04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10038558 BRISTOW HELICOPTERS Ltd. REV. 1 S-76C Modification of Rockwell Collins TCAS-4000 Applicable only to the S76C with Turbomeca Prior to installation of this modification it 17.07.2<strong>01</strong>2<br />
TCAS II update to version 7.1software. Arriel 2S2 engines.<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong>0678 BRISTOW HELICOPTERS Ltd. S-61N Activation of ADS-B Function using Mode S<br />
Extended Squitter<br />
10035883 BRISTOW U.S. L.L.C. FAA STC SR09577RC S-76A, S-76C Installation of an Automatic Deployable<br />
Emergency Transmitter (ADELT)<br />
10<strong>01</strong>4176 BRITISH AIRWAYS PLC <strong>EASA</strong>.A.S.<strong>01</strong>312 BOEING 747-400 Omnibus Modification for B747 Mid J Project<br />
Stretch Embodiment<br />
10<strong>01</strong>4177 BRITISH AIRWAYS PLC <strong>EASA</strong>.A.S.<strong>01</strong>314 BOEING 747-400 Omnibus Modification for Boeing 747-436 Hi J<br />
Project Stretch Embodiment<br />
10<strong>01</strong>4178 BRITISH AIRWAYS PLC <strong>EASA</strong>.A.S.<strong>01</strong>315 BOEING 777-200 Omnibus Modification for B777 4 Class Project Prior to installation of this modification the<br />
Stretch Embodiment.<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
18.07.2<strong>01</strong>2<br />
none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
25.07.2<strong>01</strong>1<br />
10<strong>01</strong>4376 BRITISH AIRWAYS PLC <strong>EASA</strong>.A.S.<strong>01</strong>651 BOEING 737-400 Installation of Enhanced Mode S None 25.11.2005<br />
10<strong>01</strong>5033 BRITISH AIRWAYS PLC <strong>EASA</strong>.A.S.03345 BOEING 757-200 Reconfiguration of Passenger Cabin 13.06.2008<br />
10<strong>01</strong>5055 BRITISH AIRWAYS PLC <strong>EASA</strong>.A.S.03376 BOEING 757-200 B757 GPS upgrade to EGPWS. BA B757 AFM Change Sheet No. 10, <strong>Page</strong> 1<br />
and 3 (issue 2).<br />
28.03.2008<br />
10028294 BRITISH AIRWAYS PLC <strong>EASA</strong>.A.S.<strong>01</strong>313 BOEING 777-236 07.05.2009<br />
10030714 BRITISH AIRWAYS PLC B737-400 Fuselage skin GPS antenna structural<br />
provisions<br />
None None 02.07.2<strong>01</strong>0<br />
10031240 BRITISH AIRWAYS PLC B737-400 B737 GPS UPGRADE OF EGPWS None As a prerequisite to this modification the<br />
antenna installation inaccordance with BA<br />
Service Bulletin BA-757-53-00<strong>01</strong> under<br />
<strong>EASA</strong> approval10030714 must be<br />
performed. Successful completion of the<br />
of the test i.a.w. ESA-5<strong>01</strong>-DS-4<strong>01</strong>8<br />
isrequired upon the first in<br />
05.08.2<strong>01</strong>0<br />
10039421 BRITISH AIRWAYS PLC A318/A319/A320/A321 Airbus TCAS change 7.1 update. None. Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
03.05.2<strong>01</strong>2<br />
10<strong>04</strong>0257 BRITISH AIRWAYS PLC 777-200 B777 TCAS Change 7.1 update none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
21.06.2<strong>01</strong>2<br />
10<strong>04</strong>0970 BRITISH AIRWAYS PLC B737-400 B737 TCAS Change 7.1 Update. None. Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
09.08.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 144/<strong>462</strong><br />
28.02.2007<br />
17.11.2006<br />
09.09.2008
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