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 />
10036114 AIRWOLF AEROSPACE L.L.C. FAA STC SR02964CH 206,206A,206B,206L,206L-1 Tension-Torsion strap - Replacement of life none Prior to installation of this modification it 11.08.2<strong>01</strong>1<br />
206L-3,206L-4<br />
limited part<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>6590 AIRWOLF FILTER CORPORATION <strong>EASA</strong>.IM.A.S.03000 FAA STC SA02268CH SEE ATTACHED <strong>EASA</strong><br />
APPROVED TYP<br />
10<strong>01</strong>7141 AIRWORK FRANCE <strong>EASA</strong>.R.S.<strong>01</strong>243 AS 355 F, AS 355 F1, AS 355 F2<br />
AS 355 N<br />
10<strong>01</strong>7142 AIRWORK FRANCE <strong>EASA</strong>.R.S.<strong>01</strong>244 AS 350 B, AS 350 BA<br />
AS 350 B1, AS 350 B2<br />
AS 350 B3<br />
10<strong>01</strong>7190 AIRWORK FRANCE <strong>EASA</strong>.R.S.<strong>01</strong>327 AS 350 B, AS 350 B1<br />
AS 350 B2, AS 350 BA<br />
AS 350 B3<br />
10<strong>01</strong>7191 AIRWORK FRANCE <strong>EASA</strong>.R.S.<strong>01</strong>328 AS 355 E, AS 355 F, AS 355 F1<br />
AS 355 F2, AS 255 N, AS 355 NP<br />
10<strong>01</strong>5355 AIRWORTHINESS RESOURCES<br />
CORPORATION<br />
Installation of Airwolf Filter Corp Air Oil<br />
Seperator<br />
Installation of Thales AGILE 2 external camera<br />
and associated cabin electronic control unit.<br />
Installation of Thales AGILE 2 external camera<br />
and associated cabin electronic control unit, in<br />
accordance with AIRWORK STC file<br />
n°AWF.0<strong>01</strong>.05 revision A, dated January 2007,<br />
or later <strong>EASA</strong> approved revision.<br />
Nouveau système de prises de vues frontales<br />
(Front Mounted Camera Installation).<br />
Nouveau System de Prises de Vues<br />
Frontales(Front Mounted Camera Installation)<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<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
1. 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 upon the<br />
airworthiness of the product.2.<br />
This STC is not approved for Category A<br />
operations.<br />
<strong>EASA</strong>.IM.A.S.00640 REV. 1 TCCA STC SA00-148 BOMBARDIER CL-415 Installation of an Integrated Liquid Spray 1. Operation in accordance with AFM<br />
System (ILSS)Relocation of the cockpit control Supplement C53790 Rev. B or later approved<br />
panel for the Integrated Liquid Spray System revision. AMM Supplement A65-10, or later<br />
(ILSS)<br />
approved revision.2. Prior to installation of<br />
this modification the installer must determine<br />
that the interrelationship betwee<br />
10<strong>01</strong>7050 AKV Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>474 FAA STC SR<strong>01</strong>958LA EUROCOPTER FRANCE AS 350<br />
B2<br />
Installation of AKV, Inc. Ng/Np Cycle Counter<br />
P/N 350NGLTSB2<br />
AS350B2 modification iaw STC<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>222 issued on 20 March 2008<br />
is required prior to the installation of the Ng/Np<br />
Cycle Counter. The Ng/Np Cycle Counter can<br />
only be installed on day/night VFR aircraft with<br />
non-FADEC equipped engine.The Ng/Np<br />
Cycle<br />
10028164 AKV Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>555 FAA SR00631DE-D 31.07.2009<br />
10<strong>01</strong>7181 ALIDAUNIA S.R.L. <strong>EASA</strong>.R.S.<strong>01</strong>3<strong>04</strong> A109 E Installation of a Ginevri Incubator Type "Baby Agusta A109E equipped with Agusta Kit EMS<br />
14.08.2006<br />
10<strong>01</strong>7242 ALIDAUNIA S.R.L. <strong>EASA</strong>.R.S.<strong>01</strong>436 MBB-BK 117 C-1<br />
Shuttle Intensive Care" P/N 7634B complete of P/N 109-0326-69-103.<br />
the attachment fittings<br />
MB <strong>01</strong>8/ALI/2008 "Installation of GPS/Satellite Prior to installation of this modification the<br />
System usable to locate the helicopter position. 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 />
18.07.2008<br />
10028026 ALIDAUNIA S.R.L. P-<strong>EASA</strong>.R.S.<strong>01</strong>508 A109S BM No. 020/AL/2008 Installation of a "Ginevri"<br />
Incubator Type "BabyShuttle Intensive Care"<br />
10035253 ALIDAUNIA S.R.L. A109A II MB 022/ALI/2<strong>01</strong>0 "Installation of Alternate<br />
Static Pressure Source forthe Indicator:<br />
Altimeter, Airspeed & Vertical Speed"<br />
19.02.2009<br />
27.11.2008<br />
27.02.2007<br />
16.06.2008<br />
16.06.2008<br />
22.10.2007<br />
29.07.2008<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 />
26.11.2009<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 />
15.07.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 70/<strong>462</strong>
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