04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10<strong>01</strong>43<strong>01</strong> AEROTEC CONCEPT <strong>EASA</strong>.A.S.<strong>01</strong>545 BEECH C90 Installation of radio communication<br />
1. This STC is limited to Beechcraft C90 SN LJ<br />
12.09.2005<br />
systemsModel: Beechcraft C90 SN LJ 710 710.2. This STC is approved only for the<br />
product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph "Description". Compatibility with<br />
other aircraft configurations shall be deter<br />
10<strong>01</strong>4391 AEROTEC CONCEPT <strong>EASA</strong>.A.S.<strong>01</strong>677 MOONEY M20E BRNAV capacity with AP Steering Modification limited to s/n 28R7931294The<br />
AFMS BRNAV Garmin 430 must be used with<br />
this modification<br />
<strong>04</strong>.05.2006<br />
10<strong>01</strong>4756 AEROTEC CONCEPT <strong>EASA</strong>.A.S.02944 CESSNA 208<br />
CESSNA 208A<br />
CESSNA 208B<br />
Video Mast Installation under Cessna 208. 28.08.2007<br />
10<strong>01</strong>4794 AEROTEC CONCEPT <strong>EASA</strong>.A.S.02996 PIPER PA-31T Installation ATC mode S. 1. This STC is limited to the S/N: 7720036<br />
and 8020037.2. Prior to installation of this<br />
modification the installer must determine that<br />
the interrelationship between this modification<br />
and any other previously installed modification<br />
will introduce no a<br />
10.09.2007<br />
10<strong>01</strong>4799 AEROTEC CONCEPT <strong>EASA</strong>.A.S.03002 PIPER PA-31T Modification radio installation. 1. This STC is limited to the S/N 7720036.2.<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect<br />
10<strong>01</strong>4985 AEROTEC CONCEPT <strong>EASA</strong>.A.S.03277 BRITTEN NORMAN BN-2T<br />
ISLANDER<br />
10<strong>01</strong>5093 AEROTEC CONCEPT <strong>EASA</strong>.A.S.03430 REV. 1 C-212-DD Navigation / Communication (NAV/COM) set<br />
replacement and HFCommunication set<br />
(provisions) installationThis STC replaces a<br />
previous NAV/COM system by an up-to-date<br />
one, andinstalls a new HF communication set<br />
(provision).This revision restores the aircraft I<br />
Survey Capacity on BN-2T Supplemental Airplane Flight Manual, revision<br />
00, dated 17 January 2008, or later approved<br />
revision must be on board when modification is<br />
installed.Instruction for Continued<br />
Airworthiness, revision 00, dated 26 January<br />
2008 and Supplemental Airplane Mainte<br />
1. This STC is limited to the MSN 3872. HF<br />
communication set (subpart of this STC) is not<br />
approved (notinstalled / not operational – wiring<br />
provisions are accepted)<br />
10.09.2007<br />
08.<strong>04</strong>.2008<br />
Prior to installation of this modification it <strong>01</strong>.06.2<strong>01</strong>1<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>01</strong>7145 AEROTEC CONCEPT <strong>EASA</strong>.R.S.<strong>01</strong>248 EUROCOPTER FRANCE EC 120 Modification des sources d’attitude, d’écart de Limited to aircraft EC120B s/n1327, F-GJIR<br />
19.<strong>01</strong>.2007<br />
B<br />
cap et GPS du système pilote automatique only, when equipped with <strong>EASA</strong>.IM.R.S.1056<br />
PA85 SAGEM(change of sensors sources for Rev.1 and <strong>EASA</strong>.R.C.<strong>01</strong>912 and<br />
attitudes retention, heading error select and<br />
GPS steerings of Sagem PA85 Automatic Pilot<br />
system)<br />
<strong>EASA</strong>.R.C.<strong>01</strong>913 changes<br />
10<strong>01</strong>7169 AEROTEC CONCEPT <strong>EASA</strong>.R.S.<strong>01</strong>277 EUROCOPTER FRANCE EC 120 Improvement of "VG Fail" alarm for<br />
Limited to aircraft EC120B S/N 1<strong>04</strong>9, G-VIPR<br />
<strong>04</strong>.08.2006<br />
B<br />
<strong>EASA</strong>.R.S.<strong>01</strong><strong>01</strong>7 and <strong>EASA</strong>.IM.R.S.<strong>01</strong>056 only, when equipped with <strong>EASA</strong>.R.S.<strong>01</strong><strong>01</strong>7<br />
installations<br />
and <strong>EASA</strong>.IM.R.S.<strong>01</strong>056<br />
10<strong>01</strong>7193 AEROTEC CONCEPT <strong>EASA</strong>.R.S.<strong>01</strong>330 EUROCOPTER FRANCE SA AEROTEC avionics modification n° 6306: This STC is limited to SA 365 N s/n 6218 and<br />
12.02.2007<br />
365N<br />
installation of:two NAV/COM/GPS GARMIN can be installed only by AERTOTEC technical<br />
GNS 430 for IFR B-RNAV "En route" staff in accordance with AEROTEC STC<br />
operations, with their associated GARMIN GA Implementation File n°6306, revision 1 dated<br />
56 GPS antenna,two MID CONTINENT MD 41 26/10/06, or later revision.AEROTEC minor<br />
Annunciation Control Units,an ALLIED SIGNAL modification n°6206, approved under <strong>EASA</strong>.R.<br />
KA 33 cooling blo<br />
10034668 AEROTEC CONCEPT C-212-DD ( C212-300) Mod 0921: EGPWS Installation This STC is limited to the MSN 387 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 />
19.<strong>04</strong>.2<strong>01</strong>1<br />
10034675 AEROTEC CONCEPT C90A Installation d'une antenne SATCOM iridium -<br />
dossier aerotec 1082rev1<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 />
19.<strong>04</strong>.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 41/<strong>462</strong>
Change language