Skytrac ISAT-100 Скачать руководство пользователя страница 4

SkyTrac Systems Ltd. 

 

Document Rev. 02.010 

ISAT-100-OPD-SOI 

iv  

Restricted Proprietary and Confidential Information 

 

 

Document Revision History Continued 

Rev 

ECO

 

Page 

Description 

Date 

Approval 

01.47 

027 

All 

Updated SOI format implemented 
Additional details on Maintenance 
and Continued Airworthiness, and 
Airworthiness Limitations were 
added. 

May 30, 2005  K.Wallace

 

01.48 

051 

Pg 10, 24, 
25 

Added Audio Interface Section 

Dec 15, 2005  T. Ratch 

01.49 

Pg 7, Pg 
11. 

DO-160D Test Qualification 
Clarified. D0-160D Sec 21 
corrected to Cat M. 

Jan 20, 2006 

T. Ratch 

02.00 

Pg 1 

Revision number changed to 02.00 

Jan 26, 2006 

T. Ratch 

02.001

 

052, 

088 

 

Updated Address.  Updated rev to 
xx.(y)yy format. 

Aug 18, 2006  T. Ratch 

02.002

 

124 

8, 19 

Added instructions how to do 
functional test without PDA . 
Corrected spelling any typos. 

July 17, 2007  T. Ratch 

02.003

 

0145

 

 

Add reference to Installation 
Drawing 

July 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 

T. Ratch 

02.005

 

170 

Add reference to  ISAT-100 
Installation Kit Bill of Materials 
(DOC0159)  

May 01, 2009  T. Ratch 

02.006

 

195 

2, 3, 6, 9, 
12, 14, 15, 
17, 19, 20, 
22, 23 

Made updates as specified in 
NCR090414-001 

Sep 15, 2009  T. Ratch 

02.007

 

305 

6,9 

Added sideways mounting 
orientation 

April 26, 2010

 

T.Ratch 

02.008

 

386 

13, 16, 18, 
19, 20, 22 

Added STS0021 as the new part 
number for STS-ISAT-ANT. 
Changed “18 – 30VDC” to “22 – 
30VDC” in section 4.4. Removed 
reference to ITRAX Palm Software. 
Replaced activation instructions 
with SkyWeb activation instructions. 
Added description of what blinking 
LED patterns mean. Corrected 
spelling of syncro in section 4.7.1. 

Dec 20, 2010  T. Ratch 

2.009 

392 

Updated airworthiness limitations 
for sideways installation 

Jan 24, 2011 

T. Ratch 

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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