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 />
10037159 AIRBERLIN TECHNIK GmbH A320-214 A320 Cabin Reconfiguration for AZAL - This design change (STC) is applicable to the This STC does not require a revision or 07.11.2<strong>01</strong>1<br />
following AirbusA320-214 serial number supplement to the original TCHolder's<br />
aircraft (MSNs):2685; 2846; 2853; 2865; 2991 EWIS Instructions for Continued<br />
and 3006.<br />
Airworthiness.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other p<br />
10039755 AIRBERLIN TECHNIK GmbH <strong>EASA</strong>.A.S.005<strong>04</strong> REV. 1 A330-322 Cabin reconfiguration from a 387 Y/C layout to None Prior to installation of this modification it 22.05.2<strong>01</strong>2<br />
a 18 B/C + 331 Y/Clayout.This STC installs a<br />
must be determined thatthe<br />
new cabin arrangement with in-seat video<br />
interrelationship between this modification<br />
andadditional galley installations.The Revision 1<br />
and any other previouslyinstalled<br />
retains the certificated design of the<br />
modification and/ or repair will introduce<br />
<strong>EASA</strong>.A.S.005<strong>04</strong> andcapture the tran<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong>1988 AIRBORNE MAINTENANCE AND FAA STC ST<strong>01</strong>096CH 767-200/ -300 Upgrade of Teledyne Digital Flight Data<br />
Acquisition Unit<br />
10<strong>04</strong>1989 AIRBORNE MAINTENANCE AND REV. 1 FAA STC ST02325CH 767-200/ -300 Installation of Electronic Standby Instrument<br />
System (ESIS)<br />
10033764 AIRBORNE TECHNOLOGIES GmbH REV. 1 P.68TC "OBSERVER" Change of cabin layout /For the installation of<br />
different mission equipment in a<br />
VulcanairP.68TC aircraft, the aircraft cabin has<br />
to be modified and provisions toaccommodate<br />
Mission Equipment have to be installed. This<br />
modificationincludes the removal of t<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 />
Only to be installed on a/c with <strong>EASA</strong> STC<br />
10036223 installed.<br />
Prior to installation of this modification it 05.11.2<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 />
Limited to S/N 454, 456 and 459 Prerequisites:Vulcanair Service Bulletin<br />
No. 163 must be installed prior or<br />
concurrentthis modificationVulcanair<br />
Mod.P68/129 must not installed prior or<br />
concurrent thismodificatonThe approval<br />
holder shall fulfill the obligations of Part<br />
21,Paragraph<br />
10033844 AIRBORNE TECHNOLOGIES GmbH REV. 2 T182T Camera Hatch Installation none The approval holder shall fulfil the<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 />
repair<br />
24.05.2<strong>01</strong>2<br />
10034631 AIRBORNE TECHNOLOGIES GmbH REV. 1 P2006T Provisions for surveillance configurationFor Step 1 and 3 can be installed without Prior to installation of this modification it 26.10.2<strong>01</strong>1<br />
standard analogue instruments equipped prerequisite, step 2 and step 4requires step 1 must be determined thatthe<br />
aircraft:Step 1: installation of a camera hatch, and step 3The installation of this STC must be interrelationship between this modification<br />
electric doors, and a 28Vmission power carried out while production of theaircraft at the and any other previouslyinstalled<br />
systemStep 2: installation of an electric camera facilities of the airplane manufacturer. modification and/ or repair will introduce<br />
lift For Garmin G950 equipped aircr<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10036443 AIRBORNE TECHNOLOGIES GmbH P.68 "OBSERVER 2"<br />
P.68 "OBSERVER"<br />
P.68TC "OBSERVER"<br />
10038317 AIRBORNE TECHNOLOGIES GmbH P.68 "OBSERVER 2"<br />
P.68 "OBSERVER"<br />
P.68TC "OBSERVER"<br />
Mission cabin configuration /For the installation<br />
of different mission equipment in a Vulcanair<br />
P.68aircraft, the aircraft cabin has to be<br />
modified and provisions toaccommodate<br />
Mission Equipment have to be installed. The<br />
installation ofmission equipment it<br />
None Prerequisite:Vulcanair Service Bulletin<br />
No. 163 must be installed prior or<br />
concurrentthis modificationThe approval<br />
holder shall fulfill the obligations of Part<br />
21,Paragraph 21.A109. Prior to<br />
installation of this modification it must be<br />
determined tha<br />
Electric Camera Lift installation/Installation of Airborne Technologies STC-AT-036 must be<br />
an electric camera lift, an operator console and installed prior or concurrentwith this<br />
acamera lift control panel.<br />
modification<br />
<strong>04</strong>.<strong>01</strong>.2<strong>01</strong>2<br />
08.09.2<strong>01</strong>1<br />
The approval holder shall fulfill the 06.02.2<strong>01</strong>2<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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 55/<strong>462</strong>
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