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 />
10032621 AIR METHODS CORPORATION FAA STC SR00698DE-D BELL 429 Installation of Patient Loading System 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 />
17.11.2<strong>01</strong>0<br />
10<strong>04</strong>0541 AIR METHODS CORPORATION FAA STC SR00523DE SA365N, SA365N1, AS365N2 Installation of Emergency Medical Interior 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 />
09.07.2<strong>01</strong>2<br />
10<strong>04</strong>0543 AIR METHODS CORPORATION FAA STC SR00525DE SA365N, SA365N1, AS365N2 Installation of two (2) aft jump seats 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 />
09.07.2<strong>01</strong>2<br />
10<strong>04</strong>0545 AIR METHODS CORPORATION FAA STC SR00524DE SA365N, SA365N1, AS365N2 Installation of Articulating Patient Loading<br />
System<br />
10<strong>01</strong>7134 AIR SERVICE CENTER S.R.L. <strong>EASA</strong>.R.S.<strong>01</strong>228 A119 ASC 119-<strong>01</strong>-00 “Helibasket Kit” /Installation of<br />
External Basket<br />
10<strong>01</strong>7154 AIR SERVICE CENTER S.R.L. <strong>EASA</strong>.R.S.<strong>01</strong>260 A119 ASC 119-02-00 External self moving mirror<br />
kit/installation of external mirror in accordance<br />
with "Certification Report" Edition 0 dated 5<br />
February 2007 Rev. 1 dated 19 March 2007.<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 />
09.07.2<strong>01</strong>2<br />
Report Helibasket ASC 119-<strong>01</strong>-00 Part.3<br />
Chapter 4 RFM Supplement Ed.2 dated 21<br />
August 2006<br />
This installation should not be incorporated in<br />
any aircraft unless it is determined that the<br />
interrelationship between this installation and<br />
any previously approved configuration will not<br />
introduce any adverse effect upon the<br />
10034544 AIR SERVICE CENTER S.R.L. REV. 1 182 SERIES Installation of Vaccine Dispersal Kit.<br />
airworthiness of the aircraft<br />
None. None. 11.05.2<strong>01</strong>1<br />
10034547 AIR SERVICE CENTER S.R.L. REV. 1 AS 350 B3 Installation of Vaccine Dispersal Kit. None. None. 11.05.2<strong>01</strong>1<br />
10<strong>01</strong>4992 AIR SUPPORT INTERNATIONAL S.r.l. <strong>EASA</strong>.A.S.03288 PIPER PA-31T1 ASI BMA <strong>04</strong>/B/06 “Installation of Garmin GNS 1. Prior to installation of this modification the<br />
22.10.2008<br />
430 & GNS 530, Goodrich WX 500, Garmin installer must determine that the<br />
MX 20 and Accessories”<br />
interrelationship between this modification<br />
andany other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product. The insta<br />
10<strong>01</strong>5293 AIR SUPPORT INTERNATIONAL S.r.l. <strong>EASA</strong>.A.S.03835 MOONEY M20K ASI BMA <strong>01</strong>/B/09 “ Installation of Garmin GNS<br />
430W for B-RNAV Operation”<br />
1) The approval holder shall fulfil the<br />
obligations of Part 21, Paragraph 21.A1092)<br />
10030246 AIR SUPPORT INTERNATIONAL S.r.l. PA -30<br />
Limited to S/N 25-0862<br />
ASI BMA <strong>01</strong>/B/10 "Installation of Garmin GNS None.<br />
430W approved for B-RNAV andother avionic<br />
equipment".<br />
None. 07.06.2<strong>01</strong>0<br />
10030248 AIR SUPPORT INTERNATIONAL S.r.l. PA-30 None. None. 07.06.2<strong>01</strong>0<br />
10<strong>01</strong>4142 AIRBERLIN TECHNIK GmbH <strong>EASA</strong>.A.S.<strong>01</strong>256 REV. 1 A330-322 Cabin reconfiguration from a 18 B/C + 331 Y/C none Prior to installation of this modification it 22.05.2<strong>01</strong>2<br />
layout to a 18 B/C + 343Y/C layout.This STC<br />
must be determined thatthe<br />
installs a new cabin arrangement.The Revision<br />
interrelationship between this modification<br />
1 retains the certificated design of the<br />
and any other previouslyinstalled<br />
<strong>EASA</strong>.A.S.<strong>01</strong>256 andcapture the transfer of<br />
modification and/ or repair will introduce<br />
STC ownership from LTU (owned by Air<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>4924 AIRBERLIN TECHNIK GmbH <strong>EASA</strong>.A.S.03172 REV. 1 A330-322 Business Class extension to a 30 B/C + 295<br />
Y/C layout.This STC modifies cabin<br />
arrangementfrom a 18 B/C +343 Y/C layout to<br />
a 30B/C +295 Y/C layout with new B/C seat<br />
and stowage compartmentinstallations.The<br />
Revision 1 retains the certificated design of the<br />
E<br />
24.10.2006<br />
30.<strong>04</strong>.2007<br />
10.06.2009<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 />
22.05.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 54/<strong>462</strong>
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