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 />
10032471 AIRLIFT A/S AS 350 B, AS 350 BA, AS 350 B1 Installation of Geophysical Equipments in A cargo mirror allowing in-flight observation of Prior to installation of this modification it 11.11.2<strong>01</strong>0<br />
AS 350 B2, AS 350 B3<br />
accordance with MasterDocument List DO-350- the spectrometer and EM/ magnetometer must be determined thatthe<br />
25-107, revision 0, dated 09.11.2<strong>01</strong>0 sensors must be installed<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 />
10035077 AIRLIFT A/S REV. 1 AS365N3 Installation of NVIS Lighting System in<br />
accordance with Airlift MOD.DO-365-33-1<strong>04</strong>.<br />
Note: Revision 1 introduces new helicopter<br />
configurations.<br />
10035080 AIRLIFT A/S P-<strong>EASA</strong>.R.S.<strong>01</strong>514 AS 365N2 Installation of NVIS Lighting System in<br />
accordance with Airlift MOD.DO-365-33-1<strong>01</strong>.<br />
10036162 AIRLIFT A/S AS350B1<br />
AS350B2<br />
AS350B3<br />
EC130B4<br />
10<strong>04</strong>1311 AIRLIFT A/S MBB-BK 117 C-2 NVIS certification in order to enable Night<br />
Vision Goggles operation.<br />
10031253 AIRMOTIVE ENGINEERING<br />
CORPORATION<br />
REV. 1 FAA STC SE1<strong>01</strong>29SC SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
10<strong>01</strong>4<strong>01</strong>1 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.<strong>01</strong>054 PIPER PA-23-250 Installation of1. COM/VOR/ILS/GPS-System<br />
Garmin GNS 4302. ELT Kannad 406AF<br />
10<strong>01</strong>4427 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.02472 CESSNA 208 Installation of a FLIR System, Inc. Ultramedia<br />
III/HD television camera. New Pilot Operating<br />
Handbook Supplement PO-0023-250000.<br />
Refer to applicable Flight Manual Supplement The installation of this modification by<br />
(FMS) for list of equipmentmandatory for Night third persons is subject towritten<br />
Vision Imaging System (NVIS) certification. permission of the approval holder and<br />
holding and disposal ofthe approved<br />
appropriate documentation. Installation of<br />
NVIS/NVG compatible lighting does not<br />
include or implyapproval<br />
Refer to applicable Flight Manual Supplement<br />
(FMS) for list of equipmentmandatory for Night<br />
Vision Imaging System (NVIS) certification.<br />
The installation of this modification by<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
holding and disposal ofthe approved<br />
appropriate documentation. Installation of<br />
NVIS/NVG compatible lighting does not<br />
20.<strong>04</strong>.2<strong>01</strong>2<br />
24.05.2<strong>01</strong>1<br />
Installation of Bendix/King KRA 405B Radar AS350B3 - only aircraft with Arriel 2B and<br />
include or implyapproval<br />
The approval holder shall fulfil the 17.08.2<strong>01</strong>1<br />
Altimeter.<br />
Arriel 2B1 engines installed.<br />
obligations of Part 21,<br />
Paragraph21A.118A. Prior to installation<br />
of this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repa<br />
Refer to applicable Flight Manual Supplement - The installation of this modification by<br />
(FMS) for list of equipmentmandatory for Night third persons is subject towritten<br />
12.09.2<strong>01</strong>2<br />
Vision Imaging System (NVIS) certification. permission of the approval holder and<br />
This Major Change is applicable only to holding and disposal ofthe approved<br />
helicopters deliveredNVIS-friendly from appropriate documentation. - Installation<br />
Eurocopter Deutschland GmbH, as defined of NVIS/NVG compatible lighting does<br />
not include or implyappro<br />
Installation of rotocoil, valve springs, ni-resist none Prior to installation of this modification it <strong>04</strong>.11.2<strong>01</strong>0<br />
valve guide, exhaustvalve with chrome flash on<br />
must be determined thatthe<br />
stem, and rocker shaft with thrust buttons<br />
interrelationship between this modification<br />
inaccordance with ECi Drawing Number<br />
and any other previouslyinstalled<br />
AEC65314, Rev E, dated February 6,2003, or<br />
modification and/ or repair will introduce<br />
later FAA approved revision - <strong>EASA</strong><br />
no adverse effectupon the airworthiness<br />
of the productIf the h<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
VFR; no AP, Max speed (camera operationg)<br />
115 KIAS, 2 pilots and max 4 passengers (see<br />
POH Supplement for full Limitations text).<br />
10<strong>01</strong>4848 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.03070 BEECH B200 SUPER KING AIR TDR-94D-007 Mode S Transponder Dual<br />
Installation.<br />
10<strong>01</strong>4849 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.03071 CESSNA T303 Installation of GNS480 COM/NAV/GPS,<br />
TAWS8000, Sky 497 Skywatch, KCS55A<br />
Compass System, SL30 COM/NAV,<br />
KN63DME, GWX68 Radar, MX200 MFD and<br />
GMA 347 Audio System. This installation<br />
includes also one Digiflow and Engine<br />
monitoring system.<br />
10<strong>01</strong>4851 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.03073 REV. 1 TWIN COMMANDER AIRCRAFT Installation of Garmin GTX 330 Mode S<br />
690<br />
Transponder<br />
10<strong>01</strong>4952 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.03216 CESSNA S550 (CITATION II) Installation of Bendix/King KLN 900, Shadin Prior to installation of this modification the<br />
ADC-200 and Garmin GNS 530A.<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 />
10<strong>01</strong>5062 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.03388 COMMANDER AIRCRAFT 690A GPS Antenna Installation. 25.03.2008<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 67/<strong>462</strong><br />
26.07.2006<br />
06.02.2006<br />
05.07.2007<br />
17.09.2007<br />
05.03.2008<br />
19.09.2007
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