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 10014782 GKN AEROSPACE SERVICES LIMITED EASA.A.S.02980 BOEING 737-100 Number 2 Cockpit Windshields Addition of This approval provides for the installation of the 19.12.2007 BOEING 737-200 Layers of Polyrethane Interlayer to the Existing referenced windows individually or in any BOEING 737-200C Qualified Design to improve In-Service combination. BOEING 737-300 BOEING 737-400 BOEING 737-500 BOEING 737-600 BOEING 737-700 BOEING 737-700C BOEING 737-800 BOEING 737-900 Reliability. 10036545 GKN AEROSPACE SERVICES LIMITED P-EASA.A.S.03492 REV. 1 B777-200, B777-200LR Installation of a GKN Aerospace designed None Replacement of a Flight Compartment 02.11.2011 B777-300, B777-300ER Boeing 777 No 1 Windshield PartNo. 10702 Window Number 1 per this STC withGKN B777F (LH) / 10703 (RH); or Part No. 10712 (LH) / ATS part no. 10712 (LH) / 10713 (RH) 10713 (RH) together with the relevantwiring loom modification constitutes an Alternative Method of Compliance(AMOC) to the terminating action requirements of 10015318 GLOBAL AIRWORKS, Inc. EASA.IM.A.S.00254 REV. 1 FAA STC ST01626LA; EASA.IM.A.S BOMBARDIER CL-600-2B19 BOMBARDIER CL-600-2C10 BOMBARDIER CL-600-2D24 10016684 GLOBAL AIRWORKS, Inc. EASA.IM.A.S.C.0105 9 REV. 1 FAA STC ST01585LA A330-201, A330-202, A330-203 A330-223, A330-243, A330-301 A330-321, A330-322, A330-323 A330-341, A330-342, A330-343 10041546 GLOBAL AIRWORKS, Inc. FAA STC ST3042CH ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-500 ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212, ATR 72-212A. Installation of Airworks Cockpit Door Prior to installation of this modification the Surveillance SystemRevision 1: Amended FAA installer must determine that the STC ST01626LA interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install Installation of AirWorks Cockpit Door Prior to the installation of this modification it Surveillance Systems (Validationof the FAA must be determinedthat the interrelationship STC ST01585LA). This STC installs a CDSS. between this modification and any The Revision 1 has been issued to correct the otherpreviously installed modification and/or references of AssociatedTechnical Documents. repair will introduce noadverse effect upon the airworthiness of the product. 05.01.2009 30.11.2011 Installation of a Global AirWorks Cockpit Door None Surveillance SystemThis STC installs a cockpit door surveillance system (CDSS) allowingcrew to view video images of the area outside the cockpit door. None 26.09.2012 10015704 GODERICH AIRCRAFT Inc. EASA.IM.A.S.01691 - BEECH B300 Artex ELT C406-N Installation. Modification limited to s/n FL-175.Maintenance must be in accordance with above Continued Airworthiness document 10015705 GODERICH AIRCRAFT Inc. EASA.IM.A.S.01692 BEECH B300 Universal UNS 1E Flight Management System Installation. Modification limited to s/n FL-175.Operation must bein accordance with Goderich Aircraft Inc. Flight Mnaual Supplement FMS05097-1 Revision N/C approved 20 September 2005 or later approved revision. Maintenance must be in accordance with above Continued Air 10015886 GODERICH AIRCRAFT Inc. EASA.IM.A.S.02004 O-LSA06-081/D (LSTC) BEECH 400A (HAWKER 400 XP) Cabin Entertainment Equipment Installation. This Installation is limited to the Serial No. RK- 37 (Registration SE-DRS).This approval is for electrical/avionics aspects only. Structural aspects of this installation are not included and require separate approval. 10015887 GODERICH AIRCRAFT Inc. EASA.IM.A.S.02005 O-LSA06-117/D (LSTC) BEECH 400A (HAWKER 400 XP) Change in interior seating arrangement, 1. This Installation is limited to the Serial No. addition of sink to existing rear lavatory, RK-37 (Registration SE-DRS).2. Compatibility fabrication and installation of RH fwd of this modification with other previously cabinet,revision of existing LH fwd cabinet, approved modifications must be determined by revision to interior finishing details, and addition the installer. of new fuselage antenna. 10016452 GODERICH AIRCRAFT Inc. EASA.IM.A.S.02798 TCCA STC O-LSA08-056/D ISSUE 3 FALCON 10 EASA Validation of Transport Canada Limited STC O-LSA08-056/D Issue 3:Cabin Entertainment Equipment Upgrade for Falcon 10 serial number 161 aircraft in accordance with Avionics Design Services Ltd. Master Drawing List MDL08009 Revision B, dated 31st March EASA STC limited to Falcon 10 serial number 161 aircraftSee original Transport Canada Limited STC O-LSA08-056/D Issue 3See: Avionics Design Services Ltd. Master Drawing List MDL08009 Revision B, Issue 1, dated 31st March 2008.Goderich Aircraft Inc. Mainten 04/01/2013 Page 236/462 17.01.2006 17.01.2006 09.11.2006 19.12.2006 21.04.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014214 GOMOLZIG FLUGZEUG- UND EASA.A.S.01374 REV 1 CESSNA 182E Installation of Noise Reduction Kit C182- 1. The approval is valid only in combination 04.08.2006 MASCHINENBAU CESSNA 182F 606650 with the installation of FAA STC SA009133SC CESSNA 182G (Texas Skyways Inc) or STC SA00152WI (Air CESSNA 182H Plains Services Corp.) Both with own EASA CESSNA 182J approval.2. The approval for the models CESSNA 182K CESSNA 182L CESSNA 182M CESSNA 182N CESSNA 182P CESSNA 182Q CESSNA F182-P CESSNA F182-Q Cessna 182 E, F and G is not valid fo 10014302 GOMOLZIG FLUGZEUG- UND EASA.A.S.01546 DR300/108, DR300/125 Operation on unleaded automotive gasoline in 14.09.2005 MASCHINENBAU DR300/180R, DR315 DR400/120(D), DR400/125 DR400/140B, DR400/180R DR400/2+2, DR400/140 accordance with Norm EN 228 10014483 GOMOLZIG FLUGZEUG- UND EASA.A.S.02546 PIPER PA-23-250 Modification 13452Alteration of Piper PA-23- 13.03.2006 MASCHINENBAU 250 aircraft to aerial work with a Leica ADS 40 digital camera installation in addition to the installation of Zeiss RMK 15 Top Cameras based on EASA approval No. 2004-9428 10014590 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10014635 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10014670 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10014832 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10014836 GOMOLZIG FLUGZEUG- UND MASCHINENBAU 10014907 GOMOLZIG FLUGZEUG- UND MASCHINENBAU EASA.A.S.02699 DIAMOND HK-36 SUPER DIMONA Modification of the Dimona HK 36 R "Super Dimona" equipped with the engine Rotax 912 A3 with the alternative Propeller MTV-21-A- CF/C175-05. EASA.A.S.02779 CESSNA 172S Installation of Noise Reduction Kit C172S- 606560 EASA.A.S.02829 REV. 2 CESSNA 172RG Modification 14839Installation of Low Noise Silencer Kit "System Gomolzig" C172RG_606520 All S/N of the variant: HK 36 R "Super Dimona" 11.06.2008 None 26.09.2006 As referred in AFM-S Must be maintained iaw. Original Cessna 22.02.2012 MM and in addition iawMaintenance Instructions given in the above mentioned InstallationInstructions or later approved revisions. Prior to installation of this modification it must be determined thatthe interrelatio EASA.A.S.03047 REV. 1 1. PA-34-200T (SENECA II) System PA-34-812000Installation of Penta As referred in AFM-S Must be maintained iaw. Original Piper 21.12.2011 1. PA-34-220T (SENECA III) Camera SystemSystem PA-34-813000 MM and in addition iawMaintenance 1. PA-34-220T (SENECA IV) Version 2024425Camera Hatch and Instructions given in the above mentioned 2. PA-34-220T (SENECA V) Equipment Installation InstallationInstructions or later approved revisions.Prior to installation of this modification it must be determined thatthe interrelations EASA.A.S.03052 CESSNA 182 Towing Kit Cessna 182 "System Gomolzig" Cessna 182M, N,P,Q,R, equipped with SMA 12.10.2007 C182-820000".The Cessna 182 and its series SR 305-23-MA01 Diesel engine according to equipped with the SMA Diesel engine shall be equipped with a towing system for banning towing and sailplanes up to 850 kg MTOW. STC EASA.A.S.00774. EASA.A.S.03145 REV. 1 TP206C-E, TU206B, TU206E-G, T206H. Cessna Exhaust System with Extension1. as referred in limitations section of the AFM-S TP206C-E; TU206B, E-G Exhaust System with xxx Extension c()206()-6065802. T206H Low Noise Silencer Kit CT206H-606570 Prior to installation of this modification it 30.11.2012 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. If the 04/01/2013 Page 237/462
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04/01/2013 Page 1/462 - EASA

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