CDP-300 Installation Manual
Contents
1. Ce o gt VW SKYTRAC YOUR SATCOM TECHNOLOGY PARTNER CDP 300 Installation Manual DOC0449 Applies to PN 104 300 01 104 300 02 Document Revision 01 005 March 4 2013 SkyTrac Systems Ltd 200 170 Rutland Road North Kelowna BC Canada Tel 1 250 765 2393 Fax 1 250 765 3767 Web www skytrac ca Email support skytrac ca Copyright 2013 SkyTrac Systems Ltd All rights reserved SkyTrac Systems Ltd Document Revision History Rev ECO Description Date Author 01 000 172 Initial Release July 28 2009 T Ratch 01 001 283 Incremented revision number for document version control Mar 03 2010 G Ross Corrected title of section 2 2 01 002 266 Added short term operating temperature in 2 4 Oct 14 2010 Y Liu Added warranty period starts from date of purchase from 01 003 368 SkyTrac Systems Dec 14 2010 Y Liu Corrected warranty statement Added ESD caution Removed approval column from revision history Corrected DOR Aek qualification string and table in section 2 5 Corrected part dunez 2011 Goss numbers and added asterisk to note in section 1 3 4 Updated warranty information Changed the minimum Ee operating voltage to 20 5V Removed references to CDU Neier le Caution The CDP 300 contains static sensitive circuitry that could be damaged from large electrostatic discharges directly into the connector pins Use care when handling the CDP 3002. Type Part Num Description Compatibility CDP 300G 104 300 01 CDP 300 with antiglare display filter 101 200 01 101 200 03 105 300 01 105 300 02 105 300 03 105 300 04 CDP 300C 104 300 02 CDP 300 with NVIS B display filter 101 200 01 101 200 03 105 300 01 105 300 02 105 300 03 105 300 04 Note Please contact STS Client Services for software version requirements Document Rev 01 005 Restricted Proprietary and Confidential Information DOC0449 Page 9 of 23 SkyTrac Systems Ltd 2 SYSTEM SPECIFICATIONS 2 1 General This section contains the specifications and a list of the physical and electrical requirements for the CDP 300 2 2 Power Requirements for the CDP 300 System Table 2 Power Requirements Component Power Requirements CDP 300 Input Voltage 20 5 to 32 VDC 28 VDC nominal Average Power 7 W typical 12W maximum 2 3 Digital and Analogue l Os Table 3 Digital and Analogue I Os Current Sinking Output Maximum 32 VDC 200 mA Meets requirements of TIA EIA 232 F standard Reese PONS TX maximum 13 2 V RX maximum 25V Meets requirements of TIA ElA 485 A standard RS 485 Ports Fail safe receiver Open circuit Refer to the CDP 300 User s Guide DOC0500 for configuration options 2 4 Physical Specifications Table 4 CDP 300 Physical Specifications Oper
3. ssccssecceeceeseeeseseeeeneeeeeeeeeesaeseseeeeeeeeeseaesesaaeenseeeeseeseaseaeenseaenes 7 Document Rev 01 005 DOC0449 Page 4 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 1 GENERAL 1 1 Introduction This publication provides technical information for the installation of the CDP 300 The CDP 300 when used in conjunction with the DVI 300 provides an interface to read and send email messages receive and answer sat phone calls and display ISAT 200 parameters The CDP 300 along with the DVI 300 provides a rich interface for accessing the global voice and text communications features of SkyTrac System s Iridium based ISAT 200 This combined interface is referred to as the CDP DVI If you are operating in CDP DVI mode refer to the DVI 300 Installation Manual DOC0456 for details about installation of the DVI 300 1 2 Contents This manual contains procedures and other information for installing the CDP 300 system It is divided into the following sections Section 1 General This section contains a product overview and an overview of the contents of this manual Section 2 System Specifications This section contains tables that list the power requirements and electrical specifications for the components of the CDP 300 Section 3 Mechanical Installation This section contains the procedures for the physical installation of the CDP 300 system components Section 4 Electrical I
4. No Limitation of installation is identified 8 MAINTENANCE AND CONTINUED AIRWORTHINESS 8 1 Continued Airworthiness The backlighting of the CDP 300 is provided by light emitting diodes LEDs Periodically inspect your CDP 300 for non functioning LEDs If an LED is non functioning have the CDP 300 replaced by an authorized technician 8 2 Maintenance Instructions With the exception of the lighting as explained in Section 6 1the CDP 300 does not require any maintenance 9 FIRMWARE UPDATES The CDP 300 is equipped with a serial port to enable firmware updates to the device Detailed instructions on how to update the firmware are included in the CDP 300 User s Guide Refer to SkyTrac s website at www skytrac ca for a list of firmware updates available or contact SkyTrac Client Services IMPORTANT NOTE Depending on the time period between shipping of your unit and the physical installation at your location firmware upgrades may become available It is recommended that you contact SkyTrac Systems Client Services to confirm if any upgrades are available for the unit when installing Document Rev 01 005 DOC0449 Page 22 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 10 CDP 300 HUMAN MACHINE INTERFACE 10 1 General This section provides a brief description of the CDP 300 human machine interface components For more detailed information on each of these components refer to the CDP
5. o Check the connection between CDP 300 and DVI 300 if installed o Check the connection between CDP 300 and ISAT 200 If installed activate the DVI 300 emergency switch The CDP 300 will display the emergency message De activate the emergency switch and confirm the unit returns to normal mode Verify if the emergency message is cleared and the Home menu is displayed Use the CDP 300 to place a sat phone call to a ground based telephone Confirm that the call is established and both parties can hear each other clearly Adjust the system volume if necessary To make calls using the CDP 300 voice communication must be enabled in the ISAT Contact the Program Manager with respect to SkyTrac Systems to have voice communication enabled in the ISAT The ISAT must receive its programming instructions through the satellite link and therefore needs a view of the sky in order for the voice communication to be enabled Document Rev 01 005 DOC0449 Page 18 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd e The CDP 300 brightness can be controlled in two automatic modes and these two modes must be tested separately if they are to be used The brightness mode can be selected through the CDP System menu o Place the CDP 300 in Optical Sensor Mode Locate the sensor in the front panel Cover the sensor with your thumb Verify if the LED brightness decrease Remove your thumb from the sensor and verify if the LED bri
6. 5 2 ISAT 200 Configuration The CDP can also be used to configure the ISAT 200 Please refer to the ISAT 200 Installation Manual DOC0334 and CDP 300 User s Guide DOC0500 for additional information The CDP can be used to set the ISAT 200 DC Mic Bias on or off set the Microphone input range set the speaker volume and select ring tones via the menu system Document Rev 01 005 DOC0449 Page 17 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 6 POST INSTALLATION TESTS 6 1 General This section contains instructions for tests to be performed after the installation to confirm that the system has been installed correctly Post installation tests are mandatory for all ISAT 200 installations The following post installation function test must be performed after installation of the CDP 300 6 1 1 Function Test Setup Ensure that the wiring harness is securely installed Ensure that the ISAT 200 antenna has a clear view of the sky Obtain the CDP 300 User s Guide for reference during the function test Function Test Apply power to the CDP 300 DVI 300 if installed and ISAT 200 systems Ensure the ISAT 200 is operating and that its antenna has a clear view of the sky Verify if the CDP 300 displays a start up message After a few seconds the CDP 300 will display the Home menu if it successfully establishes communication with the DVI 300 and the ISAT 200 If you get an error message
7. Reserved for future use Do not connect 13 Reserved Reserved for future use Do not connect 14 Reserved Reserved for future use Do not connect 15 Reserved Reserved for future use Do not connect Document Rev 01 005 Restricted Proprietary and Confidential Information DOC0449 Page 15 of 23 SkyTrac Systems Ltd 4 2 2 CDP 300 DB 9 Connector Pin out Table 8 CDP 300 DB 9 Connector Pin Descriptions Pin Pin Name Function Description 1 N C Do not connect 2 RXD Receive Data 3 TXD Transmit Data 4 DTR Data Terminal Ready 5 GND Ground 6 DSR Data Set Ready 7 RTS Ready To Send 8 CTS Clear To Send 9 N C Do not connect 4 3 ISAT 200 System Installation Reference Drawings Approved installation drawings from the appropriate STC should be used for installation of the ISAT 200 System of which the CDP 300 is a component Please refer to the ISAT 200 System Installation Reference Drawings DOC0461 when an STC is not applicable 4 3 1 CDP 300 Installation Wiring Diagram Notes The following notes pertain in general to the CDP 300 Installation Wiring Diagram Illustrations All signal and power shield continuity must be individually maintained through bulkhead disconnects Please refer to the ISAT 200 System Installation Reference Drawings DOC0461 or applicable STC drawings for additional installation notes IMPORTANT NOTICE All system interconnect cables m
8. should be set to commonly used frequencies with the squelch open VOR DME receivers should be selected for display If possible set up a DME ramp test set on the frequencies indicated and adjust the output until the flags are out of view The transponder and encoder should be monitored with ramp test equipment Set the output of the transponder test set to 3db above the output necessary to achieve 90 reply If possible set the ADF to a nearby navigation station Operate the CDP 300 unit for at least 10 minutes During this time use the keypad on the CDP 300 to navigate the menus and send text messages or make satphone phone calls These operations will exercise the CDP 300 communications link to the DVI 300 or ISAT 200 The EMI test for the ISAT 200 See ISAT 200 Installation Manual DOC0334 exercises the ISAT 200 functionality including satellite communication and should be completed separately for new ISAT 200 installations or when audio is added to an ISAT 200 installation Observe the GPS for any degradation in satellite status availability or flags Listen for any noise or detected audio signals on the VHF Communication Listen for any noise or detected audio signals on the VOR LOC receiver audio look for any movement of flags or needles on the VOR LOC GS navigation display s Observe the transponder for any loss of reply or spurious reply List the power plant fuel and other electric instruments on the EMI RFI Test Report and note
9. 300 User s Guide DOC0500 10 2 Display The CDP 300 includes a 20 character display for displaying emails phone numbers and configuration information 10 3 Keypad The CDP 300 has a four button keypad which is used for scrolling through the menu and accessing different configuration options and error messages 10 4 Ambient Light Sensor Beside the display is an Ambient Light Sensor which will automatically detect the ambient light level 10 5 RS232 Programming Port The RS232 programming port is used for updating the CDP 300 firmware directly from a computer with Windows XP or later Document Rev 01 005 DOC0449 Page 23 of 23 Restricted Proprietary and Confidential Information
10. Taa ea a aE DE 7 Sele O DEE EE EE 7 A O B PESO EE 8 1 3 3 CDP 300 Installation Components ooncccnnncnnnncnnccnocccccnrnnnn cnn nn cnn cnn 8 134 er D WA Mel EE 9 2 System Specifications EE 10 2 1 General ee eene A A EA a ee ve ee ee IAEA 10 2 2 Power Requirements for the CDP 300 System nr ran 10 2 3 Digital and Analogue Q5 iirin eege unde eine iaa 10 2 4 Physical SpecifICAIONS tii NEEN 10 2 5 Safety Compliance EE 11 2 5 1 Environmental Test Summary c ccecececeeeeeeeeeeeeeneeseeeecaeeecaaeedeaaeseeeeesaeeesaaeeseeeeseaeeesnaeeseaeeesaes 12 3 Mechanical Installation cuisine narco ienaa aaea hadat adada eia aeaaaee aiaee ianiai 13 3 1 Eae e EEE EE et eege eege AE e ee 13 3 2 installation im te EE 13 3 3 Malin Installation EE EE 13 3 4 CDP 300 Component Weights ooooocnccccincccnoccccnonanononnnonoccnoncnnnn canon r ranas 13 3 5 Unpacking and Inspecting the System Component ooocccnccccnoccconocanonoccnonccnnnnnnn nn nn nan n cnn canaria 14 3 01 Product Mountains coli ria a oa 14 3 6 Installation Material Smain iaa 14 3 6 1 Installation Kit for the CDb 200 nono nan nnnnnnn nn nn nn nana nn cnn nn nannanans 14 31622 O O O OO 14 4 Electrical InstallatiON cidcid Gunes susnccaeenueveveesceaccpasuuedsuentoastedndsveenevunccteaudendenceuaseabantesscucsee 15 4 1 GOneral clas ta ot E E Be ale a Ee WEE Me e 15 4 2 Biet lef Si EE e 15 4 2 1 CDP 300 DB 15 Connector Pinot 15 4 2 2 CDP 300 DB 9 Connector Pin OUt ccccc
11. Vibration UG 9 0 Explosion Proofness X 10 0 Water Proofness X 11 0 Fluids Susceptibility X 12 0 Sand and Dust X 13 0 Fungus Resistance X 14 0 Salt Spray X 15 0 Magnetic Effect Z 16 0 Power Input B 17 0 Voltage Spike B 18 0 AF Susceptibility X 19 0 Induced Signal Susceptibility X 20 0 RF Susceptibility X 21 0 RF Emissions M 22 0 Lightning Induced Transient Susceptibility X 23 0 Lightning Direct Effects X 24 0 Icing X 25 0 Electrostatic Discharge X 26 0 Fire Flammability A Document Rev 01 005 DOC0449 Page 12 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 3 MECHANICAL INSTALLATION 3 1 General This section contains procedures for the mechanical installation of the CDP 300 Included are unpacking instructions a table listing the weight of each component and instructions for completing the physical installation of the CDP 300 3 2 Installation Limitations The following installation regulations must be adhered to When installing the CDP 300 the installer must have a working knowledge of aircraft electronics installation and be a holder of either an FAA Repairman s Certificate or a Transport Canada equivalent All installations should meet the requirements of FAA advisory circular AC43 13 1B 3 3 Main Installation Tasks The main tasks for this installation are listed below 1 Unpack and inspect the system components Check the contents of the installation kit agains
12. any anomalies that occur while transmitting Assess the results If the aircraft is equipped with an autopilot or stability augmentation system then test fly the aircraft and verify that operation of the CDP 300 unit does not have adverse effects on these systems After checking for gross effects at a safe altitude fly an approach with each of the different navigation systems coupled to the autopilot ILS GPS ETC and look for any anomalies Document Rev 01 005 DOC0449 Page 20 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd If the installed system passes all of the applicable EMI tests then no further action is required If interference is observed then the interference must be assessed against the appropriate standards of airworthiness for the system in question For example it is permissible for a VFR certified GPS to lose navigation capability under certain conditions providing that it recovers properly and promptly but it is not permissible for an IFR Approach certified GPS to be affected in the same way A complete discussion of all the standards of airworthiness to be applied in assessing EMI effects is beyond the scope of this document Document Rev 01 005 DOC0449 Page 21 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 7 AIRWORTHINESS LIMITATIONS 7 1 Installation Limitations No Limitation of installation is identified 7 2 Operation Limitations
13. ating Temperature 15 C to 55 C Short Term Operating 40 C to 70 C Temperature 30 minutes Operating Altitude Max Operating 55 000 ft 16 760 m L 5 7 145 8 mm Size H 1 8 46 7 mm W 3 1 78 5 mm excluding connectors Weight 0 33kg 0 73 Ibs Mounting DZUS rails using 4 1 4 Turn Studs Document Rev 01 005 DOC0449 Page 10 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 2 5 Safety Compliance CDP 300C and CDP 300G are qualified to the DO 160E environmental category A1 F1 CXB SBM UG XXXXXXZBBXXXMXXXXX The tests demonstrated that the CDP 300 does not exhibit any unsafe performance when exposed to the specified environmental test conditions and that installation of the CDP 300 in accordance with the installation instructions in this Manual will not pose a hazard to the continued safe flight and landing of the aircraft Document Rev 01 005 DOC0449 Page 11 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 2 5 1 Environmental Test Summary The following table summarizes DO 160E Environmental Testing for the CDP 300 Table 5 Environmental Testing Summary Section Test Name Category A1 4 0 Temperature and Altitude F1 4 5 4 In Flight Loss of Cooling 5 0 Temperature Variation C 6 0 Humidity X Operational Shock a Crash Safety e SBM 8 0
14. by 20 symbols and a keypad 5 keys The keypad is used to navigate through the menu structure of the CDP 300 The CDP 300 is currently available in 2 models CDP 300G and CDP 300C CDP 300G has a commercial grade antiglare filter and a green backlit panel CDP 300C has a NVIS B green filter The CDP 300 has a current sinking output for a buzzer and dimmer voltage measuring circuits for standalone CDP mode The CDP 300 is designed to provide an easy to use interface to the ISAT 200 The interface enables the user to make Sat phone calls by using a preprogrammed quick dial list from anywhere in the world Pre programmed text messages are also supported allowing users to get important information to the ground in an efficient and timely manner without distraction from the mission The CDP 300 can also function in combination with the DVI 300 This enables the CDP 300 to display the characters entered by the DVI 300 keypad 1 3 3 CDP 300 Installation Components An installation kit PN 106 300 01 is offered for installation of the CDP 300 The parts list of the Installation Kit can be found in the CDP 300 Installation Kit Bill of Materials DOC0464 The installation kit contains a mating connector to the CDP 300 back shell and all necessary hardware to attach it Document Rev 01 005 DOC0449 Page 8 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 1 3 4 CDP 300 Models Table 1 CDP 300 Models
15. cccnconcccncncnnnnnnoncncnnnnnnnnononanannnnnnnnnonnnnnn aran ono cnn an anna nn nn cnn 16 4 3 ISAT 200 System Installation Reference DrawingS oooooncccnncconnconnncccnonccnnonn nana nac c cnn rana 16 4 3 1 CDP 300 Installation Wiring Diagram Notes 16 5 Configuration of the CDP 300 ccccsseeceeeseeeceeeseeeeeesneeeeenseeeseensneeseeeneaesesnsnaeseseneaeseensnaesesesnaesennenes 17 5 1 CDP 300 Brightness Configuration cccccccecceeeeeeeeceeeeceeeeeceaeeeeaaeeeeeeeseaeeeseaeseeaaeseaeeeseeeesaeeseaeeeeed 17 5 2 ISAT 200 Contiguration ees Age EE aed nla deeded di edd dete 17 6 POSE INStallatioN L tze ee SNE SNE iii 18 6 1 GO Header 18 6 1 1 Function Test Setup iniciara tada iia 18 A Klee leie RT EE 18 Ga Pees EE Cl KEE 20 7 Airworthiness Limitation NEE NENNEN ninia sdanounddeteunvs ARENS AE ee EEN 22 7 1 Installation Wun e i 3 sce a teenth Retest tad 22 7 2 Operation ue 22 8 Maintenance and Continued Airworthiness 2 2 2 0 00ssssssssesssesesssessessssessssnssesssssssessesseneneseneeenes 22 8 1 Continued Airworthiness cccccccononccnccnnnnnnnnacnnnnnnnnonononancnnnnnnnnnnnnnnnnn cnn nono nan nana nnn nono nana nana n nn nn a 22 8 2 Maintenance ln Coen TEE 22 Document Rev 01 005 DOC0449 Page 3 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 9 Firmware Updates i 2c ccccccccccrssecscccecencceretencterssscctesecenncestesecteredcnceessssentes evencuusse p
16. ected edenctessescetededenccoereteecters 22 10 CDP 300 Human Machine Interface c ccccsccesseeeeseeeeeseeeeeseeesnaeensneeeneeeeseaesesaeeenseaeeeeeeeseaeseseeeenseaeeennes 23 10 1 Contra a A AAA na 23 10 2 tele A e a 23 EC WR ele MEET 23 10 4 Ambient Light Ener eege deu Adasen een natin Haina ean es 23 10 5 RS232 Programming POrt EE 23 List of Tables Tabl e 1 ein RO E 9 Table 2 Power Requirements cssseecccsseeeceeesneeeeensneeeeenseeeeeenseaeeeenseeeeeseseeeeeseseaeeeseseeeeesaseeeeeseseeeeesnseeeseees 10 Table 3 Digital and Analogue W OS sssssssssuunsuunuunnunnnunnnuunnnunnnnnnnunnnunnnunnnnnnnunnnnnnnnnnnnnnnnnnnnnnnnnnn annn nnnn nannan nnna 10 Table 4 CDP 300 Physical Specifications s sssunseunseunreunneunreunnnunnnunnnunnnunnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn ennn nnnn nannan 10 Table 5 Environmental Testing Gumman sssssesnssunseunreuneunnnunnnunnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn ennnen nennen nann 12 Table 6 Component Weights cssecceseceseeeeeeeeeeneeeeeeneeesaeeenneeeneeaesaaesasaaesgeeeeseaeeesaesaseeeseeeeessaeeesnaesenseaeees 13 Table 7 CDP 300 DB 15 Connector Pin Descriptions cccseessseesseeeneeeeeeeeeeseaeseseeeeneeeeseeesesneneeeseeeees 15 Table 8 CDP 300 DB 9 Connector Pin Descriptions ecccseeeseeeeseeeeeeeeeeeeneeseaeseneeeeeeeeeeseaeseseenenseeeees 16 List of Figures Figure 1 ISAT 200 System Block DiaQraim
17. ghtness increases o Place the CDP 300 in Dimmer Bus Mode Turn off the aircraft dimming bus and verify that the backlighting for the keys is ON and the LED display is bright for day operations Now turn ON the aircraft dimming bus and observe that the LED Display dims to night operation brightness levels Gradually adjust the dimmer bus voltage Verify the backlighting and led display follow the dimmer bus voltage Document Rev 01 005 DOC0449 Page 19 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 6 1 3 EMI Test Note The CDP 300 is installed as part of the ISAT 200 system Please use ISAT 200 System EMI RFI Test Template DOCO478 RO1 000 for EMI test procedures The purpose of this test report is to verify that the operation of the CDP 300 does not interfere with basic aircraft systems and avionics The CDP 300 has to be installed and function tested with the ISAT 200 and or the DVI 300 Refer to the ISAT 200 System Installation Manual DOCO334 and DVI 300 Installation Manual DOC0456 for more information Most of the EMI tests can be accomplished on the ground In some cases flight testing is required or is easier If the aircraft is approved for IFR operations then it is mandatory that interference between the CDP 300 and the approach aids be checked in flight The existing on board GPS should be operational and navigating with at least the minimum compliment of satellites The VHF Communication
18. nces Additional information about the components of the ISAT 200 system can be found in the ISAT 200 Installation Manual DOC0334 and the CDP 300 User s Guide DOC0500 Document Rev 01 005 DOC0449 Page 6 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 1 3 System Components The CDP 300 is a peripheral of the ISAT 200 System The CDP 300 can operate stand alone or in conjunction with a DVI 300 CDP DVI mode The CDP DVI must be connected to an ISAT 200 with up to date firmware versions on all STS equipment Refer to the CDP 300 User s Guide DOCO0500 or www skytrac ca for the firmware revisions needed for the CDP 300 and ISAT 200 1 3 1 ISAT 200 The ISAT 200 is the primary component of the ISAT 200 System The ISAT 200 provides position reporting and messaging with global coverage in near real time The CDP 300 provides a user cockpit control head to the system Please refer to the ISAT 200 installation manual for more information regarding installation of the ISAT 200 ANTENNA AE DVI COP sg j ISAT 200 gt w AIRCRAFT ICS 40 o Figure 1 ISAT 200 System Block Diagram Document Rev 01 005 DOC0449 Page 7 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 1 3 2 CDP 300 The CDP 300 has a small easy to use form factor well suited to the demanding environment of working aircraft The CDP 300 consists of a DZUS rail mounted display 3 lines
19. not to touch the connector pins unless properly grounded Warning Changes or modifications not expressly approved by SkyTrac Systems Ltd STS could void the user s authority to operate the equipment Warranty Information SkyTrac Systems Ltd warrants this product to be free of defects in materials and workmanship and that the product meets or exceeds approved factory acceptance test requirements STS reserves the right to replace any warranted product at its sole discretion during the warranty period The CDP 300 is under warranty for one year from the date of shipment from SkyTrac Systems For failed units caused by defective parts or workmanship contact SkyTrac Systems for an RMA Once an RMA has been obtained the unit should be returned to SkyTrac Systems Ltd 200 170 Rutland Road North Kelowna B C Canada V1X 3B2 Proprietary Notice The information contained in this document is proprietary and confidential to SkyTrac Systems Ltd No part of this document may be reproduced or transmitted in any form or by any means electronic or mechancial without express written permission from SkyTrac Systems Ltd Document Rev 01 005 DOC0449 Page 2 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd Table Of Contents 1 GONG CT EE EE E 5 1 1 A O 5 1 2 Contents lot a laos 5 pF AIP rr ele ENEE e 6 A O gees 6 1 3 System COMPONENTS hikinen eiorinn aaaea ia aaae aaae aaa aE aE aa e a aA
20. nstallation This section contains the information needed to complete the electrical connections to the CDP 300 system Section 5 Configuration of the CDP 300 This section contains instructions on how to configure and set up the CDP 300 system Section 6 Post Installation Tests This section contains instructions for tests to be performed after installation to confirm that the system has been installed correctly Document Rev 01 005 DOC0449 Page 5 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd Section 7 Airworthiness Limitations This section describes the installation and operational limitations of the CDP 300 system Section 8 Maintenance and Continued Airworthiness This section describes the steps required for the continued airworthiness of the CDP 300 system Section 9 Firmware Updates This section indicates the methods available to update the CDP 300 and where to find the required instructions Section 10 CDP 300 Human Machine Interface This section provides a brief description of the CDP 300 human machine interface components 1 2 1 Audience This manual is intended for qualified aircraft avionics technicians referred to as installers The context of the manual assumes that the installer is familiar with the tools materials and techniques of wiring and metal work required for installing radios antennas and related components into aircraft 1 2 2 Refere
21. red to complete the electrical connections in a CDP 300 installation Included are diagrams and tables that call out and list the pin locations of the connectors used in the installation as well as system wiring diagrams with installation notes When installing the CDP 300 the installer shall have a working knowledge of aircraft electronics installation and be a holder of either an FAA Repairman s Certificate or a Transport Canada equivalent All installations should meet the requirements of FAA advisory circular AC43 13 1B IMPORTANT NOTICE All system interconnect cables must be connected before power is applied to the system 4 2 Line Functions This section describes the pin layout of the CDP 300 DB 15 and DB 9 connector 4 2 1 CDP 300 DB 15 Connector Pin out Table 7 CDP 300 DB 15 Connector Pin Descriptions Pin Pin Name Function Description 1 Ground CDP 300 Ground Pin 2 28V Connect to 28Vdc 3 RS 485 RS 485 positive 4 RS 485 RS 485 negative 5 Buzzer Ground sinking output used for buzzer activation 6 Reserved Reserved for future use Do not connect 7 Reserved Reserved for future use Do not connect 8 Ground CDP 300 Ground Pin 9 RS 232 RX RX line of RS 232 Databus to DVI 300 Do not connect if DVI 300 is not used 10 RS 232 TX TX line of RS 232 Databus to DVI 300 Do not connect if DVI 300 is not used 11 Dim Ctl In Dimmer voltage input 12 Reserved
22. stems to activate the satellite communications services 3 5 1 Product Mounting To operate as part of the CDP DVI the CDP 300 has to be mounted just above the DVI 300 If the CDP 300 is mounted already disconnect the connector for CDP 300 and remove the CDP 300 from the aircraft DZUS rails Place the CDP 300 over the DVI 300 and secure them together using CDP DVI Mounting Brackets on both sides Connect the wiring harness to the rear of the CDP 300 and DVI 300 Be sure to install all connector mounting hardware required Mount the CDP 300 and DVI 300 to the aircraft DZUS rails using the DZUS fasteners on them 3 6 Installation Materials 3 6 1 Installation Kit for the CDP 300 The CDP 300 is installed using the CDP 300 Installation Kit P N 106 300 01 The Installation Kit contains all the components necessary to install the CDP 300 Components from the ISAT 200 Installation Kit will also be required 3 6 2 Wiring Harness Determine the location of the CDP 300 in order to determine wiring harness lengths Create the wiring harness for your model of CDP 300 referencing applicable approved installation drawings for your airframe Ensure the wiring harness complies with the requirements of FAA advisory circular AC43 13 1B Document Rev 01 005 DOC0449 Page 14 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 4 ELECTRICAL INSTALLATION 4 1 General This section contains the information requi
23. t the parts list on the Installation Kit Package and verify that all components are included and were not damaged during shipping 2 Product Mounting Determine the approximate location of the CDP 300 3 Install and secure the CDP 300 4 Configure the CDP 300 5 Test the CDP 300 IMPORTANT NOTICE All system interconnect cables must be connected before power is applied to the system 3 4 CDP 300 Component Weights The following table provides the weight for the CDP 300 system Table 6 Component Weights Component Weight CDP 300 0 33kg 0 73 lbs Document Rev 01 005 DOC0449 Page 13 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 3 5 Unpacking and Inspecting the System Components 1 Check the items in the shipment against those listed on the shipping invoice to ensure that all items have been received If any items are missing contact SkyTrac Client Services 2 Carefully remove each item from its individual packaging 3 Inspect each item for damage that may have been incurred during shipping In case it is necessary to submit a damage claim save the shipping container to help verify the claim 4 After all items have been unpacked it is suggested that you save the containers and packaging materials in case it becomes necessary to reship an item 5 Verify and record the serial number of the CDP 300 This information is required when contacting SkyTrac Sy
24. ust be connected before power is applied to the system Document Rev 01 005 DOC0449 Page 16 of 23 Restricted Proprietary and Confidential Information SkyTrac Systems Ltd 5 CONFIGURATION OF THE CDP 300 The main configuration required during installation is the brightness control configuration described below Additional configuration of the address book quick dial numbers etc may be done by the user via the instructions contained in the CDP 300 User s Guide 5 1 CDP 300 Brightness Configuration When used in the CDP DVI mode the CDP 300 brightness is slaved to the DVI 300 brightness control The DVI 300 brightness is controlled via the aircraft dimmer bus This mode is the default mode Refer to the DVI 300 Installation Manual DOC0456 for details on wiring the DVI 300 for dimmer bus brightness control Optionally the brightness of the CDP DVI can be controlled manually via the keypad or automatically via an optical sensor which detects ambient light levels and sets the brightness appropriately No wiring is required to use the manual or optical sensor brightness control modes The user can choose one of the modes at any time via the menu interface Refer to the CDP 300 User s Guide DOC0500 for details about changing the mode of brightness control via the CDP 300 menu system In standalone mode the CDP 300 can use the optical sensor or the dimmer bus may be wired to the CDP 300 and used to control brightness
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