Difference between revisions of "TCAS Version 7.1"
From Aeroscan Service
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|style="background-color:#98FB98; color:black; text-align:center;"|RT-950 | |style="background-color:#98FB98; color:black; text-align:center;"|RT-950 | ||
|style="background-color:#98FB98; color:black; text-align:center;"|7517900-10020 | |style="background-color:#98FB98; color:black; text-align:center;"|7517900-10020 | ||
| − | |style="text-align:left;"|Ан-12, Ан-74, Ан-124, Dornier 328-300, Embraer | + | |style="text-align:left;"|Ан-12, Ан-74, Ан-124, Dornier 328-300, Embraer 145/190 |
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|style="background-color:#FFFF66; color:black; text-align:center;"|RT-951 | |style="background-color:#FFFF66; color:black; text-align:center;"|RT-951 | ||
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|style="background-color:#ACE1AF; color:black; text-align:center;"|RT-910 | |style="background-color:#ACE1AF; color:black; text-align:center;"|RT-910 | ||
|style="background-color:#ACE1AF; color:black; text-align:center;"|Note [1] | |style="background-color:#ACE1AF; color:black; text-align:center;"|Note [1] | ||
| − | |style="text-align:left;"|Embraer | + | |style="text-align:left;"|Embraer 145/190 |
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|style="background-color:#FFFF66; color:black; text-align:center;"|RT-910 | |style="background-color:#FFFF66; color:black; text-align:center;"|RT-910 | ||
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|style="background-color:#98FB98; color:black; text-align:center; width:60px"|TPU-67B | |style="background-color:#98FB98; color:black; text-align:center; width:60px"|TPU-67B | ||
|style="background-color:#98FB98; color:black; text-align:center; width:90px"|066-01146-2X21 | |style="background-color:#98FB98; color:black; text-align:center; width:90px"|066-01146-2X21 | ||
| − | |style="text-align:center; text-align:left;"|Ан-12, Ан-24, Ан-26, Ил-76ТД, Як-40, Л-410, Ми-8МТВ-1, Cessna | + | |style="text-align:center; text-align:left;"|Ан-12, Ан-24, Ан-26, Ил-76ТД, Як-40, Л-410, Ми-8МТВ-1, Cessna 560XL/680 |
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|style="text-align:center;"|[[CAS-81A]] | |style="text-align:center;"|[[CAS-81A]] | ||
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|style="background-color:#98FB98; color:black; text-align:center;"|TPA-100B | |style="background-color:#98FB98; color:black; text-align:center;"|TPA-100B | ||
|style="background-color:#98FB98; color:black; text-align:center;"|940-0351-001,-010<br>940-0451-001 | |style="background-color:#98FB98; color:black; text-align:center;"|940-0351-001,-010<br>940-0451-001 | ||
| − | |style="text-align:left;"|An-32RE, Airbus A320, Boeing 737 | + | |style="text-align:left;"|An-32RE, Airbus A320, Boeing 737, DC-9-80 (MD-80) |
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|rowspan="3" style="background-color:white; vertical-align:center; text-align:center;"|[[File:RockwellCollins_logo.png|link=]] | |rowspan="3" style="background-color:white; vertical-align:center; text-align:center;"|[[File:RockwellCollins_logo.png|link=]] | ||
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|style="background-color:#ACE1AF; text-align:center;"|TTR-921<br>TTR-2100 | |style="background-color:#ACE1AF; text-align:center;"|TTR-921<br>TTR-2100 | ||
|style="background-color:#ACE1AF; text-align:center;"|Note [2] | |style="background-color:#ACE1AF; text-align:center;"|Note [2] | ||
| − | |style="text-align:left;"|DC-9- | + | |style="text-align:left;"|DC-9-80 (MD-80), Boeing 737 |
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|style="background-color:#FFFF66; color:black; text-align:center;"|TTR-921 | |style="background-color:#FFFF66; color:black; text-align:center;"|TTR-921 | ||
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|style="background-color:#98FB98; color:black; text-align:center;"|TTR-921 | |style="background-color:#98FB98; color:black; text-align:center;"|TTR-921 | ||
|style="background-color:#98FB98; color:black; text-align:center;"|822-1293-033 | |style="background-color:#98FB98; color:black; text-align:center;"|822-1293-033 | ||
| − | |style="text-align:left;"|Ан-12, Ан-24, Ан-26, Ан-140, Ан-32, Airbus A320 | + | |style="text-align:left;"|Ан-12, Ан-24, Ан-26, Ан-140, Ан-32, Airbus A320, Boeing 737/767, Bombardier CL-600, DC-9-80 (MD-80), Learjet 60, Dassault Falcon 20/50, SAAB 340 |
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|style="text-align:center;"|[[TCAS-4000]] | |style="text-align:center;"|[[TCAS-4000]] | ||
Revision as of 16:41, 12 June 2018
| EN | UK | RU |
| New TCAS logic would definitely bring significant safety benefits... − such conclusion was made by ICAO investigations that has issued the new requirements for forward fit (from 1 January 2014) and retrofit (by 1 January 2017) of aircraft ACAS installations with an upgraded collision avoidance logic known as TCAS Version 7.1 (Amendment 85 to Annex 10, Volume IV). Similar deadlines were set by the State Aviation Administration of Ukraine in the Operational Directive No. ED-02-15. The European Commission has published Regulation No. 1332/2011 mandating the carriage of ACAS II version 7.1 within European Union airspace from 1 December 2015 by all civil aircraft. |
All information needed for pilots training regarding TCAS version 7.1 is listed below. We provide complex services to our clients to upgrade TCAS to version 7.1:
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Send your inquiry by fax, e-mail or using form on page Quick Inquiry. |
| TCAS SYSTEMS SUMMARY TABLE | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
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| DOCUMENTS (STC) | |
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