Difference between revisions of "TCAS Version 7.1"
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|rowspan="2" style="text-align:center;"|[[TCAS II|TCAS II]] | |rowspan="2" style="text-align:center;"|[[TCAS II|TCAS II]] | ||
| − | | | + | |style="background-color:#FCE883; color:black;text-align:center;"|RT-910 |
| − | |style="background-color:# | + | |style="background-color:#FCE883; color:black;text-align:center;"|4066010-904 |
| − | |style="background-color:# | + | |style="background-color:#ACE1AF; color:black; text-align:center;"|RT-910 |
| − | |style="background-color:# | + | |style="background-color:#ACE1AF; color:black; text-align:center;"|Note [1] |
| − | |style="text-align:left;"| | + | |style="text-align:left;"|Embraer ERJ-145 EP/EU/LR |
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| + | |style="background-color:#FFFF66; color:black; text-align:center;"|RT-910 | ||
|style="background-color:#FFFF66; color:black;text-align:center;"|4066010-910 | |style="background-color:#FFFF66; color:black;text-align:center;"|4066010-910 | ||
|style="background-color:#98FB98; color:black; text-align:center;"|RT-910 | |style="background-color:#98FB98; color:black; text-align:center;"|RT-910 | ||
|style="background-color:#98FB98; color:black; text-align:center;"|4066010-914 | |style="background-color:#98FB98; color:black; text-align:center;"|4066010-914 | ||
| − | |style="text-align:left;"|Boeing 737-500 | + | |style="text-align:left;"|Boeing 737-500 |
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|rowspan="3" style="background-color:white; vertical-align:center; text-align:center;"|[[File:Honeywell_logo.png|link=]] | |rowspan="3" style="background-color:white; vertical-align:center; text-align:center;"|[[File:Honeywell_logo.png|link=]] | ||
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|style="background-color:#FCE883; text-align:center;"|066-50000-2XXX | |style="background-color:#FCE883; text-align:center;"|066-50000-2XXX | ||
|style="background-color:#ACE1AF; text-align:center;"|TPA-100B | |style="background-color:#ACE1AF; text-align:center;"|TPA-100B | ||
| − | |style="background-color:#ACE1AF; text-align:center;"|Note [ | + | |style="background-color:#ACE1AF; text-align:center;"|Note [2] |
|style="text-align:left;"|Airbus A319-115, A320-2XX, A321-2X1, A330-223, SAAB 340 | |style="text-align:left;"|Airbus A319-115, A320-2XX, A321-2X1, A330-223, SAAB 340 | ||
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|style="background-color:#FCE883; text-align:center;"|622-8971-022 | |style="background-color:#FCE883; text-align:center;"|622-8971-022 | ||
|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 [ | + | |style="background-color:#ACE1AF; text-align:center;"|Note [3] |
|style="text-align:left;"|DC-9-83 (MD-83) | |style="text-align:left;"|DC-9-83 (MD-83) | ||
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{| style="border-collapse:collapse; border: 1px solid dark; text-align:justify;font-size:0.9em;" cellpadding="3" border="0" | {| style="border-collapse:collapse; border: 1px solid dark; text-align:justify;font-size:0.9em;" cellpadding="3" border="0" | ||
|Notes: | |Notes: | ||
| + | # | ||
#Aircraft equipped with CAS-81A systems require replacement of TPA-81A by TPA-100B processor. | #Aircraft equipped with CAS-81A systems require replacement of TPA-81A by TPA-100B processor. | ||
#The TTR-920 is not upgradable to Change 7.1. Aircraft equipped with TTR-920 processor require replacement of TTR-920 by TTR-921 or TTR-2100 processor, minor wiring changes and new connector kit should be installed. We can provide necessary tools and equipment, test set for TCAS check, materials and staff. The customer issues Engineering Order and final CRS (maintenance level is line). | #The TTR-920 is not upgradable to Change 7.1. Aircraft equipped with TTR-920 processor require replacement of TTR-920 by TTR-921 or TTR-2100 processor, minor wiring changes and new connector kit should be installed. We can provide necessary tools and equipment, test set for TCAS check, materials and staff. The customer issues Engineering Order and final CRS (maintenance level is line). | ||
Revision as of 15:10, 16 June 2015
| 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. |
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| DOCUMENTS (STC) | |
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