone Hi Comm Audio Lo Com Phone Lo Mic Audio Hi Com Mic Hi SKY 7A22 to Dimmer Buss Note 12 Com 3 Mic Lo Audio Enable Audio Shield Configuration Gnd Dial Annunci ator Panel P11 J1 customer supplied Note S Shield 28VDC Dimmer Event Switch 1 SKY UASSS FOI Event Switch 2 Dialer A1 Event Switch 3 ESA Dialer A2 Event Switch 4 Dialer A4 Event Switch 7 SKY VERSES Code Under Fire Event Switch 8 Emergency Annuctator 1 SKY 73A22 Tracker Status Annuciator 2 SKY 74A22 Dialer Status Aux Tracker Status Lite Aux Annuc Power Note 4 Note 20 Aux Emergency Lite Note 14 Squat Switch Aux Code Under Fire Lite Event Switch SKY 90A22 SKY 91A22N Aux Dialer Status Lite Gnd A C on Gnd SKY 10A22N Gnd Event Switch Optional Switch closure P N 1616 051 XX Note 2 Diagnostic Conn P8 J8 P10 Configuration Module Note 19 Xie cuir iere d petii ege Sei dg SRY SIOE pl Le Note 21 Config SDA 9 Conf ig SDA Data In 3 3 Config Data Out Config Data In Data Lo 5 Config Data In Seb ___ Config Data Out NC Config Gnd SKY Genes Config Gnd NC Config Pwr Config Pwr NC Sh
16. deems the Sky Connect System safety sensitive the essential buss may be used An electrical load analysis may be required when doing so 3 4 Revision Date April 25 2005 Revision 2 02 C sky Connect TRANSCEIVER PIN ASSIGNMENTS The below Table is a listing of pin assignments and signal flows Read Notes and pay attention to the asterisk for changes in Original and A Model Trackers Table 4 denotes changes in A Model SOP units and others with newer version of LBT Pin Description Flow 1 Ground Input Gnd 2 Ringer output or Audio Enable Input SEE NOTE 1 In Out Pa A Model only PCM Transmit or IDT ground Gnd IMPORTANT DO NOT STRAP AS AUDIO ENABLE ON SOP A MODEL 3 Comm Audio Lo or POTS audio shield Gnd 4 DSC Uplink Classic Systems only In 5 PC DCD Data Connections only Out 6 NC 6 IDT DPL Mic audio Hi In 7 Microphone Audio Hi POTS Ring SEE NOTE 2 In T Mic Audio Input for SOP A Model In 8 Program Stat Factory Use Do Not Connect 9 Shield Configure ground Gnd 10 Shield Configure ground Gnd 11 Shield Configure ground Gnd 12 Configuration Module Power 3 3V Do Not Connect to other Out than ICM 13 Shield Configure ground Gnd 14 Shield Configuration ground Gnd 15 Annuciator 1 Sinks 100ma to Ground Out 16 Annuciator 2 Sinks 100ma to Ground Out 17 Annuciator 3 Sinks 100ma to Ground Out 18 Annucia
17. device consists of a transceiver an L band antenna and a dialing audio data interface device The remote mounted transceiver is the heart of the system and contains the Iridium satellite LBT L Band Transceiver The LBT can be thought of as the phone in the satellite phone system and the modem in the data system as it is the connection used to gain access to the Iridium network 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 different modules are added to define the function of the transceiver as a whole Phone versions contain a POTS and or DSC DSC in older units only module allowing the LBT to be dialed and interfaced with remotely Each Sky Connect 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 and in a pinch website browsing The Tracker system contains an additional module and offers an optional internal 12 channel GPS module Tracker uses the short burst data transfer portions of the Sky Connect suite though it can be coupled with any of the phone systems Any system can exist alone or co exist with another and upgrades can be done to any system at any time without incurring additional cost penalties The Iridium system can only be occupied by one call at a time whether it is voice data or Short Burst Data These systems ex
18. service 1 2 5 Aircraft type and registration number 1 2 6 Complete contact information for customer using the product 1 3 Antenna placement plan 1 3 1 Pay close attention to the length of coax from the antenna to RT 1 3 2 Follow manual instructions on placement near other Sat COM and Comm antennas 1 4 Notebook computer with tracker setup program CD included with RT Information that will be needed for configuration 1 4 1 How the event switches were wired 1 4 2 What type of switches MOM ALT Press 1 4 3 What phone numbers need to be entered optional 2 WIRING 2 Wire system as drawn you the installer are responsible to the FAA for methods and practices used during the installation 2 2 Continuity checks 2 3 Power polarity checks 2 1 Revision Date April 25 2005 Revision 2 02 C skyConnect 3 CONFIGURATION 3 1 Configure RT to work with event switches as connected in wiring 3 2 Configure external GPS to talk to Sky Connect RT Aviation or NMEA RS232 format data 3 3 Enter phone numbers optional 2 2 Revision Date April 25 2005 Revision 2 02 C sky Connect 3 INSTALLATION GENERAL PRIOR TO INSTALLATION Perform a visual inspection of the equipment for evidence of damage incurred during shipment A DISCUSSION ON SIM CARDS No testing can occur until a valid SIM card is installed in the transceiver and the PIN code turned off The account has to be activated with an Iridium service
19. shot of Tracker Setup program for setting switch types and rapid report criteria BUTTON SWITCH STATUS and CONFIGURATION Switch Types All Event inputs are selectable as either Momentary Latched toggle Squat or dialer inputs Momentary Switch requires a momentary press of greater than 5 seconds to be active Momentary events happen once on button press Toggle Switch requires external latching Latched events annunciate once as the condition is entered and once as the condition is exited Each Toggle switch is capable of causing a change in reporting rate from normal to rapid Squat Only one switch may be selected as a squat input The first switch selected to squat will be the only one read A squat switch is defined as a latched switch which is grounded while aircraft is on the ground If selected this switch will cause a slow reporting rate until the ground condition is lifted The Squat switch is not required to enter the enroute condition but is recommended for helicopters or other special purpose aircraft that may loiter in a small area while enroute Without a squat switch rate change from slow to normal is determined on an algorithm based on speed and distance from power on position 7 8 Revision Date April 25 2005 Revision 2 02 C sky Connect Dialer Tracker systems utilizing basic telephony require three dialer positions each representing one bit of data encoded to select a speed dialing position Do not selec
20. tray The dimensions are 5 75 x 1 125 with an overall depth of 2 8 and depth behind panel of 2 1 1 4 TRACKER WIRING Follow the installation drawing 1616 900 5XX for the interconnection of the Tracker system into the aircraft As always pay close attention to the notes that apply to that drawing Wiring of the Tracker system is mission specific Tracker can be entirely standalone or tied to multiple aircraft systems The Tracker system is designed to be extremely flexible with open architecture Switched input options are limited only by the customer and the specific capabilities of the GIS software used for aircraft tracking The Audio Controller for the Tracker SOP system requires approximately 80 ma at any voltage between 10 and 32 VDC and must be protected by an external fuse or circuit breaker Tracker SOP A does not use the Audio Controller The SOP dialer should be powered through either a bright dim switch or through a rheostat If not connecting the dialer to a dimmer buss connect to 14 28 VDC through a circuit breaker The dialer is entirely passive and can be dimmed through a range of 4 1 VDC The internal lights are LEDs and are designed to work with both 14 and 28v dimmers so plan you dimming scheme appropriately If two or more dialers are to be installed they may be wired in parallel with the addition of isolation diodes on the dialer lines Al A2 and A4 See wiring drawings for details 2 POSTINSTALLATION TE
21. what suits your installation PC connector may be used for upgrades and PC data calls Avoid long RSe3e runs in noisey enviroments may require an in line noise suppressor contact tech support PS 206485 1 connector AMP CPC with 206062 1 hood and H H H PS MEASOB 2ESg DT Tapa SS MSSSSS7ESSSEBISSNLBELE GPS antenna used in installations if GPS sensor installed in P8 and Hood P N DE 24657 tranceiver Configuration module is optional Terminal strip part number and make up customer optional Ps EE Wire dimmer to 5 28VDC or through 1 amp breaker in absense P7 P7 PTA1e 1KC install kit from NAT of dimmer buss P13 and Hood P N DA 20961 d Squat Collective WOW switch should be used for helicopter Pile Me4308 2 4F 37 pin female w DC24660 hood H H H ZE but optional for fixed wing A C Tracker 1 thru 4 may only be used for data calls do not install if not needed Tracker A excluded from need of extenal filtering Factory upgrades exist to add functionality to the AFF unit These include annuciators event inputs data and basic telephony Unswitched audio is shown here as an example wire to pilot s preference A switched input may be used if pilot so desires Must be RG174 or equiv less than 30 in length If configuration module is installed these wires must not be more then 8 long Aux connections may be used to operate external lites Mount in remote location for easy access Connect PC serial ceb
22. will be unable to make or receive calls SC1 Factory Use 2 PHONE TESTING 2 1 2 2 AIRCRAFT TO GROUND Using ground power turn on the Aircraft master avionics master or what ever is required to fully power all elements of the installed Sky Connect system The Iridium antenna must have an unimpeded view of the sky Operating next to a hangar can cause occasional brief signal interruption Allow at least one minute for the system to register on the Iridium network Using the international country code area code and number place a phone call i e 001 301 891 0600 If using an executive handset you can test speaker mode at this point as well GROUND TO AIRCRAFT A call to the aircraft from the ground can be done in one of two ways 1 call the aircraft number using the international code of 011 88 163 xxx xxxx where the xs are the given number 2 Call the Iridium phone number 480 768 2500 and then dial the 88 163 xxx xxxx number This option may not be available to all customers Use of this option depends on activation of this feature at time of purchase The second example is cheaper for customers calling within the US because it offers Iridium users a special rate per minute Note There are some inherent delays and audio quality degradation in the use of satellite communications These anomalies can come and go depending on current azimuth to the satellite in use and even specific satellite characteristics C
23. 0 in length If configuration module is installed these wires must not be more then 8 long Aux connections may be used to operate external lites Mount in remote location for easy access Connect PC serial ceble here for unit configuration Diodes are 1N4001 or equivalent Parts RevisTons and Notes Approved Mike Freuder Changed 12 APR 2005 16 42 Sky Connect Transce ver J1 P1 Non ESS Buss 11 to 33 VDC f Tracker Dash Number Chart 11 to 33 VDC 11 to 33 VDC aoe Tracker with GPS Gnd Tracker no GPS Gnd Tracker with Phone and GPS Gnd Tracker with Phone and no GPS 1 RSe3e In Hi SKY G0ASSS H Tracker AFF with GPS 1 RS232 In Lo L GPS Data From GPS Aviation or NMEA 0183 marine Tracker AFF no GPS 2 RS232 In Hi SETS LA 2 RSe3e Out Hi e Messenger Data To From RSe3e device 2 RS232 Lo os Note 3 Shield Event Switch 1 40AB8 7 Event Switch 2 41A22 Event Switch 3 seno i Event Switch 4 sano e Event Switch 5 sano Event Switch 6 asa Event Switch 7 seno _ e Event Switch 8 sno eg Note 4 L1 NL Annuciator 1 SOA22 8 KY 51422 Note 12 Annuciator 2 Amnuc tetor 8 Diagnostic Conn Annuciator 4 m et Note 19 Configuration Module W 1 VF NIN Congif SCL SKY SORS35 Config SCL Data Out SKY S3RS35 NSS 2 ont ESDA SE EE Config Data Out ESCHER Config Data In Dat
24. 203 02 X Flush Mount unpainted w Handset 1616 203 02 Flush Mount painted white w Handset 1616 200 02 Flush Mount painted White with black Handset 4 1 Revision Date April 25 2005 Revision 2 02 C skyConnect Description Components Product Requirements And Part Number 1616 200 02 X Flush Mount unpainted with black Handset 1616 295 xx Cradle w o power supply 1616 295 xx Cradle back plate only 1616 105 01 Transceiver Mounting Tray 1616 297 01 Cradle power supply 1616 103 01 Black replacement Handset Requires selection only of service 1616 102 02 AC powered battery charger provider and for spare batteries cradle type 1616 102 03 AC powered phone charger 1616 150 01U Upgrade kit for adding Tracker Requires credit with GPS to existing Executive and billing unit information for SBD service 1616 150 02U Upgrade kit for adding Tracker Requires credit without GPS and billing information for SBD service Executive Same as above Two transceivers two base Requires selection 1616 200 stations dual element antenna of service or dual antennas four provider and handsets and four cradles cradle type w chargers S67 1575 165 Dual Element Antenna 4 2 Revision Date April 25 2005 Revision 2 02 C sky Connect 1 2 EXECUTIVE COMPONENT SPECIFICATIONS Weight Base station Weight Each Cradle Base Sta Dimensions 1 02 Ibs 15 lbs phones 02 Ibs eac
25. C sky Connect Sky Connect Series Installation Manual Revision 2 02 Dated April 25 2005 Revision Date April 25 2005 Revision 2 02 C sky Connect TABLE OF CONTENTS LISFTOFRENDSION Sila IV INDEX OF ACRONYMS 3100 ul IGURA V 1 GENERAL INFORMATION PP s S 1 1 1 GENERAL arena 1 1 1 1 INIRODUC TION tanta n 1 1 1 2 SYSTEM DESCRIPTION QT Q 2222 2 un u awam pri e uu sirena 1 1 1 3 TECHNICAL SPECTIRICATIONN iii 1 3 2 TINS PALL AION PROCESS paia aa 2 1 E INSTPAPEPEATIONPDEANNING S o NE NE 2 1 1 1 Wiring detresse aac baia 2 1 1 2 SIM card activation aid e loi at oe e b INN s NNNM pM 2 1 1 3 Antenna placement plan visa oe e ee aue EXE ER E ERRANT IAS FERRE SERERE EE Ee 2 1 2 WIRING ee Ev 2 1 3 CONPIGURATION V ue n 2 2 3 INSTALLATION GENERAL E 3 1 PRIOR TO INSTALLATION nennen eene rhnn eren nennen nnns essen nnne n nnns sese nennen nns s esee rennen nnns nennen 3 1 A DISCUSSION ON SIM CARDS ii 3 1 SIM PIN REMOVAL ALL SYSTEMS E 3 1 GENERAL SYSTEM COMPONENTS THAT APPLY TO ALL SYSTEMS een 3 2 GENERAL INSTALLATION INSTRUCTIONS nennen eenennn nennen ente nn nnne n nre n nnne enne 3 3 1 ANTENNA PLACEMENT aee des ARANCE a i e aa a tire 3 3 2 ANTENNA CABLE TE 3 3 3 TRANSCEIVER STRUCTURAL MOUTING esses eese eene nennen rennen nennen eene ennt 3
26. CTIONS 1 ANTENNA PLACEMENT The Aero Antenna AT2775 L Band antenna should be placed as far as practical from other transmitting antennae A minimum of 30 inches is recommended to other L Band transmitting antennae The Iridium antenna is itself a transmitting antenna and as such an eighteen inch minimum spacing to GPS antennae is recommended The Iridium antenna requires full view of the sky above Shadowing and interference can occur when mounted near vertical stabilizers and other structures inherent to aircraft When used in conjunction with an internal GPS for Tracker a separate active Sensor 67 1575 39 GPS antenna is supplied See Figure 4 for antenna dimensions Note Inmarsat systems commonly referred to as Satcom will greatly interfere with the performance of the Iridium antenna This interference may appear to be intermittent with aircraft position as the Inmarsat transmitting antenna array is electrically steer able depending on azimuth to satellite Inmarsat will disrupt Iridium communications whenever active Inmarsat should be disabled when Iridium is in use alternatively filters are available for Inmarsat systems which essentially act as an Iridium bandpass filter Consult Sky Connect for more information The antenna should be mounted in accordance with the manufacturer s instructions and reference FAA AC43 13 2A The antenna should be properly bonded to the aircraft ground plane to aid in eliminating unwanted interference Su
27. D v c o E inside corner Figure 8 Cordless Handset Cradle Surface mount lacks flange and is cut to accommodate these d 2 02 1si0on Rev April 25 2005 Date 1s10n Rev UOHl23UU0 JAMO a pe19 buIBIeyI SIM Cel pa12810Jd euipoL LO OLL 9LOL 1equunu yed DOAEE LL SjueuunJjsu SNIeD ISNI Sig Vl mo GEN ow v E un en 2 Ki amp e Cai o E 4 9 Revision 2 02 Revision Date April 25 2005 Notes 1 Connect 22AWG spliced as shown to 18AWG 2 Optional switches require diode protection if connected to anything other than ground All audio wires are twisted pairs shield floats at one end All unused pins are reserved DO NOT connect anything to reserved pins Seng Hood PAN DI 000200 All wire numbers are examples use what suits your installation PC connector may be used for upgrades and PC data calls Avoid long RSe3e runs in noisey enviroments may require an in line noise suppressor contact tech support PS 206485 1 connector AMP CPC with 206062 1 hood and H H H PS MEASOB 2ESg DT Tapa SS MSSSSS7ESSSEBISSNLBELE GPS antenna used in installations if GPS sensor installed in P8 and Hood P N DE 24657 tranceiver Configuration module is optional Terminal strip part number and make up customer optional Ps EE Wire dimmer to 5 28VDC or through 1 amp breaker in absense P7 P7 PTA1e 1KC i
28. GPS information for SBD service 1616 050 03 RT for Tracker w phone and Requires selection internal GPS sensor of service 1616 050 04 RT for Tracker w phone no provider and GPS credit and billing information for SBD service 1616 050 05 RT for Tracker AFF with Requires credit internal GPS sensor and billing 1616 050 06 RT for Tracker AFF no GPS information for 1616 050 03 05 only AT2775 110GAW TNCF Iridium Antenna S67 1575 39 GPS Antenna 1616 500 03 SatTalk II Interface 1616 051 01 SOP Dialer Control Head with Code Blue lettering 1616 051 03 SOP Dialer Control Head with Under Fire lettering 1616 105 01 Transceiver Mounting Tray 1616 050 99 Tracker Setup CD ROM 1616 052 01 PC Interface Adapter for use with Tracker and External PC in high RFI EMI environments 1616 900 01 Tracker w GPS install kit contains Tray Connectors Iridium antenna GPS antenna Manuals Software 1616 900 02 Tracker no GPS install kit contains SBD service Revision Date April 25 2005 7 1 Revision 2 02 C sky Connect Description Components Product Requirements And Part Number Tray Connectors Iridium antenna Manuals Software 1616 900 03 Tracker SOP w GPS install kit contains Tray Connectors Iridium antenna GPS antenna Manuals Software 1616 900 04 Tracker SOP no GPS install kit contains Tray Connectors Iridium antenna GPS antenna Manuals Sof
29. IM card problem CURRENT GPS DATA WINDOW all auto detected Latitude Indicates the current Latitude from the GPS receiver Longitude Indicates the current Longitude from the GPS receiver Altitude Indicates the current altitude from the GPS receiver Selectable to read in feet or meters Ground Speed Indicates in knots the speed detected from the GPS receiver AIRCRAFT VEHICLE CONFIGURATION WINDOW Aircraft Type Aircraft type determines the parameters selected for the activating of the enroute condition Select as appropriate even if a squat switch not required is utilized 7 5 Revision Date April 25 2005 Revision 2 02 C sky Connect Registration 6 15 character identifier When used with Flight Explorer GIS software this number must accurately reflect registration though this information may be blocked from display if desired Some GIS packages will truncate data entered in the identifier window External GPS bps Indicates the data speed rate at which the GPS is sending to the Tracker if the external GPS is in use TRACKER CONFIGURATION WINDOW Message Interval User may select default or change these settings to desired rates SLOW 2 to 999 min This rate is the ground setting for Tracker reporting rate A start of flight message or removal of a ground on ground squat switch will cause an immediate switch to the Normal reporting rate The grounding of the ground on ground squat switch will ca
30. PC for programming the PC should not be connected directly to the installer provided female connector used to connect to the ICM s male connector Only pins 2 3 and 5 are used for configuration the remainder of the pins are used internally and damage can be done to the Tracker and the PC if these lines are connected to a PC inadvertently See wiring diagrams 24 TRACKER TESTING In order to fully test Tracker you will need access to a PC running Flight Explorer Tracker Edition or an approved GIS display system In the event that this is not available to you contact Sky Connect Technical Support where we can remotely aid in your testing Refer to Appendix A for additional troubleshooting advice The Installer can verify the proper wiring of every onboard component with a combination of the Tracker Setup program and the all in one annunciator light The Installer can be assured that their portion of the job is acceptable if the onboard unit consistently indicates that it is sending and completing messages This is indicated by a fast pulse as messages are sent at programmed intervals followed by a solid green indication It is the customer s responsibility to choose the manner in which they display their tracked aircraft not the installers 7 10 Revision Date April 25 2005 Revision 2 02 C sky Connect Note Only one Iridium source can occupy the network at one time If a Sky Connect voice option is installed and in use
31. Part Number FlightDeck 1616 300 01 RT for Phone system only Requires selection 1616 300 1616 350 01 RT for Phone with Tracker of service provider and internal GPS sensor includes GPS antenna 1616 350 02 RT for Phone with Tracker no GPS 1616 301 01 NAT PTA Dialing controller with Connector 1616 900 01 FlightDeck install kit contains Tray Connectors Iridium antenna Manuals AT2775 110GAW TNCF Iridium Antenna 1616 350 01 only 67 1575 39 GPS Antenna 1616 105 01 Transceiver Mounting Tray 1616 350 01U Upgrade kit for adding Requires credit Tracker with GPS and billing 1616 350 02U Upgrade kit for adding information for Tracker without GPS SBD service 5 1 Revision Date April 25 2005 Revision 2 02 C skyConnect 1 2 FLIGHTDECK COMPONENT SPECIFICATIONS USING NAT PTAI12 DIALPAD Regulatory Compliance DO 160D Env Cat AI DI BAB SBM UF XXXXXXZBABB UTX MXXXX Temperature Range 20 Celsius to 55 Celsius Altitude Range 50 000 feet Weight Unit Rack Hardware 63 lbs Physical Dimensions Depth 4 17 Inches behind panel including connector Width 5 75 Inches Height 1 12 Inches Power Requirements Voltage 18 30Vdc Power Requirements Current 25 Amps 27 5Vdc Lighting Power Req Current 1 milliamp 27 5Vdc 1 milliamp SVDC Inputs 150 Ohm amplified Dynamic Mic 250 mVrms Mic Bias 13Vdc selectable on off POTS Plain Old Telephone Service O
32. STING No testing can occur until a valid SIM card is installed in a transceiver the PIN code turned off and the account has been activated with an Iridium service provider Systems 7 3 Revision Date April 25 2005 Revision 2 02 C sky Connect 2 1 are generally shipped with a SIM card installed with the PIN code disabled and the service inactive The customer is responsible for this activation as the customer receives the bills for the phone use This process can take a day and should be done in advance of the installation testing TRACKER SETUP IMPORTANT you must exit the Tracker Set Up program before the unit will transmit data signals Power cycle the Tracker after configuration to make sure new settings are in use TRACKER SETUP is a small configuration and diagnostic program that is provided on CD ROM but can be emailed if necessary The program comes as an executable file and must be placed in a folder along with the two accompanying dll files that are provided Tracker Setup should run on all Windows operating systems 98 or newer Using a standard DB9 serial data cable not a null modem cable connect a computer with the TRACKER SETUP program to the installer provided diagnostic port of the Sky Connect Transceiver Turn power on to the Sky Connect system and all associated components If a status annunciator light is installed wait for the software revision to flash long blinks for major number short blinks for mi
33. Tracker Status Annuciator 2 SKY 74A22 Dialer Status Pilot Phones L Aux Tracker Status Lite e r Note 14 Squat Switch WOW AU ARRUGE over SE Event Switch SKY 90Aee SKY 91A22N Note 20 Aux Emergency Lite ROS Ehones io Gnd A C on Gnd Aux Code Under Fire Lite i Aux Dialer Status Lite gY 10A22N Gnd Audio Hi Pilot Mic Hi Event Switch Optional Switch closure Pilot Mic Lo Note 2 P N 1616 0S1 XX i PTT pass thru Pecos Configuration Module SSAPS P10 Note 19 P N 1616 500 03 e RL Dare Out PIT s esse 21 Sg Seng 2 ES Diagnostic Conn Audio Panel Config Data Out Config Data In Data Lo PTT Config Data In see __ U UOO Config Data Out NC Mic Lo Config Gnd SKY Gonos Config Gnd NC P O J1 P10 Mic Hi Config Pwr Config Pwr NC Shield NC NC NC Phones Lo NC Phones Right P N 1616 S0S 01 Phones Left Alternate Diagnostic Port Wiring W O Config Module customer supplied P4 SKY 3A22S SKY AG S Ciridiun N Tracker Dash Number Chart P N ATS775S TNC EZ Tracker with GPS Tracker no GPS Tracker with Telephony and GPS cs N Tracker with Telephony and no GPS P N S67 1575 39 Tracker AFF with GPS Tracker AFF no GPS UE Ce Tracker Dialer System HI Z Wiring Dwg e 1616 S00 SSO Approved Changed S MAR 2005 08 33 Sky Connect Transcelver J1 P1 Avionics Non ESS Buss SatTalk III 11 to 33 VDC DE 11 to 33 VDC 11 to 33 VDC Joe gt SKY 8A22 28V Gnd Note 4 Gnd SKY SAPEN Gnd
34. a Lo S s Contig Data In Config Data Out NC Cont CRA RD M Config Pwr Config Pwr NC Shield NC NC NC NC NC NC P N 1616 905 01 Alternate Diagnostic Port Wiring W O Config Module PC Data Connector P4 ADS 9g 1 SKY 3A225 5 1 b SKY 4A20S 3 s o mu i ES SKY SAS OI m N k A o N co SKY 6A20S TNC Ed P N ATS77S P N S87 1575 39 zi z oO P N 1616 050 0X see KE numbers T Tracker System Wiring Dwg 1616 300 500 Approved Changed S MAR 2005 08 36 Sky Connect Transcelver J1 P1 Non ESS Buss SatTalk II 11 to 33 VDC A P12 41 11 to 33 VDC A 11 to 33 VDC E 18 9 IV sky gaze 28VDC Gnd 28VDC Note 4 Gnd SKY SA22N Gnd Gnd Gnd Wa 1 Fa 1 RS232 In Hi n 1 RS232 In Lo hs GPS Data From GPS Aviation or NMEA 0183 mar ine Note 3 Comm Audio Hi SKY PROSS Comm Audio Hi Comm Audio Lo Audio Lo Mic Audio Hi Mic Audio Hi Shield SKY 7A22 Mote ue AUTO Enable Dtal Annunctator Panel Pliot s Phone Jack I P11 J1 SKY S0ASSS Phone Audio Lo Phone Audio R 1 H Phone Audio L Shield Note S 28VDC Dimmer Note May be Mono Event Switch 1 SKY UASSS Position Event Switch 2 Dialer A1 Event Switch 3 SKY 71A885 Dialer Ae Plot s Mic Jack N A Event Switch 4 Dialer A4 ESCHER Audio Lo i pass thru Configuration Gnd Event Switch 7 ES Code Under Fire Lite Event Switch 8 Emergency Annuciator 1 SKY 73A22
35. al amplification of the phone audio Operationally it is the same as the original Tracker SOP described in 3 3 without the SatTalk 2 Audio Controller 3 2 2 The Dialer used for the new system remains the same as the previous dialer described in paragraph 3 3 2 7 12 Revision Date April 25 2005 Revision 2 02 C sky Connect 3 3 TRACKER SOP Tracker is also capable of storing a limited number of phone numbers for quick dialing at the push of a button This is considered basic telephony and adds voice capability to the existing Tracker functions This is not a full featured phone like Executive FlightDeck or Classic This system is designed for specific mission critical applications Tracker SOP consists of a transceiver antenna additional GPS antenna with internal GPS use a Sat Talk 2 audio interface not included in the Tracker SOP A version a dial pad with a six position rotary switch and four input switch annunciators Contact Sky Connect for more information on configuration options Most audio panels only support 1 2 duplex or push to talk communications For obvious reasons this is somewhat limiting for phone conversations The reason Full Duplex audio panels are recommended for proper operation is to retain the full transmission capabilities of your on board communications transceivers In a full duplex system Comm 3 is devoted to the Satellite phone while Comm 1 and 2 are the VHF Transceivers When a call is i
36. al the country code area code and number followed by the pound key The pound key is required to alert the phone that the end of the dial string has been reached No call will be initiated without the pound key You will hear call progress tones followed by the ringing sound For calls within the US for example dial as follows 001 301 891 0600 where 00 is international access 1 is the country code for the US and 1s the end of the dialing string You may also pre dial before getting a dial tone by simply keying in the number then hit the green key to send the call as you would on a cell phone Optionally dialing strings can be stored in phone memory locations The phone may be completely shut off by holding down the red key This will save the rechargeable batteries from discharging Holding this same red key down will also turn the phone on Note The rechargeable batteries in the phone become a part of the circuit when the handset is placed in the cradle DO NOT USE ALKALINE OR OTHERWISE NON RECHARGEABLE BATTERIES Placing non rechargeable batteries in a charger is dangerous Do not store handsets without batteries in the charger Note Turning power on to the aircraft or buss powering the base station will cause the handsets to turn on Turning off the power to the base station WILL NOT turn off power to the handsets Handsets must be powered down individually It is recommended that the handsets be pow
37. alls will occasionally be dropped due to momentary signal loss in excess of 12 seconds This sometimes frustrating characteristic is a normal aspect of all wireless communications 8 2 Revision Date April 25 2005 Revision 2 02 C sky Connect 9 APPENDIX A Troubleshooting TROUBLESHOOTING THE SKY CONNECT SYSTEMS Table 1 Description of Problem Possible Causes Executive FlightDeck Classic only Unit has no external indication of Check power and ground connections for proper power polarity and to ensure no shorts or opens Verify 11 33 VDC at the 62 pin connector Check connector seating Contact Technical Support Power light comes on but register light Verify unit is outside clear of obstructions hangars remains blinking Check all antenna connections and cable Verify customers service plan is fully activated with service provider Verify SIM Card PIN is deactivated Verify that Inmarsat system if on aircraft is deactivated or properly filtered Verify cable length and type is appropriate to achieve not more than 3dB loss at 1 6 GHz Check antenna placement on aircraft to be free of obstructions or shadowing Executive handset reads line in use Another handset is off hook A data call is in progress Verify that the Transceiver is powered and that the off hook light is off Check wiring between Transceiver and Base Station for Intermittent opens or shorts of Tip Ring lines
38. als 1616 401 01 Handset Interface 1616 402 01 Hang up Cup 1616 403 01 Handset 1616 405 01 Handset kit AT2775 110GAW TNCF Iridium Antenna 1616 105 01 Transceiver Mounting Tray 1616 450 01U Upgrade kit to add Requires credit and Tracker with GPS billing information 1616 450 02U Upgrade kit to add for SBD service Tracker without GPS 6 1 Revision Date April 25 2005 Revision 2 02 C sky Connect 1 2 CLASSIC COMPONENT SPECIFICATIONS Weight Unit Hardware 80 Ibs Cradle Phone Physical Dimensions Length 8 5 Inches Width 2 0 Inches Height 1 5 Inches 2 00 Inches with phone in cradle Interface Physical Dimensions Length 1 75 Inches Width 3 50 Inches Height 1 375 Inches Inputs DSC DC level Outputs DC level Connectors RJ45 D sub 9 Cradle Mounting 4 4mm tapped holes Interface Mounting 4 6 mounting holes 1 3 CLASSIC STRUCTURAL MOUNTING The Sky Connect Classic should be mounted in accordance with standard practices found in FAA Advisory Circular 43 13 2A To mount the Classic Handset Cradle install 4 4mm screws into the rear of the cradle Mount the cradle to any suitable armrest interior panel drawer divider or other structural member The cradle can mount horizontally or vertically and has a locking detent Mount the handset interface box in a suitable location near the handset as the handset plugs directly in to the interface using an RJ 45 connec
39. amp breaker in absense P7 P7 PTA1e 1KC install kit from NAT of dimmer buss P13 and Hood P N DA 20961 d Squat Collective WOW switch should be used for helicopter Pile Me4308 2 4F 37 pin female w DC24660 hood H H H ZE but optional for fixed wing A C Tracker 1 thru 4 may only be used for data calls do not install if not needed Tracker A excluded from need of extenal filtering Factory upgrades exist to add functionality to the AFF unit These include annuciators event inputs data and basic telephony Unswitched audio is shown here as an example wire to pilot s preference A switched input may be used if pilot so desires Must be RG174 or equiv less than 30 in length If configuration module is installed these wires must not be more then 8 long Aux connections may be used to operate external lites Mount in remote location for easy access Connect PC serial ceble here for unit configuration Diodes are 1N4001 or equivalent Parts RevisTons and Notes Approved Mike Freuder Changed 12 APR 2005 16 42 Sky Connect Transcelver A NAT PTA12 J1 P1 Dialpad Audio Interface Non ESS Buss Audio Panel SKY 19A22 11 to 33 VDC A tU 11 to 33 VDC Note 17 11 to 33 VDC Unswitched Audio in E 1 s Ring Audio Hi M Unswitched Audio in Ring Audio Lo Gnd RIng Audio Opt tonal KU Shield ong I e Phone Audio Hi Com 3 Audio in CH Phone Audio Lo Shield I Mic Audio Hi Cn S MICC Cor L Lo
40. ance of the installation testing 2 1 TRANSCEIVER INDICATIONS AND PHONE SETTINGS Refer to Section VIII for a description of how 2 1 The transceiver indicates during normal operation 2 1 2 To test the phone 2 2 HOW TO DIAL CALLS Press the Hook key to get a dial tone Note If you do not have a dial tone at this point and hear 3 repeating melodic tones are heard do not dial Your SIM card is not de pinned See Appendix A for troubleshooting advice Dial the country code area code and number followed by the pound key The pound key is required to alert the phone that the end of the dial string has been reached No call will be initiated without the pound key You will hear call progress tones followed by the ringing sound For calls within the US for example dial as follows 001 301 891 0600 where 00 is international access 1 is the country code for the US and f is the end of the dialing string For complete instructions on how to use the PTA12 see the Northern Airborne Technology Manual 2 3 TROUBLESHOOTING TIPS Refer to Appendix A for troubleshooting advice 5 3 Revision Date April 25 2005 Revision 2 02 C sky Connect 3 OPERATIONS The Sky Connect FlightDeck system consists of the Sky Connect Transceiver and L band antenna as well as a Dzus rail mounted dial pad audio interface This system is designed for use in the cockpit utilizing the aircrafts headsets as the audio interface Wh
41. ata out Hi Diagnostics output Out 48 RS232 2 Hi Messenger output Out 49 Data in Hi Diagnostics input In 50 RS232 2 Hi Messenger input In 51 PC S RX Data Connections only In 52 RS232 1 Hi Serial GPS input In 53 Program mdl Factory Use Do Not Connect 54 Program RST Factory Use Do Not Connect 55 Event switch 8 Gnd Active configuration switch style In mom alt dial sqt 56 Event switch 7 Gnd Active configuration switch style In mom alt dial sqt 57 Event switch 6 Gnd Active configuration switch style In mom alt dial sqt 58 Event switch 5 Gnd Active configuration switch style In mom alt dial sqt 59 Event switch 4 Gnd Active configuration switch style In mom alt dial sqt 60 Event switch 3 Gnd Active configuration switch style In mom alt dial sqt 61 Event switch 2 Gnd Active configuration switch style In mom alt dial sqt 3 6 Revision Date April 25 2005 Revision 2 02 C sky Connect Pin Description Flow 62 11 33VDC positive voltage input In Note 1 Executive Classic and FlightDeck systems Ringer Lo Gnd Out Output to drive Piezio alert or light 100mA Tracker SOP systems Configuration strap for Audio Enable In Tracker SOP A Model DO NOT USE AUDIO ENABLE Note 2 Executive Classic and FlightDeck systems POTS Ring or In Out Tip Tracker SOP systems Mic Audio In In Tracker SOP A does not allow ful
42. being tested Purposes for these switches are defined by the end user For more clarity on this programming refer to the Flight Explorer Tracker edition operation manual Should you desire to use our Tech Support for these tests you will need to have available the Transceiver Serial Number IMEI aircraft flight ID and installed options configuration 7 11 Revision Date April 25 2005 Revision 2 02 C sky Connect With power applied Tracker will continue to generate position report updates at its programmed interval Once registered on the network Tracker interval reports are billed per hour of use including during the testing process Note Programmed interval directly affects customer billing Consult with end user regarding all available configuration options before accomplishing 3 OPERATION 3 1 3 2 TRACKER The Sky Connect Tracker system consists of the transceiver and L band antenna as well as an additional module in the transceiver The Tracker can be added to any of the above systems but works autonomously of them The Tracker can utilize a feed from most panel mounted GPS systems or its own internal GPS when equipped with separate active GPS antenna This feed of aviation data provides Tracker with aircraft flight parameters such as latitude longitude speed direction altitude and flight plan information if available The Tracker utilizes Short Burst Messaging over the Iridium network to send this flight i
43. call As a result the signal strength bars will alternate on and off 1 3 and 5 followed by 2 and 4 Throughout the duration of a data call Ringer This light will flash in a ringing cadence with any inbound call Power This light will remain solid at all times that external power is applied and the system is operational Off Hook This light indicates when a Executive or FlightDeck phone is off hook When this light is on you will hear dial tone or busy signal in the handset or headset Data Call This light indicates that DTR is high on the PC interface and likely that a data call is in progress This light is coincident with the flashing Signal Strength bars Voice Call This light indicates that a Voice call has connected and is in progress Register This light will blink while a unit is attempting to register with the network This process happens each time the unit is powered The light will go 8 1 Revision Date April 25 2005 Revision 2 02 C sky Connect solid once registration has occurred Registration implies that at some point at least one bar of signal strength was available for roughly ten seconds though a registered phone does not necessarily mean you currently have adequate signal strength for a call A registered unit means that a valid SIM card is installed an account is active with a service provider and the Antenna subsystem is sufficient to provide one bar of coverage Until registered you
44. d SIM card is installed in a transceiver the PIN code turned off and the account has been activated with an Iridium service provider Systems are generally shipped with a SIM card installed with the PIN code disabled and the service inactive The customer is responsible for this activation as the customer receives the bills for the phone use This process can take a day and should be done in advance of the installation testing 2 1 TRANSCEIVER INDICATIONS PHONE SETTINGS AND OPERATIONS Refer to Section VIII for a description of how 2 1 1 The transceiver indicates during normal operation 2 1 2 To test the phone 4 4 Revision Date April 25 2005 Revision 2 02 C sky Connect 2 2 EXECUTIVE HANDSET REGISTRATION In order to use your Siemens 4200 handsets you must first register all handsets to the base station in the aircraft If you are registering a new set of phones to the base station and want to de register an old set of phones please go first to the Reset instructions below Executive systems are shipped with handsets that are not necessarily assigned to the base station so this task should be accomplished in the field prior to the testing and use of the Executive system A handset that a remains Searching for an excessive time is either not registered or this is an indication that the base station is not powered 2 2 1 Be sure that the base station and the Sky Connect Transceiver are powered up 2 2 2 Power the p
45. different Verify that you are dialing an international access code followed by the Iridium number or that you are following the proper Two Stage Dialing procedures Contact your Service Provider Tracker Systems Tracker system light pulses and goes solid but winks off every five seconds It continues to pulse then goes solid followed by the wink off without any pause constantly trying to transmit No communication is being made with the Iridium Network Verify Signal Strength using Tracker Setup Program Verify unit is outside clear of obstructions hangars Check all antenna connections and cable Verify customers service plan is fully activated with Revision Date April 25 2005 9 2 Revision 2 02 C skyConnect Description of Problem Possible Causes Service provider Verify that Inmarsat system if on aircraft is deactivated or properly filtered Verify cable length and type is appropriate to achieve not more than 3dB loss at 1 6 GHz Check antenna placement on aircraft to be free of obstructions or shadowing Verify SIM Card PIN is deactivated SIM comes de pinned from factory but a change in SIM card in the field can cause problems Contact the Factory Tracker System light pulses goes solid but continues to wink off It does not attempt to resend the message immediately but waits until its scheduled interval to transmit again Light continues to wink o
46. e is free Status Annuciator Style This feature will be disabled in future releases of the software Please leave selected to All In One 7 6 Revision Date April 25 2005 Revision 2 02 C sky Connect Multi position Reporting designed to give high resolution to actual flight paths to allow medical operators for example to be able to bill for actual distance traveled as opposed to straight line distance This valuable tool accounts for deviations in course due to weather ATC etc while not significantly increasing message size cost Each position report will come with intermediate points leading up to the reported position For any given interval 5 10 or 15 intermediate intervals can be given thus increasing the number of points used for plotting distance This data can then be used for more accurate billing Example user may have 10 minute reporting watch their aircraft in real time on a GUI display On a twenty minute flight this might not appear more than a straight line but when set to 10 multi position reporting there will actually be 10 positions given for the 10 minute period in this case once per minute All of the messages are delivered in one packet thus saving the user money This tool is useful for users not using tracking for SAR purposes For accurate real time graphic display the regular reporting rate must be increased Tracker Status Iridium Modem Status Software Version IMEI Numbe
47. en used in combination with Executive party line functionality is obtained Cabin communications and conferencing are available via the dial pad audio interface when used in conjunction with a PBX The dial pad is used for the dialing and answering of calls Once connected to a call the flight crew is capable of communicating in a full duplex fashion directly through their headsets Sky Connect manufactures a number of Sat Com Headset audio interfaces to allow more flexibility depending on the specific aircrafts needs 5 4 Revision Date April 25 2005 Revision 2 02 Notes 1 Connect 22AWG spliced as shown to 18AWG 2 Optional switches require diode protection if connected to anything other than ground All audio wires are twisted pairs shield floats at one end All unused pins are reserved DO NOT connect anything to reserved pins Seng Hood PAN DI 000200 All wire numbers are examples use what suits your installation PC connector may be used for upgrades and PC data calls Avoid long RSe3e runs in noisey enviroments may require an in line noise suppressor contact tech support PS 206485 1 connector AMP CPC with 206062 1 hood and H H H PS MEASOB 2ESg DT Tapa SS MSSSSS7ESSSEBISSNLBELE GPS antenna used in installations if GPS sensor installed in P8 and Hood P N DE 24657 tranceiver Configuration module is optional Terminal strip part number and make up customer optional Ps EE Wire dimmer to 5 28VDC or through 1
48. er Messenger only systems In addition to the installed SIM card an IMEI must be recorded for customer activation on Tracker only systems The IMEI is located on the outside of the transceiver SIM PIN removal All systems If your SIM card has the PIN protection feature enabled you must enter the PIN code when prompted This PIN is normally disabled from the factory but may be requested on and will always be on when a SIM card other than the SIM Sky Connect inserted On the Executive FlightDeck systems the prompt for the PIN is a melodic three tone sequence Enter 1 PINCODE ST On a Classic handset you will be prompted to Enter Pin Do 3 1 Revision Date April 25 2005 Revision 2 02 C sky Connect so and press OK You will be prompted for the PIN each time the system is started unless the PIN is disabled This can be done on the classic handset by pressing Menu selecting Phone Setup Require SIM Card Off Consult factory for disabling instructions with Executive FlightDeck systems Note Do not attempt to make a phone call with an active SIM pin Changing the SIM card in the field to a different provider s SIM card necessitates the removal of the PIN for proper operation If a PIN is entered incorrectly three times you will lock the phone and you will be unable to do any testing until the problem is resolved by the factory Items required but not supplied Table 1
49. ered down and stowed in on board storage other than the cradles as a function of the pilot s power down checklist Press and hold the red End key until the handset powers down This will avoid inadvertent powering and discharging of the handsets and alleviate the concern of handset misplacement or theft 2 5 TROUBLESHOOTING TIPS Refer to Appendix A for troubleshooting advice 4 6 Revision Date April 25 2005 Revision 2 02 C skyConnect 3 OPERATIONS The Sky Connect Executive system consists of the Sky Connect Transceiver and L band antenna as well as a wireless base station up to four wireless handsets and flush or surface mounted charging cradles The wireless base station is mounted within the aircraft cabin and is the aircraft equivalent to the base station you would find in any wireless phone system for home use The Siemens 2 4GHz wireless handsets are fully functional phones that dial the Sky Connect Transceiver via the base station interface In addition to all of the functions you would find in a normal wireless handset multiple intercom and speakerphone functions are available allowing a great deal of flexibility in party line conferencing as well as cabin communications The handsets will work up to 300 feet from the aircraft while on the ground though this is not recommended in flight 4 7 Revision Date April 25 2005 Revision 2 02 inc imensions hes Flush Mount Cradle D Sky Connect EXECUTIVE
50. ff Valid GPS input is not available Last received GPS information is viewable in the Tracker Setup Program Verify unit is outside clear of obstructions hangars Check all antenna connections and cable Check antenna placement on aircraft to be free of obstructions or shadowing Unit was connected with reverse polarity and no longer operates or operates for a short time followed by power loss Contact Technical Support Tracker System light flashes software rev shortly thereafter the light goes solid and remains solid There are no transmissions and the light never winks even when it s sending interval has been passed Verify that you are not currently connected to the Tracker Setup Program or the diagnostic port If a separate Data connector 9 wire for PC calls has been installed check shielding of the cable You may need to install an Icarus Instruments data feed through connector Contact Technical Support Revision Date April 25 2005 9 3 Revision 2 02
51. floor board or cabinet using approved 6 hardware When choosing a location for the base station allow access to the small white reset button located on one of the large faces This white button is used for programming and resetting the base station to the handsets The 9 pin circular connector is all that is required to electrically connect the base station once it has been structurally secured in place 4 3 Revision Date April 25 2005 Revision 2 02 C sky Connect 1 4 WIRING 1 4 1 CRADLE WIRING Executive charging cradles each require power to be supplied and may utilize the same breaker as the base station but should be individually fused at the cradle to no more than Lo amp Follow the illustrations in drawing to connect the cradles Remove the two screws from the small cover below the charging mount Route 11 32 VDC through hole in cradle underside to V V In screw terminals Mechanically secure wires in terminals then provide internal strain relief for the cable Close the access cover and secure 1 4 2 TRANSCEIVER WIRING Refer to SECTION III 1 4 3 EXECUTIVE SYSTEM WIRING Follow the installation drawing 1616 900 100 for the interconnection of the Executive system into the aircraft As always pay close attention to the notes that apply to that drawing The Executive Base station requires a 1 amp pull able Circuit Breaker for external protection 2 POST INSTALLATION TESTING No testing can occur until a vali
52. h considered carry on items Length 6 88 Inches Width 2 00 Inches Height 4 56 Inches Length 8 25 Inches Cradle Dimensions Width 3 43 Inches Depth 1 25 Inches depth below flush mount Base Station Power Voltage Power Requirements Current 18 30Vdc lt 0 1 Amp 28Vdc Operating Frequency 2 4 GHz Cradle Power Voltage 11 32Vdc Cradle Power Current 0 1 Amp 28Vdc Inputs POTS Plain Old Telephone Service Outputs POTS Plain Old Telephone Service Connectors 9 pin Male Circular Amp PCB Screw terminals Mounting 4 6 tapped holes in cradle underside 4 6 holes through base station 1 3 EXECUTIVE STRUCTURAL MOUNTING The Sky Connect Executive components should be mounted in accordance with standard practices found in FAA Advisory Circular 43 13 2A 1 3 1 1 3 2 The remote phone cradles are designed for flush mounting either horizontally or vertically as they have a positive locking detent There are four tapped 6 holes on the underside of the cradle to allow specific mounts to be tailored to the aircraft Surface mount cradles are identical in mounting to the flush cradles but lack the flanged edge They are designed for use in drink rails on partitions or armrests They also may mount horizontally or vertically The base station must be located within the aircraft cabin and outside of complete aluminum enclosures The base station should be bolted to a suitable shelf panel
53. hing other than ground All audio wires are twisted pairs shield floats at one end All unused pins are reserved DO NOT connect anything to reserved pins Seng Hood PAN DI 000200 All wire numbers are examples use what suits your installation PC connector may be used for upgrades and PC data calls Avoid long RSe3e runs in noisey enviroments may require an in line noise suppressor contact tech support PS 206485 1 connector AMP CPC with 206062 1 hood and H H H PS MEASOB 2ESg DT Tapa SS MSSSSS7ESSSEBISSNLBELE GPS antenna used in installations if GPS sensor installed in P8 and Hood P N DE 24657 tranceiver Configuration module is optional Terminal strip part number and make up customer optional Ps EE Wire dimmer to 5 28VDC or through 1 amp breaker in absense P7 P7 PTA1e 1KC install kit from NAT of dimmer buss P13 and Hood P N DA 20961 d Squat Collective WOW switch should be used for helicopter Pile Me4308 2 4F 37 pin female w DC24660 hood H H H ZE but optional for fixed wing A C Tracker 1 thru 4 may only be used for data calls do not install if not needed Tracker A excluded from need of extenal filtering Factory upgrades exist to add functionality to the AFF unit These include annuciators event inputs data and basic telephony Unswitched audio is shown here as an example wire to pilot s preference A switched input may be used if pilot so desires Must be RG174 or equiv less than 3
54. hone by holding the RED button down until the unit turns on 2 2 3 Note Whenever OK is required press the soft key under OK 2 2 4 Press MENU 2 2 5 Go to H Set Settings using the round rocker switch press OK 2 2 6 Go to Reg Handset OK 2 2 7 Select Base 1 OK 2 2 8 All handsets must be registered to Base 1 Each handset will be issued its own intercom position 1 4 2 2 9 Enter a PIN of 0000 OK 2 2 10 Hold down the small white button on the base station until the phone responds with flashing and noises 2 2 11 Repeat for the 2nd phone One will display INT1 and the other INT2 Repeat as necessary for phones 3 and 4 2 3 RESETTING BASE STATION Resetting the base station deregisters all handsets previously registered to that base station Prior to power up hold down the white reset button on the base station Apply power and continue to hold down the reset button for 10 seconds Confirm handsets are deregistered by looking at handset display where searching should be displayed You will have to use the above procedure to re register all handsets that need to access that base station 2 4 HOW TO DIAL CALLS Press the green key to get a dial tone 4 5 Revision Date April 25 2005 Revision 2 02 C skyConnect Note If you do not have a dial tone at this point and hear 3 repeating melodic tones are heard do not dial Your SIM card is not de pinned Consult technical support Di
55. ield NC NC NC Alternate Diagnostic Port Wiring W O Config Module NC SKY 3AceS Note 15 SKY 4A20S REN pi SKY SAS BAM _ el pst Note 7 P N ATS778 TNC Tracker Dash Number Chart eg Tracker with Telephony and GPS P N S67 1575 39 cS N Tracker with Telephony and no GPS TNC P N 1616 050 OX See Chart for dash numbers Tracker SOP A System w o SatTalk Dwg 1616 900 554 Sky Connect Transcelver JI PI Non ESS Buss GPS Data From GPS Aviation or NMEA 0183 mai Note 3 Audio Panel Comm Audio Hi e Sea bc Com 3 Phone Hi Comm Audio Ee E l Com 3 Phone Lo Mic Audio e Com 3 Mic HI gt SKY 7422 Com 3 Mic Lo Adis Resia Dial Annunclator Panel Audio Shield i Configuration Gnd customer supp ied Shield 28VDC Dimme tch 1 2 3 3l e 3 Position Dialer A1 itch 2 x Dialer A2 Itch 3 a E Dialer A4 itch 4 Code Under Fire Emergency Tracker Status Dialer Status Aux Tracker Status Lite Aux Annuc Power Aux Emergency Lite Aux Code Under Fire Lite Aux Dialer Status Lite SKY 10A22N Gnd P N 1616 051 XX gt SKY 7B22 to Dimmer Buss Dial Annunclator Pane Event Switch Annuciator SKY 73422 Annuciator 2 SKY 74A22 28VDC Dimmer Position Dialer A1 Dialer A2 Dialer A4 Code Under Fire K Optional Switch
56. ist simultaneously but can not be used simultaneously Multiple transceivers and antennas are required for multiple channels of communication For clarity two users may be on separate handsets on the same call but two users can not be on separate handsets on different calls without a second transceiver antenna Similarly when a phone call is in progress Tracker will be unable to send SBD packets though as soon as the line is clear it will send its stored messages 1 1 Revision Date April 25 2005 Revision 2 02 5d SN 1 1o dx3 10614 euJe1u uone1s punoj5 WOON Ez c UPUMS N S PNIUYV 2 yoe1 paads uonisod Sd9 buimelg 1de uo 494924 NNICIYI H 3DovHul priu mai G je pej 12 uuo2 AS a m a Li mani CO guu luvy WC En E A La S Q g S E E S S B E 8 o Revision 2 02 Revision Date April 25 2005 1 3 C sky Connect TECHNICAL SPECIFICATIONS TRANSCEIVER Regulatory Compliance Temperature Range Altitude Range Vibration Temp Variation Power Input DC Spike Conducted Emissions Radiated Emissions Weight Unit Rack and Hardware Add Tracker Add GPS Add Messenger Physical Dimensions Length Width Height Power Requirements Voltage Power Requirements Current Transmit Power Average Transmission rate Operating Frequency Inputs Outputs Connectors Mounting
57. l Telephony Note 3 Executive Classic and FlightDeck systems POTS Tip or In Out Ring Tracker SOP systems Comm Audio Out Out 3 7 Revision Date April 25 2005 Revision 2 02 O O Ec Oo OO NN N V Tranceiver KEE TENDS Amr DM d AO 340 e TWO KUVO em 71123204 guy AO asw Figure 2 Sky Connect Transceiver Dimensions Revision Date April 25 2005 Revision 2 02 10 200 10 700 Figure 3 Transceiver Installation Clearances 3 9 Revision Date April 25 2005 150 4 Revision 2 02 Places DUIMEIpP uorej eisur euua1uy 1l 1eS uniptJ 10128uu02 ajeWa 10J ajoy aduesea D eid EYL 195 J3H ME l L dI SLL Uc 086 6 88 43H VIG OSE lt kl Zi n E kel s E KI lt lt om A cv o E Revision 2 02 Revision Date April 25 2005 1 75 REF 44 5 d 24 1 T WAS 1 900 3 50 DIA REF 48 3 88 9 218 229 5 5 5 8 DIA THRU 385 9 8 DIA X 100 C SINK 4 PLCS C SINK TO BE FREE OF PAINT Figure 5 Dimensions of the Sensor Systems GPS Antenna Revision Date April 25 2005 Revision 2 02 1 75 REF E 44 5 950 24 1 w s m 1 900 3 50 DIA REF 48 3 88 9 E 218 229 5 5 5 8 DIA THRU 385 9 8 DIA X 100 C SINK 4 PLCS C SINK TO BE FREE OF PAINT Figure 6 Dimensions of the Sensor Systems GPS Antenna Re
58. lable for configuration may change from time to time consult the factory for recent software developments and planned implementation schedule Revision Date April 25 2005 Revision 2 02 C sky Connect 2 2 CONFIGURATION SETTINGS Note The following is an explanation of what is seen on the Tracker Setup Software screen Revisions of the software are possible check the website to make sure you have the current version The following may differ with revisions TRACKER STATUS WINDOW Software Version Auto Detected This value is displayed as an aid to determine the current version of internal software the Tracker is running Can be used to determine if an upgrade is required GPS Source Auto Detected This field indicates the type of GPS data string that is coming into the Tracker and is an aid in troubleshooting problems Tested interfaces include Garmin UPSAT Except CNX80 Trimble and Honeywell panel mount formats as well as NMEA feeds Contact factory for additional interface capabilities IRIDIUM MODEM STATUS WINDOW all auto detected IMEI Number Indicates the serial number of the LBT internal to the Tracker State Gives the state the internal LBT is presently in Status Indicates if the internal LBT is in communication with the CPUs on board the Tracker Signal Strength Indicates the strength of the Iridium signal being received by the LBT Will range from 1 5 An indication of a minus here indicates a S
59. le here for unit configuration Diodes are 1N4001 or equivalent Parts RevisTons and Notes Approved Mike Freuder Changed 12 APR 2005 16 42 Handset Sky Connect Trenscelver P N 1616 403 01 HE Non ESS Buss 33 VDC 33 VDC SRY TATSS 33 VDC Classic Handset Gnd Classic Handset Connector Gnd i Interface 1616 401 01 Gnd Connector Note S Shield DSC Enable SKY 20A22 DSC Up Ink StS Ts SKY 21A22S DSC Down ink SKY 22A22S DSC Gnd SKY 23A22 Ringer Hi SKY 24A22 Ringer Lo SKY 25A22 RJ4S Connector o O00 0 2 PC Data Connector P4 NS SIM Card SKY 3APES 1 9 Note 6 b 1 H bl SKY 4AceS SEI E ane BEES pls e ss l Reader 3 RJ45 Connector Ni O0 1 CO O M O0 1 CO OO E L e nb za iridium N Card reader adapter P N AT2 77S TNC Ei P N 1616 400 01 Phone only 1616 450 01 Phone with Tracker and GPS 1616 450 02 Phone with Tracker no GPS ann Classic System Wiring Dwg 1616 900 400 Approved Changed 11 MAR eO0S 11 51 C sky Connect 7 TRACKER SYSTEM 1 INSTALLATION Be sure to cover Section III as it pertains to the transceiver installation and antenna installation that applies to all systems 1 1 TRACKER SYSTEM COMPONENTS Table 1 Description Components Product Requirements And Part Number Tracker 1616 050 01 RT for Tracker with internal Requires credit 1616 050 GPS sensor and billing 1616 050 02 RT for Tracker no
60. m overall length of DSC buss is 30 feet including compressed coil cord 2 POSTINSTALLATION TESTING No testing can occur until a valid SIM card is installed in a transceiver the PIN code turned off and the account has been activated with an Iridium service provider Systems are generally shipped with a SIM card installed with the PIN code disabled and the service inactive The customer is responsible for this activation as the customer receives the bills for the phone use This process can take a day and should be done in advance of the installation testing 2 1 TRANSCEIVER INDICATIONS PHONE SETTINGS AND OPERATIONS Refer to Section VIII for a description of how 2 1 The transceiver indicates during normal operation 2 1 2 To test the phone 2 2 HOW TO DIAL CALLS Dial 00 the country code area code and number followed by the OK key The OK key is required to alert the phone that the end of the dial string has been reached No call will be initiated without the OK key You will hear call progress tones followed by the ringing sound For calls within the US for example dial as follows 001 301 891 0600 OK where 00 is international access and the 1 is the country code for the US Optionally dialing strings can be stored in phone memory locations The Classic handset should not be unplugged while the system is on If necessary to unplug the handset or if the handset was unplugged inadvertently
61. nect Transceiver should be mounted in accordance with standard practices found in FAA Advisory Circular 43 13 2A The Transceiver is approved for mounting outside the pressure vessel See Figures 2 and 3 for unit and tray dimensions The structural mount consists of a mating tray with a self locking vibration resistant knurled thumbscrew system The tray should be bolted to a suitable avionics shelf using approved 6 hardware The 62 pin High Density D subminiature connector and 1 to 2 antenna connectors are all that is required to electrically connect the box once it has been structurally secured in place 4 TRANSCEIVER ELECTRICAL INSTALLATION Wiring must be done in accordance with FAA AC43 13 1B or most current revision A crimp tool meeting Mil Spec M22520 2 01 and a positioner are required to ensure consistent reliable crimp contact connections for the 62 pin D Subminiature connector A 2 amp pull able Circuit Breaker is required for external protection of the Sky Connect Transceiver All wiring is 18 22AWG and should use Mil Spec 22759 16 or 27500 18 wire or wire deemed appropriate to the aircraft type by the governing aviation regulatory agency See schematic for your system for wiring examples Note Sky Connect telephony systems are generally considered non essential and should be treated as such when selecting the appropriate bus for power The system should be placed behind a nonessential bus However if the mission of the aircraft
62. nformation packet to ground terminals for the monitoring of fleet aircraft Regular reporting intervals of twelve seconds to greater than 30 minutes can be set for the triggering of a flight information packet Three separate rates can be selected based on flight status In addition to interval reporting changes in flight parameters proximity to waypoint or events can trigger reports Events can be triggered by contact closures such as a squat switch or an emergency button DC level inputs may require external diode protection While no external switching or annunciation is required for the Tracker system to operate it can contain up to eight external event switches and four status annunciators It is recommended that at least one annunciator be installed in a suitable location which would provide verification of a completed message transaction This annunciator would alert the user to the system status and a reception or lack thereof of the flight information packet at the Iridium Gateway TRACKER SOP A 3 2 1 Tracker SOP A is a new version of the original Tracker SOP but without the need for the SatTalk II audio controller component The audio operations of the SatTalk 2 are now included in the Tracker SOP A transceiver This brings the operational characteristics of the Tracker SOP A model to the same as any remote mounted Comm transceiver This unit can be operated with or without an audio panel and needs no extern
63. nitiated Comm 3 is selected and communications happen as they would on a phone without the need to push to talk Meanwhile the pilot is still able to monitor his on board radios and if necessary key the Mic to allow conversations on the VHF Transceiver In a half duplex audio panel keying on any transceiver line will cause the muting of all other sources of incoming audio Safety of flight can be compromised in this fashion by muting an incoming call from ATC while holding down the key to communicate on the phone It is strongly recommended that a Full Duplex audio panel such as the PS Engineering PMA7000B or NAT AMS50 be used when interfacing the SatTalk II or the SOP Model A as a transceiver 3 3 1 SAT TALK 2 NOT USED ON SOP MODEL A The SatTalk II audio controller is a device for integrating the audio of the Tracker SOP transceiver with an aircraft audio panel For proper operation the audio panel must support Full Duplex operation In lieu of this the audio panel will require PTT in order to allow transmit audio to pass PTT is not required by the Sat Talk controller The SatTalk 2 controller is not required for Tracker R T s with part number ending in 03A or 044A A pair of headset jacks on the controller permits the connection of a general aviation dual plug headset if a headset level interface is desired The system must be used as either a transceiver interface to the audio panel or a headset level interface but not bo
64. nor number The light will then extinguish Wait approximately 2 minutes and double click on the TRACKER SETUP icon Note Sky Connect does not support the use of Serial USB converters There has not been enough reliable use of these devices If your computer does not have a 9 pin serial port purchase a PCMCIA Serial converter This type of adapter does not rely on software drivers and is hardware driven The configuration menu will appear Fields are logically laid out to help you configure the Tracker system Remember to save your changes to the Tracker if values are changed These changes are stored internally and on an optional configuration module which will be polled at every startup Restart the system and your new values are in use These configurations remain in use until TRACKER SETUP is entered again and the values are changed Remember to save changes if values are changed in any of the internal pages of the Setup program Other valuable information can be obtained from the TRACKER SETUP program including the IMEI of the LBT the status of communications with the LBT External or Internal GPS last reported position altitude speed as well as active inputs The settings entered in this page both control the flow and the data sent to the Sky Connect message switch Inaccuracies or inadvertent changes in flight ID with respect to IMEI identification are flagged at the Sky Connect message switch for customer protection Parameters avai
65. nstall kit from NAT of dimmer buss P13 and Hood P N DA 20961 d Squat Collective WOW switch should be used for helicopter Pile Me4308 2 4F 37 pin female w DC24660 hood H H H ZE but optional for fixed wing A C Tracker 1 thru 4 may only be used for data calls do not install if not needed Tracker A excluded from need of extenal filtering Factory upgrades exist to add functionality to the AFF unit These include annuciators event inputs data and basic telephony Unswitched audio is shown here as an example wire to pilot s preference A switched input may be used if pilot so desires Must be RG174 or equiv less than 30 in length If configuration module is installed these wires must not be more then 8 long Aux connections may be used to operate external lites Mount in remote location for easy access Connect PC serial ceble here for unit configuration Diodes are 1N4001 or equivalent Parts RevisTons and Notes Approved Mike Freuder Changed 12 APR 2005 16 42 SKY 8B22 Sky Connect Transce ver J1 P1 SKY 8C22 Non ESS Buss 11 to 33 VDC 11 to 33 VDC 11 to 33 VDC SKY 8A22 Gnd 1a SKY 7A22 Gnd A ds a O SKY 19422 Execut Ive Base Station Note Must not be inside metal enclosure or Notes POTS Tip aluminized honeycomb structure POTS Tip See POTS Ring POTS Ring shield PC Data Connector 28VDC P4 Gnd CN SKY 3A225 1 9 Note 6 57 L ORY FREES di Tz P N 1616
66. ode Area Code Number e g 001 301 891 0600 Cancel Figure 13 Sample screen shot of Tracker Setup program for setting preset phone numbers 7 23 Revision Date April 25 2005 Revision 2 02 C Sky Connect 8 TELEPHONE INDICATIONS and SETUP 1 TRANSCEIVER INDICATIONS The Sky Connect Executive Classic and FlightDeck transceivers are equipped with diagnostic lights on the side of the transceiver The performance of these lights is very important as an aid to diagnosing performance problems This section describes the purpose of each light On power up all lights will come on briefly followed by a blinking of the software revision Software major designator is indicated by the green Signal Strength bars while minor increment is indicated by the yellow bars Two green flashes followed by three yellow flashes indicates version 2 3 Signal Strength When registered with the network these lights will indicate your current signal strength by displaying zero to five bars Anything less than three bars will usually result in a failed call attempt Signal strength changes as azimuth to satellite changes In the air this will not have much effect On the ground satellite azimuth can have you wondering why you have no reception or can t register with the network If on the ground do not waste time get as far from the hangars as you can Signal strength is not indicated when in a data
67. omplete transmission or invalid GPS data Incomplete transmission will be followed by a fast pulse retry transmission at the selected interval Tracker units with basic telephony Tracker SOP utilize the second annunciator as the dialer status lamp This single light status lamp indicates as follows Light off No call in progress Light on Call connected Light flashing Incoming ring cadence if call not initiated at SOP Dialer Outgoing ring cadence if call is initiated by SOP Dialer is ringing but not connected Grounding the appropriate dialer buttons will select a corresponding speed dial position The annunciator will flash one to six times to allow the user to verify the position of the number the intended to dial after which the outgoing ring cadence will begin A call is terminated either after the outgoing cadence has begun or after the call is in progress by grounding any of the dialer bits An external SOP dialer unit is available for dialing annunciating phone conditions See page 23 of this section for a picture of the dialer and setup for entering numbers 7 9 Revision Date April 25 2005 Revision 2 02 C sky Connect 2 3 CONFIGURATION MODULE The configuration module if used should be installed within 8 to the 62 pin connector and secured to the harness The configuration module stores settings external to the transceiver and also provides a female connector for easy connection to a PC via straight PC cable for s
68. onfig Data In Config Data Out Cont 1g Cont ig NC NC NC Mic Audio Hi Shield Gnd Comm Audio Lo Comm Audio Hi Mic Audio Lo Mic Audio HT P N 1616 50 ternate Diagnostic Audio Panel Com 3 Mic Hi Com 3 Mic Lo Com 3 Phones Hi Con 3 Phones Lo customer supp ied Diagnostic Conn P10 Tracker Dash Number Chart Tracker with GPS no GPS with Telephony end with Telephony and Tracker AFF with GPS AFF no GPS File c cktcrt my schematics sky connect sch Title Sky Conn Dug Sheet Tracker SOP Sus Dialers No 8 Rev Drawn Mike Freuder Engineer Created 31 JAN 2005 C Approved Changed _2 MAR 2005 2 Sky Connect Transce ver 11 to 33 VDC 11 to 33 VDC 11 to 33 VDC Gnd Gnd Gnd 1 RSe3e In Hi 1 RS232 In Lo Comm Audio Hi Comm Audio Lo Mic Audio Hi Shield Audio Enable Configuration Gnd J1 P1 Non ESS Buss Heer 2a SKY 1A18S I I 1 a P SKY 8A22 a I I GPS Data From GPS Aviation or NMEA 0183 marine b Note 3 SKY CAOS SKY 7A22 Dial Annunctator Panel P11 41 SatTalk II 28VDC 28VDC SKY SA22N Gnd Gnd Comm Audio Hi Audio Lo Mic Audio Hi to Dimmer Buss Note 12 Shield Gnd Comm Audio Lo Comm Audio Hi Mic Audio Lo 28VDC Dimmer Mic Audio Hi Position Dialer A1 Dialer A2 Dialer A4 Code Under Fire Emergency Tracker S
69. provider Systems are generally shipped with a SIM card installed with the PIN code disabled and the service active The customer is responsible for this activation as the customer receives the bills for the phone use This process can take a day and should be done in advance of the installation testing This is why we ask for the activation information at the time of the sale In the event that the customer provides a SIM card it must be de pinned or the system will get blocked Contact the manufacturer if you intend to change SIM cards Sky Connect recommends 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 to test its operation A de pinned activated SIM is required before this can happen The SIM card is the identity of the user and thus must travel with the user In this case the user s SIM card is installed in the Sky Connect transceiver This process should only need to be accomplished at initial installation After user activation the phone 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 Sky Connect or a qualified avionics shop to have the SIM card replaced in order to keep the SIM card account matched with the user While activation is not required a valid SIM card must also be installed in Track
70. r State Get Tracker Settings Version 4 2bD 300003000822830 SETUP GPS Source Status Signal Strength Save New Settings MMEA Simple Modem Responds OK Status Idle Current GPS Data o Latitude 30 29 74 N Altitude 32768 Meters Feet EO Longitude 893942W Ground NA knots TrackerSetup Options Aircraft vehicle Configuration Aircraft vehicle Airplane Ls Tail ID Number Loaneri External GPS bps 9600 EI Tracker Configuration SIONE DON SEDE E Button Switch Status Message Intervals 0 2 0 2 1 minutes Message Retry Interval 30 seconds MultiPosition li B Interrupt PC Session 8 No O Yes after 10 minutes Interrupt Voice Call No _ Yes after 10 minutes Remote PW admin Figure 10 Sample screen shot of the Tracker Setup program for setting report intervals aircraft type tail number and general trouble shooting information 7 7 Revision Date April 25 2005 Revision 2 02 C sky Connect Current Value Hardware Configuration RapidRate When On Button 1 i gt OFF PRESS BUTTON No SC Button 2 OFF DIAL BUTTON Button 3 OFF DIAL BUTTON Button 4 OFF DIAL BUTTON Button 5 OFF TOGGLE BUTTON ze No Button 6 OFF TOGGLE BUTTON ze No Button 7 OFF TOGGLE BUTTON Mo Button 8 z OFF TOGGLE BUTTON ze Ho si Figure 11 Sample screen
71. rface preparation should include the use of Alodine 1001 or similar The antennae listed above as well as the Sensor S67 1575 109 Iridium antenna are all TSO d and approved for mounting on pressurized vessels Antenna installations on pressurized vessels require FAA approved design and engineering data whenever a pressure vessel requires penetration due to connector mounting holes Approved designs can be obtained from aircraft manufacturers STC data specific to the antenna or DERs Seal antenna in accordance with FAA AC43 13 2A 2 ANTENNA CABLE When routing antenna cable avoid high current wiring other transmitting antenna cables and sharp bends Antenna cable should be selected to obtain 3dB max loss at 1 6GHz The installer is responsible for providing antenna cables Use the following chart as an aid to determine the appropriate cable type for your required installed length Follow industry practices when assembling the TNC connectors RG 142 coax cable is recommended in installations up to 20 feet in length alternative cable types are listed below 3 3 Revision Date April 25 2005 Revision 2 02 C skyConnect Pre assembled cable lengths are available from EMTEQ ECS and PIC Table 3 Cable Length EMTEQ ECS PIC 15 feet PFLX195 100 352001 833141 15 25 feet PFLX240 100 311601 833141 25 40 feet PFLX340 100 311201 855122 35 60 feet 310801 822089 3 TRANSCEIVER STRUCTURAL MOUTING The Sky Con
72. t dialer if your unit does not support basic telephony The Tracker SOP Dialer should not be confused with Executive Classic or FlightDeck as they are full featured telephony systems Active Switch Inputs Grounded input All inputs generate an immediate special message of type X to be determined by the user at the display end of the chain not the aircraft Coordination is necessary at an early stage between the installation facility and the end user Pressing button 1 will generate a 1 message at the Flight Explorer GIS and indicate an active button 1 on an aircraft notification email This 1 is assigned a specific meaning at the display end of the transmission system i e The Flight Explorer screen All buttons can be configured for any type of switch need For example button press eight can serve the function of a lit latched emergency switch while also producing a more intensive reporting rate while buttons 2 4 are set to dialer Active Lamp Outputs Ground on output Four separate annunciators are available to aid in diagnosing the health and status of the installed Tracker system The annunciator 1 status lamp output indicates as follows Immediate on with power up followed by software revision flashed in Dash dot presentation Off System not available one minute after startup Solid Status OK GPS valid last message attempt successful Fast pulse Transmitting Solid with blink off every 5 sec Inc
73. t Explorer for display including Destination Speed Altitude Flight Plan etc Using the TRACKER SETUP program you can test most of the features of the installation with the exception of the full network test Any contact closures that were installed for use with Tracker can be tested at this time as well No messages will be compiled or sent while the Tracker Setup program is connected and running Messages will resume roughly one minute after the program is discontinued From the main page you can verify the GPS position speed and altitude The units IMEI and GPS input type are displayed when known The Iridium Signal strength 0 5 and Modem status are displayed and updated in real time From the Switch configuration page you can select the type and rate of each switch input but you can also test to verify the input The Setup program samples the incoming switches every ten seconds to see if they are active The switch status will display as on if a ground is applied to the corresponding pin and off if the line is floating Each closure will also generate a specific event at the PC running Flight Explorer software The program must have an assignment for the event triggers to accomplish their task The assignment for contact closure 2 for example can be assigned on the Flight Explorer PC terminal to annunciate Mission Aborted The important element here is that the contact closure number is accurate to the specific switch
74. tatus Dialer Status Shield Event Switch 1 Event Switch 2 Event Switch 3 Event Switch 4 Event Switch 7 Event Switch 8 Annuciator 1 Annuciator 2 SKY 70A22S P N 1616 500 03 SKY 72A225 Audio Panel Com 3 Mic Hi Com 3 Mic Lo Aux Tracker Status Lite Com 3 Phones Hi Aux Annuc Power Com 3 Phones Lo Aux Emergency Lite Aux Code Under Fire Lite Aux Dialer Status Lite EC SKY 10A22N Gnd SKY 73A22 SKY 74A22 Optional Switch closure customer supp ied Note 2 Novant Switch P N 1616 0S1 XX Note 14 Squat Switch SKY 90A22 e SKY 91A22N Gnd A C on Gnd Event Switch Diagnostic Conn Configuration Module SES RIO Config SCL Data Out Conf ig SDA Data In Config Data In Data Lo 2 Config Data Out NC Config Gnd NC Config Pwr NC NC NC NC Note 19 Congif SCL Conf ig SDA Config Data Out Config Data In Config Gnd Conf ig Pwr Shield SKY 60A22S e 3 DL SKY 61A22S SKY B2A202S A U SKY 3A225 P N 1616 905 01 SKY 4AeeS z s o z o A IO 01 Q CO VW Alternate Diagnostic Port Wiring W O Config Modu 4 SKY Aces IM b GS so I I SKY 6A20S I I 5 b KD P N ATS77S TNC Ei Tracker Dash Number Chart P N S87 1575 39 ors N Tracker with GPS TNC Tracker no GPS Tracker with Telephony and GPS Tracker with Telephony and no GPS Tracker AFF with GPS Tracker AFF no GPS Approved Changed S MAR 2005 08 31 Note 8 P N 1616 050 0X See Chart for
75. th For more information on a headset level interface portable installation or use with a handheld Motorola 9505 consult the Sat Talk 2 Installation Manual Rev 2 1 or higher When used as a Transceiver interface the installation is unseen to the pilot The unit is remote mounted The Privacy button has no function and the Power button must be left on for operation Incoming calls are monitored by selecting Comm3 or appropriate communications selector When a phone call is in progress the Mic audio on Comm3 is selected to allow Full Duplex communications See specific audio panel operation manual for more details 7 13 Revision Date April 25 2005 Revision 2 02 C sky Connect 3 3 2 SOP DIALER See Figure 12 in rear of this section for a visual of the SOP Dialer The Tracker SOP Dialer is an entirely passive switch annunciation panel designed with many of the most commonly used features from various special operation projects The dial pad is Dzus rail mounted and contains four switching annunciators and a rotary encoding switch The Dialer works with the Tracker SOP transceiver to allow quick access of six pre programmed numbers These numbers programmed by the user with the Tracker Setup program are used for contacting dispatch centers emergency contacts and maintenance facilities Your particular operation may utilize the six positions in an alternative way The system is designed to be fleet wide so that the number in position two is
76. the same for all pilots sharing the same mission The rotary knob is used in conjunction with the Call button to initiate an outbound call answer an inbound call or terminate a call The Call button also houses the phone status annunciator For more expanded operation see section 3 2b One momentary switch is provided for unscheduled position reports and the annunciator functions as the Tracker Status light See section 3 2b for information on the status annunciator Two latching switches are included one labeled Emergency and the other generally labeled Code These switches light to indicate they are currently active The SOP dialer can be tailor built to suit including legends though the dialer described above 1616 051 01 is the only stocked dialer Dialers can be wired alone or in parallel with isolation diodes on dialer lines see drawing for multiple position use in aircraft In either case the depressing or releasing of any switch will cause the associated lines at the transceiver to be grounded or open to ground thus initiating a message or call Each switch is a discrete input to the transceiver In the case of the Call switch a ground is applied to any one of three discrete inputs depending on the particular switch position selected 7 14 Revision Date April 25 2005 Revision 2 02 Notes 1 Connect 22AWG spliced as shown to 18AWG 2 Optional switches require diode protection if connected to anyt
77. tor 4 Sinks 100ma to Ground Out 19 Configure SDA Do Not Connect to other than Sky Connect Configuration Module 20 Event switch 1 Gnd Active In 21 11 33VDC positive voltage input In 22 Ground Input Gnd 23 DSC Gnd Classic Systems only Gnd 23 DPL Ground Classic Systems only SOP A PCM receive Gnd In 24 Program TX Factory Use Do Not Connect 25 DSC Downlink Classic Systems only Out 26 DSC Enable Classic Systems only Out 26 DPL Enable Classic Systems only SOP A PCM FS In 27 PC CTS Data Connections only Out 3 5 Revision Date April 25 2005 Revision 2 02 C sShuyconnect Pin Description Flow 28 Configure SCL In 29 Com Audio Hi POTS Tip SEE NOTE 3 Out 29 Com Audio Hi Out 30 Diagnostics Gnd Gnd 31 RS232 1 Gnd Gnd 32 RS232 2 Gnd Gnd 33 Shield Configure ground Gnd 34 Program Md0 Factory Use Do Not Connect 35 Shield Configure ground Gnd 36 PC GND Data Connections only Gnd 37 PC S TX Data Connections only Out 38 PC DTR Data Connections only In 39 PC RTS Data Connections only In 40 Program Rx Factory Use Do Not Connect 41 Ringer Hi Input Voltage Out 42 11 33VDC positive voltage input In 43 Ground Input Gnd 44 NC 44 PCM clock Classic System only SOP A IDT DPL Audio Out Out 45 PC RI Data Connections only Out 46 PC DSR Data Connections only Out 47 D
78. tor The ringing piezo alert for the handset is contained within the interface box A trim pot on the interface allows selection of alert volume Four 6 holes are provided for Classic interface mounting If the interface is mounted behind interior an auditory test should be done with engines running to ensure adequate alert volume Handset cable should feed through a hole in the interior located behind the mounting cradle for cleanest aesthetics Note The Classic Handset and cradle are considered small parts in accordance with FAR 25 Appendix F Part 1 Paragraph a 1 v when used in a single handset configuration and therefore meet the flammability requirements of FAR 25 853 Multiple installations of handsets will not meet the flammability requirements of FAR 25 853 The handset cord meets or exceeds the electrical wiring flammability requirements of FAR 25 Appendix F Part 1 Paragraph a 3 6 2 Revision Date April 25 2005 Revision 2 02 C skyConnect 1 4 CLASSIC WIRING Follow the installation drawing 1616 900 400 for the interconnection of the Classic system into the aircraft As always pay close attention to the notes that apply to that drawing Classic handsets interface via an external interface box using a 9 pin D subminiature connector and the handsets RJ 45 connector A maximum of 30 between transceiver and the Classic handset is allowed RG 316 or equivalent wiring must be used for the DSC bus data signals Maximu
79. tware 1 2 TRACKER SOP COMPONENT SPECIFICATIONS Weight SAT II unit hardware 9 Ibs SAT II controller Physical Dimensions Length 6 5 Inches Width 3 375 Inches Height 1 1 Inches Mounting Flange plate included uses 4 6 screws in a 6 25 x 2 5 pattern Connectors DB 37 male Standard Headset and Mic Jacks Power 10 33 VDC 80 ma max Weight SOP Dial pad 8 Ibs SOP Dial pad Physical Dimensions Height 1 12 inches Width 5 75 Inches Total Depth 2 8 Inches Depth Behind Panel 2 Inches Connectors DB 15 male Power 8 32 VDC 80 ma max 7 2 Revision Date April 25 2005 Revision 2 02 C sky Connect 1 3 TRACKER SOP STRUCTURAL MOUNTING The Tracker SOP A has eliminated the use of the SatTalk 2 audio controller and only the RT and the DOP Dialer need be considered for mounting If you are using the original version of the SOP system P N 1616 050 03 04 the Sat Talk 2 audio controller normally is installed using a flange mounting plate that is supplied and may be attached to the bottom of the audio controller using the existing screws that secure the bottom plate Using the flange plate the controller is mounted using four 6 screws ina 6 25 by 2 5 pattern Alternatively a bracket can be fashioned to strap the controller in place The SOP Dial pad is a Dzus mounted unit and will mount in any standard Dzus rail Adapters are available to convert Dzus for use in a standard 6 25
80. use a return to the Slow reporting rate NORMAL 2 to 999 min This rate will be selected during enroute conditions when not selected to the Rapid rate Changes to Rapid rate can be coincident with a message report of type X to be defined at the GIS display level RAPID 2 to 999 min This rate will be selected during enroute conditions when a selected toggle is engaged enter the Rapid reporting rate Changes to Rapid rate can be coincident with a message report of type X to be defined at the GIS display level Any switch is configurable to be a Rapid rate reporting switch when active Active Grounded condition Message Retry Interval Time before retry selectable from 10 to 999 sec In the event of poor signal coverage and a failed transmission attempt this setting will select the retry rate for queued messages Interrupt PC Session Voice Session user selectable from 0 to 999 min In a single channel system one transceiver one Iridium antenna the system is capable of only one communication at a time be it voice data or short burst data In installations where tracking is a primary concern this override time allows disconnect of the session that is preventing a SBD data communication of position If selected on interrupt time is based on the integer entered here if selected off a voice or data call may go on indefinitely during which time no position reports will be sent Queued messages are sent by the Tracker when the lin
81. utputs 100mW into 600 or 150 Ohms 1 3 FLIGHTDECK STRUCTURAL MOUNTING The Sky Connect FlightDeck should be mounted in accordance with standard practices found in FAA Advisory Circular 43 13 2A The FlightDeck dial pad is the NAT PTA12 This is a Dzus mounted unit and will mount in any standard Dzus rail Adapters are available to convert Dzus for use in a standard 6 25 tray For specific mounting information refer to the NAT PTA12 Installation Manual For specific audio interfaces refer to appropriate installation manual or contact Sky Connect Instruments Tech Support for assistance 1 4 FLIGHTDECK SYSTEM WIRING Follow the installation drawing 1616 900 200 for the interconnection of the FlightDeck system into the aircraft As always pay close attention to the notes that apply to that drawing For complete wiring instructions of the Northern Airborne Technology PTA12 see the current revision of that manual from NAT 5 2 Revision Date April 25 2005 Revision 2 02 C skyConnect 2 POST INSTALLATION TESTING No testing can occur until a valid SIM card is installed in a transceiver the PIN code turned off and the account has been activated with an Iridium service provider Systems are generally shipped with a SIM card installed with the PIN code disabled and the service inactive The customer is responsible for this activation as the customer receives the bills for the phone use This process can take a day and should be done in adv
82. vision Date April 25 2005 Revision 2 02 1 25 31 8 DIA CLEARANCE HOLE FOR CONNECTOR NAMEPLATE Figure 7 Dimensions for the Sensor Systems GPS Antenna 3 13 Revision Date April 25 2005 Revision 2 02 C Sky Connect 4 EXECUTIVE SYSTEM 1 INSTALLATION Be sure to cover Section III as it pertains to the transceiver installation and antenna installation that applies to all systems All systems are capable of having the Tracker options installed For Tracker installation and system testing and operation see Section VII 1 1 EXECUTIVE SYSTEM COMPONENTS Table 1 Description Components Product Requirements And Part Number Executive 1616 100 01 RT for Phone system only Requires selection 1616 100 1616 150 01 RT for Phone with Tracker and of service internal GPS sensor includes provider and GPS antenna cradle type 1616 150 02 RT for Phone with Tracker no GPS 1616 101 01 Base Station with connector AT2775 110GAW Iridium Antenna TNCF 1616 150 01 only 67 1575 39 GPS Antenna 1616 900 01 Executive install kit contains Tray Connectors Iridium antenna Manuals Selection of Cradles and Phones Handsets are Black w Gray Face 1616 203 01 Surface Mount painted Black w Handset 1616 203 01 X Surface Mount unpainted w Handset 1616 200 01 Surface Mount painted Black with black handset 1616 200 01 X Surface Mount unpainted with black Handset 1616
83. ystem configuration The purpose of the module is to alleviate the need to reprogram to an individual aircraft if units are shifted amongst the fleet Removal and replacement of the Sky Connect Transceiver with a different unit will keep the Users stored settings the same though a tail number to serial number configuration mismatch will be logged as a security procedure via the iridium network Theft for re use of the Sky Connect Tracker is impractical as not only do we know who you are but exactly where you are Regardless the configuration procedure only needs to occur once or when a configuration module is replaced An additional use for the configuration module would be to update all of the phone numbers in a fleets systems This becomes a time saving device allowing one module to program each aircraft only necessitating the update of the individual tail numbers The male connector on the ICM connects via 6 wires to the 62 pin connector of the Tracker system The female connector is the configuration port for both the ICM and the Tracker itself If the configuration module is in place during programming settings are saved to the transceiver and to the ICM If the ICM is connected at startup the configuration is read from the ICM If it is not present at startup the system uses its internal memory which is re flashed by the ICM at startup when connected NOTE While the female connector on the ICM is designed to be connected directly to a

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