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Skytrac ISAT-100, Инструкция по эксплуатации и руководство по установке

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SkyTrac Systems Ltd. 

 

Document Rev. 02.010 

ISAT-100-OPD-SOI 

ii  

Restricted Proprietary and Confidential Information 

 

 
 

 

Document Revision History 

Rev 

ECO

 

Page 

Description 

Date 

Approval 

01.20

 

- 

 

Initial Release 

July 2003 

KWallace 

01.30

 

012 

S 4.6 

Amendment to Install Notes:

  

Added upright mounting 
requirement and vent hole 
requirements. 

Sept 18, 2003 

KWallace 

 

- 

S 4.6 

Amendment to Install Notes:

  

Added paragraph on potential 
Hydrogen release rate, suggested 
install space and ventilation 
requirements. 

Oct 14, 2003 

KWallace 

 

- 

S 2.7 

Amendment to Environmental 

Test Summary:  Section 9 and 22 

 

Comments:  Note 1. 

Oct 16, 2003 

KWallace 

 

- 

S 2.8 

Amendment to Continued 

Airworthiness:  Periodic 
inspection notes 

Oct 16, 2003 

KWallace 

 

- 

S 4.5 

Amendment to Overview:

  Added 

point 9 regarding PDA usage. 

Nov 7, 2003 

KWallace 

 

- 

S 2.1 

Amendment to Operating 
Temperature 

Nov 18, 2003 

KWallace 

 

- 

S 4.8.2 

Amendment to EMI Test

 to be 

consistent with EMI/RFI Test for 
ISAT-100 (Doc # 238-50064-00) 

Nov 18, 2003 

KWallace 

 

- 

S 1.2 

Amendment to DO-160D:

  

Corrected DO-160D Category 

Nov 18, 2003 

KWallace 

 

- 

S 2.1 

Amendment to Operating 
Temperature 

Nov 20, 2003 

KWallace 

 

- 

S 2.7 

DO-160D:  

Section 4.5 Add 

Category A4 

Nov 20, 2003 

KWallace 

 

- 

S 4, A-B 
Pg 26 

Revised second line to read 
“Equipment near active 
INMARSAT terminals” 

Mar 3, 2004 

KWallace 

The document reference is online, please check the correspondence between the online documentation and the printed version.

Содержание ISAT-100

Страница 1: ...02 010 April 9 2013 SkyTrac Systems Ltd 200 170 Rutland Road N Kelowna BC Canada V1X 3B2 Tel 250 765 2393 Fax 250 765 3767 Web www skytrac ca Email techsupport skytrac ca Copyright 2013 SkyTrac Syste...

Страница 2: ...2003 KWallace S 2 8 Amendment to Continued Airworthiness Periodic inspection notes Oct 16 2003 KWallace S 4 5 Amendment to Overview Added point 9 regarding PDA usage Nov 7 2003 KWallace S 2 1 Amendmen...

Страница 3: ...lace S 4 6 1 Fig 4 3 Updated Connector Diagram according to Table 4 1 Dec 16 2004 KWallace S 4 8 Fig 4 5 Updated Connector Pinout Jan 5 2005 KWallace S 4 6 Fig 4 2 S 4 6 1 Fig 4 4 Table 4 2 Updated 10...

Страница 4: ...28 2008 T Ratch 02 004 0165 Pg1 pg 4 pg7 Updated applies to Statement Pg 4 Add section ISAT 100 Installation Kit pg 7 delete section Installation Kit and the list of material for the kit Feb 24 2009...

Страница 5: ...nted product at its sole discretion during the warranty period The Model ISAT 100 Airborne Data Position Communicator is under warranty for one year from date of shipment from SkyTrac Systems Ltd For...

Страница 6: ...LIMITATIONS 6 4 INSTALLATION INSTRUCTIONS 7 4 1 INSTALLATION REQUIREMENTS 7 4 2 UNPACKING AND INSPECTING 7 4 2 1 Identifying Your ISAT 7 4 2 2 Equipment Packing Log 7 4 3 OVERVIEW 7 4 4 ISAT 100 INSTA...

Страница 7: ...INESS 23 6 1 CONTINUED AIRWORTHINESS 23 6 2 MAINTENANCE INSTRUCTIONS 23 7 APPENDIX A 24 7 1 ISAT 100 FRONT PANEL DIAGRAM 24 7 2 ISAT 100 REAR PANEL DIAGRAM 25 8 APPENDIX B 26 8 1 CAUSES OF RF INTERFER...

Страница 8: ...Env Cat A4 D1 XAB SMB UF XXXXXXZBBXXXMXXXX Appendix A illustrates the Front and Rear Panel layout of the ISAT 100 1 3 Purpose of Equipment The ISAT 100 is the primary hardware component of a system d...

Страница 9: ...o required installation of the following components This installation may require 1 or more reboots Microsoft Jet Engine NET 2 0 ODBC Drivers UltiCassini WebService for FlightMap World FlightTrac Suit...

Страница 10: ...ver Receiving Method 12 Channel Parallel Receiver Acquisition time 48 seconds after power up cold start 0 1 seconds for re acquisition Position accuracy Less than 25 m without Differential GPS 1 5m wi...

Страница 11: ...Stations and Systems SES Harmonized EN for EN 301 441 2 4 Audio Interface The Audio Output can provide 100 mW into 600 or 300 ohm nominal The Audio Output is short circuit protected Nominal microphon...

Страница 12: ...0 0 Waterproofness X No test required 11 0 Fluid Susceptibility X No test required 12 0 Sand and Dust X No test required 13 0 Fungus Resistance X No test required 14 0 Salt Spray X No test required 15...

Страница 13: ...installed in a location that provided adequate ventilation space as specified in section 4 4 Installation of the ISAT 100 for operation above 16 000 ft is only approved for an upright orientation If...

Страница 14: ...that each item listed on the packing slip has been shipped in the container Verify and record the IMEI Number of the ISAT 100 This information is required when contacting SkyTrac Systems to activate...

Страница 15: ...ctor RS 232 cable should not exceed 40 ft 1 Must use shielded RS 232 cable 4 4 ISAT 100 Installation The ISAT 100 is designed to be secured by its mounting rails to the airframe using six 6 AN 3 bolts...

Страница 16: ...t position or a sideways position and none of the venting holes in the top cover or in either side panel should be covered at any time The ISAT 100 may not be mounted inverted See Installation Limitat...

Страница 17: ...be grounded in order to enable the internal battery Use AWG 20 wire to hook up the 28VDC aircraft main power source protected through a 3 Amp breaker to the ISAT 100 It is important to remember that t...

Страница 18: ...ISAT 100 OPD SOI Page 11 of 26 Restricted Proprietary and Confidential Information FIGURE 4 3 System Connector Diagram The document reference is online please check the correspondence between the onli...

Страница 19: ...h K Voltage Seeking Digital Input 2 L Ground Seeking Digital Input 3 M Voltage Seeking Digital Input 4 N Ground Seeking Digital Input 5 Squat Collective P Voltage Seeking Digital Input 6 Engine On Off...

Страница 20: ...etween 0 and 30 volts when applied to pin E will be converted to a digital value with 12 bits of resolution Pin F Analog Input 3 An analog voltage level between 0 and 30 volts when applied to pin F wi...

Страница 21: ...king Emergency Grounding pin R will produce a digital logic high The default configuration uses pin R to monitor an emergency or panic switch Pin S Digital Output 1 Current Sinking The default use for...

Страница 22: ...RXC Data Connector J2 Pinout Designation GROUND A K B J C H D G E F Table 4 2 Data Connector Pin Description 10 Pin Data Connector Pin Description A Ground Signal B RS 232 Channel 1 Transmit C RS 232...

Страница 23: ...ss coax cable like ECS 310801 311601 311501 311201 and refer to manufacturers specs for attenuation at 1 6 GHz Attenuation of equal or less than 3dB is required The bond between the airframe and the a...

Страница 24: ...sue a PC executable file that will perform any upgrade A standard serial DB9 computer cable RS 232 will be required to connect a laptop or PC to the ISAT 100 Although a serial to serial connection is...

Страница 25: ...ure the AUDIO LEVEL follow the below procedure 1 Adjust ISAT 100 to minimum AUDIO LEVEL 2 Establish a phone call 3 Slowly increase the AUDIO LEVEL until desired volume is heard If audio signal quality...

Страница 26: ...receiving end If audio signal quality begins to degrade while increasing gain decrease gain until signal quality is good 4 8 Post Installation Tests 4 8 1 Initial Verification Test The avionics instal...

Страница 27: ...ing pattern of two quick blinks on solid Optional If the audio system is connected a tone should be heard when the ISAT starts up c Test connected audio system and peripheral devices place a phone cal...

Страница 28: ...degradation in satellite status availability or flags Listen for any noise or detected audio signals on the VHF Comm s Listen for any noise or detected audio signals on the VOR LOC receiver audio loo...

Страница 29: ...ISAT is working properly and the ISAT has strong Iridium satellite link and GPS lock The position reporting function of the ISAT 100 is transparent to the aircraft crew The position reporting interval...

Страница 30: ...vely flying aircraft If the ISAT 100 is not installed in an actively flying aircraft for a period of time that is greater than 3 months apply 28 Volts to System connector for six 6 hours to maintain b...

Страница 31: ...100 OPD SOI Page 24 of 26 Restricted Proprietary and Confidential Information 6 APPENDIX A 6 1 ISAT 100 Front Panel Diagram The document reference is online please check the correspondence between the...

Страница 32: ...PD SOI Page 25 of 26 Restricted Proprietary and Confidential Information 6 2 ISAT 100 Rear Panel Diagram REAR Dimensions inch mm The document reference is online please check the correspondence betwee...

Страница 33: ...SkyTrac Systems Generally speaking an Iridium unit located within 15 to 45 meters 50 to 150 feet respectively of an operating INMARSAT mini M or Standard C terminal will likely experience interruptio...

Страница 34: ...The document reference is online please check the correspondence between the online documentation and the printed version...

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