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 />
10038324 AIRBORNE TECHNOLOGIES GmbH P2006T Hatch Cover. STC-AT-003 must be installed prior this The approval holder shall fulfill the 07.02.2<strong>01</strong>2<br />
modification.<br />
obligations of Part 21,<br />
Paragraph21.A109.Prior to installation of<br />
this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repai<br />
10039513 AIRBORNE TECHNOLOGIES GmbH P2006T Police cabin configuration/Installation of a Airborne Technologies STC no. "STC-AT-003", Prior to installation of this modification it 08.05.2<strong>01</strong>2<br />
camera lift for 10" gimbals, operator console step 1 (analogueinstruments) or step 3 (Garmin must be determined thatthe<br />
andreplacement of hatch doors by fixed G950 version) of latest approved revisionmust interrelationship between this modification<br />
coversFor standard analogue instruments be installed prior this modification.<br />
and any other previouslyinstalled<br />
equipped aircraft step 1 of this STCis<br />
modification and/ or repair will introduce<br />
applicable, for Garmin G950 equipped aircraft<br />
no adverse effectupon the airworthiness<br />
s<br />
of the product.<br />
10<strong>04</strong><strong>01</strong>98 AIRBORNE TECHNOLOGIES GmbH P2006T Title: Provisions for radar operationDescription: STC-AT-003 step 1 or step 3 and EO-AT-<strong>04</strong>7<br />
Installation of a radome below the<br />
photogrammetric hatch,activation of the rear<br />
hatch (installed with EO-AT-<strong>04</strong>7), installation<br />
ofa ventral fin, upgraded mission power supply<br />
system and removal of hatchdoors<br />
must be installed prior thismodification.<br />
Prior to installation of this modification it 18.06.2<strong>01</strong>2<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>0955 AIRBORNE TECHNOLOGIES GmbH P.68 C, P.68 C-TC Title: Mission cabin configuration P.68 C / Vulcanair SB-163 must be carried out prior this Prior to installation of this modification it 07.08.2<strong>01</strong>2<br />
Description: This STC consists of 3 steps: Step STC.<br />
must be determined thatthe<br />
1: To install different mission equipment in a<br />
interrelationship between this modification<br />
Vulcanair P.68aircraft, step 1 modifies the<br />
and any other previouslyinstalled<br />
aircraft cabin and installs provisions<br />
modification and/ or repair will introduce<br />
toaccommodate Mission Equipment. S<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong>2009 AIRBORNE TECHNOLOGIES GmbH EC135 P2+ Title: Provisions for surveillance operations<br />
Description: Installation of provisions for<br />
surveillance operations,consisting of the<br />
following parts:Step 1 : Provisions for<br />
surveillance operationsStep 2 : Cabin<br />
provisionsStep 3 : Trim mass installation<br />
10<strong>01</strong>3925 AIRBUS S.A.S. <strong>EASA</strong>.A.S.0<strong>01</strong>96 REV. 1 AIRBUS A319-112 Cabin reconfiguration into an executive 44 pax, The Document Ref.: DIT/N/20<strong>04</strong>/1726/OS<br />
in accordance with the Modification Approval Revision B must be incorporated as a<br />
Sheet (MAS) Ref. SOG-00-830, issue 4, dated supplement to the Airplane Flight Manual<br />
September 20, 20<strong>04</strong><br />
(AFM)<br />
10<strong>01</strong>3936 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00347 REV. 1 AIRBUS A330-203 VIP Cabin Installation 1. The approval of this modification is limited<br />
to the Airbus A330-203 MSN 487 which is<br />
used as a private aircraft. The limitations and<br />
conditions defined in the <strong>EASA</strong> Datasheet are<br />
applicable. A copy of this STC and of the MDL,<br />
AFM must be enclosed in t<br />
10<strong>01</strong>3937 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00348 REV. 1 AIRBUS A330-203 Installation of a SATCOM Live TV system. 1. The approval of this modification is limited<br />
to the AIRBUS A330-203 MSN 487. The<br />
limitations and conditions defined in the <strong>EASA</strong><br />
Datasheet are applicable. A copy of this STC<br />
and of the MDL, AFM must be enclosed in the<br />
file of the modified aircraft. An<br />
10<strong>01</strong>3945 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00387 REV. 5 LBA STC TA<strong>04</strong>41 ISSUE 4 A300B4-6<strong>01</strong>, -603, -605R<br />
A300B4-620, -622, -622R<br />
<strong>EASA</strong> STC <strong>EASA</strong>.A.S.00387 revision 4 (ref. to<br />
former Luftfahrt BundesamtSTC TA<strong>04</strong>41 Issue<br />
4) The STC <strong>EASA</strong>.A.S.00387 has covered the<br />
transfer of the STC TA<strong>04</strong>41 Issue4 (original<br />
Aviation Authority reference) from the original<br />
AviationAuthority (LBA) to the <strong>EASA</strong><br />
10<strong>01</strong>3946 AIRBUS S.A.S. <strong>EASA</strong>.A.S.0<strong>04</strong>03 REV. 1 A310-3<strong>04</strong> - <strong>EASA</strong> STC <strong>EASA</strong>.A.S.0<strong>04</strong>03 revision 1(Ref.<br />
to former DGAC-F STC S1-72-<strong>01</strong>)- The STC<br />
<strong>EASA</strong>.A.S.0<strong>04</strong>03 has covered the transfer of<br />
the STC S1-72-<strong>01</strong>(Original Aviation Authority<br />
reference) from the original AviationAuthority<br />
(DGAC-F) to the <strong>EASA</strong> allowing the conve<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 />
30.10.2<strong>01</strong>2<br />
02.07.2008<br />
<strong>04</strong>.07.2008<br />
<strong>04</strong>.07.2008<br />
N/A 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 />
05.03.2<strong>01</strong>2<br />
N/A Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other<br />
previouslyinstalledmodification and/ or<br />
repair will introduce no adverse effect<br />
upon theairworthiness of the product.<br />
26.02.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 56/<strong>462</strong>
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