04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10029712 DART AEROSPACE Ltd. P- TCCA STC SH07-36 A119 & AW119 MKII TCA STC SH07-36 Issue 2 "Replacement Not Applicable Prior to installation of this modification it 15.04.2010 EASA.IM.R.S.01380 Windows Kit" - D119-755-011/-14 -This STC must be determined thatthe involves removing of the existing window and interrelationship between this modification installing a flatwindow (-011) in LH or RH crew and any other previouslyinstalled door or installing a bubble window (-14)in the modification and/or repair will introduce RH crew door) no adverse effectupon the airworthiness of the product. 10031514 DART AEROSPACE Ltd. TCCA STC SH05-4 AS350 B, B1, B2, B3, BA, D Installation of an Auxiliary Side Locker Fuel Tank. 10032253 DART AEROSPACE Ltd. TCCA STC SH09-37 ISSUE 1 1. 214B, 214B-1 2. 212, 412, 412 EP 3. 204B, 205A-1 10033253 DART AEROSPACE Ltd. TCCA STC SH10-44 206, A, A1, B, B1 L, L1, L3, L4, 407 none Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product 20.08.2010 D412-791 Safety Enhancement kits None Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 05.11.2010 Automatic Door Opener Kits (Cabin and Baggage Doors). None Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product 07.01.2011 10034340 DART AEROSPACE Ltd. TCCA STC SH10-49 429 Installation of UltraPaws. None. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 25.03.2011 10034634 DART AEROSPACE Ltd. EASA.IM.R.S.01560 TCCA STC SH92-18 AS350B, BA, B1, B2, B3, D, D1 D350-567 Vertical Reference Window Installations. Addition of AS350Dl tolist of models.This STC revises and supersedes DGAC France STC 84-5[1103, dated 27September 2002. None Prior to installation of this modification the 17.07.2009 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. The installati 10034636 DART AEROSPACE Ltd. EASA.IM.R.S.01561 TCCA STC SH92-18 AS355E, F, F1, F2, N, NP D350-567 Vertical Reference Window None Prior to installation of this modification the 31.07.2009 Installations.This STC is a revision of and installer must determinethat the supersedes DGAC-F STC 168-511104 dated interrelationship between this modification 27September 2002 for addition of AS355N and and any otherpreviously installed NP to list of models. modification will introduce no adverse effect uponthe airworthiness of the product. The installati 10034637 DART AEROSPACE Ltd. EASA.IM.R.S.01453 TCCA STC SH02-33 1. AS350 D, B, B1, B2, BA, B3 1. (OP-3369 OPTION EXCLUDED) 2. AS355 E, F, F1, F2, N 10035429 DART AEROSPACE Ltd. REV. 2 TCCA STC SH11-1 206L, 206L-1, 206L-3, 206L-4 407 Installation of Dual High Back Seat, Left Forward Position (Modificationapproved by TCCA under STC SH02-33 issue 1) D407-797 Heli Utility Basket and Heli Access Step Installation, Revisionto STC 10035429 to add D407-797-311 Heli Access Step. None Prior to installation of this modification the 03.06.2009 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. The installati None. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 28.11.2011 04/01/2013 Page 166/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10039042 DART AEROSPACE Ltd. REV. 1 206 A/B/L/L1/L3/L4 Screw In Windshield Modification. None. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 30.04.2012 10042362 DART AEROSPACE Ltd. DGAC STC 168- SI0994 REV. 1 TCCA SH 90-4 ISSUE 4 AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP. 10016785 DART AEROSPACE USA, Inc. EASA.IM.R.S.01126 FAA STC SR01583SE AGUSTA AB-412 AGUSTA AB-412EP BELL 205A BELL 205A-1 BELL 205B BELL 212 BELL 412 BELL 412 CF BELL 412 EP 10016934 DART AEROSPACE USA, Inc. EASA.IM.R.S.01320 REV. 1 FAA STC SA00475SE BELL 206 BELL 206A BELL 206B BELL 206L BELL 206L-1 BELL 206L-3 BELL 206L-4 BELL 407 10016945 DART AEROSPACE USA, Inc. EASA.IM.R.S.01339 TCCA STC SH98-14 BELL 206A BELL 206B BELL 206L BELL 407 10017001 DART AEROSPACE USA, Inc. EASA.IM.R.S.01412 FAA STC SR00211SE EUROCOPTER FRANCE AS 350 B1 EUROCOPTER FRANCE AS 350 B2 EUROCOPTER FRANCE AS 350 B3 EUROCOPTER FRANCE AS 350 BA EUROCOPTER FRANCE AS 350 C EUROCOPTER FRANCE AS 350 D EUROCOPTER FRANCE AS 350 D1 EUROCOPTER FRANCE AS 350B EUROCOPTER FRANCE AS 355E EUROCOPTER FRANCE AS 355F EUROCOPTER FRANCE AS 355F1 EUROCOPTER FRANCE AS 355F2 EUROCOPTER FRANCE AS Installation of rear locker extender as defined in Dart Aerospace LtdMaster Document List No. MDL-D350-604 Rev. C.Note 1.This approval amends DGAC STC 168-SI0994 to add the AS355N and AS355NPaircraft models.Note 2.This STC is the validation of TCCA STC SH9 Installation of DART D412-742 Float Skidtubes (FAA STC SR01583SE issued on 29 July 2005) Replacement of the original landing gear skid tubes and saddles with DART Aerospace Model D206-642 skid tubes and saddles. This TV modifies STC EASA.IM.R.S.01320 D206-628 Heli Access Steps. This STC has been classified as “BASIC” by the FAA and is approved under the Type Validation Principles. D350-764 Shoulder Harness Kits. This STC has been classified as "BASIC" by the FAA and has been approved under the PTVP. 10017034 DART AEROSPACE USA, Inc. EASA.IM.R.S.01458 FAA STC SR00948SE 355N AGUSTA A-119 FAA STC SR00948SE “D119-675 Heli-Access- AGUSTA AW-119 MKII Step”. 10017045 DART AEROSPACE USA, Inc. EASA.IM.R.S.01469 REV. 1 FAA STC SR00910SE EUROCOPTER CANADA BO-105 D105-674 Skidtube Installation i.a. with FAA LS A- EUROCOPTER DEUTSCHLAND BO-105 STC SR00910SE None Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 27.11.2012 Installation Insttruction IIN-D412-742 Rev. B dated 3 October 2005 or later approved document.This approval should not be extended to other rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined b 04/01/2013 Page 167/462 12.05.2006 10.09.2007 26.07.2007 05.03.2008 18.04.2008 07.01.2009
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04/01/2013 Page 1/462 - EASA

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