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 10038053 FOKKER SERVICES B.V. F28 MARK 0070 Activation of WLAN functionality of an already -Installation of EASA STC 10027637 is a Prior to installation of this modification it 16.01.2012 installed andcertificated router (ref EASA STC prerequisite for this STC-Limitation of Wireless must be determined thatthe 10027637)The Fokker 70 aircraft contains a Local Area Network as documented in AFM interrelationship between this modification router that has been certificatedunder STAC changeAFMJET2011-007 and any other previouslyinstalled 10027637. Fokker Services will activate and modification and/ or repair will introduce certificate theWLAN functionali no adverse effectupon the airworthiness of the product. 10042160 FOKKER SERVICES B.V. B737-600/-700/-800/-900/-900ER Introduction of LED light assembles in the Boeing B737 NG aircraft 10015713 FOKKER50FREIGHTER STC CORP. EASA.IM.A.S.01710 REV 1 FAA STC ST01916LA FOKKER F.27 MARK 050 Installation of Large Cargo door.Installation of Large Cargo door. 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. 12.11.2012 1. To allow the carriage of cargo STC IM.A.S.01711 shall be incorporated;2. The maximum number of occupants in the aircraft including crew members is 3;3. This STC is approved only for the product configuration as defined in the approved design da 10015714 FOKKER50FREIGHTER STC CORP. EASA.IM.A.S.01710 REV 1 FAA STC STO1916LA - EASA.IM.A. FOKKER F.27 MARK 050 21.05.2008 10015715 FOKKER50FREIGHTER STC CORP. EASA.IM.A.S.01711 REV 1 FAA STC ST00260DE FOKKER F.27 MARK 050 Installation of Class E Cargo Interior, 1. Cargo Loading Manual WB-2052 Rev. C or 02.11.2007 configuration 24B301-211 in accordance with later approved revisions shall be used when Branson Aircraft Corporation Drawing List loading the aircraft.2. This STC is approved 24A300, revision B dated November 5, 1996, only for the product configuration as defined in FAA approved November 7, 1996 or later the approved design data referred to in the revision approved in accordance with ED Decision paragraphs "Description" and “As 10028703 FORCED AEROMOTIVE FAA STC SE10926SC IO-550-N Installation of BAR Air, LLC supercharger The supercharged IO-550-N engine is limited Prior to installation of this modification it 03.02.2010 TECHNOLOGIES system on Teledyne ContinentalMotors IO-550- to 29.6 in Hg (204 kPa) MAPand 2700 RPM or must be determined thatthe N Engines in accordance with Master Drawing 310 HP (231 kW). interrelationship between this modification ListMDL-SR22-1-E, Revision A, dated April 4, and any other previouslyinstalled 2008 or later FAA approvedrevision - EASA modification and/ or repair will introduce Validation of FAA STC SE10926SC. no adverse effectupon the airworthiness of the product If the 10029290 FORCED AEROMOTIVE TECHNOLOGIES 10029878 FORCED AEROMOTIVE TECHNOLOGIES 10030005 FORCED AEROMOTIVE TECHNOLOGIES FAA STC SA10925SC SR22 Installation of BAR Air, LLC modified Teledyne As referred in limitations section of the AFM-S Continental MotorsIO-550-N iaw. MDL-SR22-1- 22006Engine must be modified acc. EASA A, Rev. E or later FAA approved revisions.Installation requires EASA STC 10028703 to be installed. STC 10028703 FAA STC SE10233SC O-470-L, -R, -S, -U Installation of a Belt-Driven Vortech V-1S supercharger assembly on theTeledyne Continental Motors (TCM) O-470-L, O-470-R, O-470-S, and O-470-Uengines in accordance with Type Inspection Data contained in MasterDrawing List No. MDL-182-1-E, Rev. D, dated Ja FAA-STC SE10233SC 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R The supercharged O-470-L, -R, -S, and -U engines are limited to 28 inHg(193 kPa) MAP and 2600 RPM or 230 HP (171.5 kW) with minimum fuel gradeAvgas 100LL. Installation of Rod Sage Supercharged This Supplemental Type Certificate requires Teledyne Continental Motors (TCM)O-470-L, O- installation of EASA STC10029878 (see also 470-R, O-470-S and O-470-U Engines in acc. FAA-STC SE10233SC) with FAA STCSA10232SC 10033805 FR AVIATION LIMITED B300 Observer Training Platform Mod.-B300. The approval is limited to the Aircraft Serial Numbers: FL-597,FL-618, FL-629 and FL-633. 21.05.2008 Prior to installation of this modification the 17.03.2010 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product.The installatio 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 productIf the h 28.04.2010 Prior to installation of this modification it 10.05.2010 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 Prior to installation of this modification the 09.02.2011 installer must determinethat the ,,interrelationship between this modification and any otherpreviously installed ,,modification will introduce no adverse effectupon the airworthiness of the product. The instal 04/01/2013 Page 224/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10035091 FR AVIATION LIMITED TYPE: FAN JET FALCON Extended underwing stores carriage (flutter This approval only addresses the clearance of The responsible design organization must 30.05.2011 BASIC, D AND E SERIES clearance)The goal is to approve the flutter the pod configurationswith respect to flutter, all ensure that the intendedconfiguration is clearance of underwing storeconfigurations other aspects of the certification process,such within the scope of the approved design installed onto Fan Jet Falcon aircraft with as structural strength, effects on aircraft definition forthe flutter analysis. existingunderwing hard points. This design handling andperformance, system safety and definition establishes an envelope of environmental prot 10042074 FRAKES AVIATION EASA.IM.A.S.00228 1900 Installation of engine exhaust stub in 1. Compability of this modification with 28.10.2004 1900C accordance with Frakes AviationInstallation previously installed equipmentmust be 1900D drawing number FA5726, dated September 6, determined by installer 2. This SIC is 200 1985, for the 200series, and drawing FA5601 issued as result of the validation of the 200C dated June 19, 1995 for the 300 and Frakes AviationSIC N° SA8703SW 300 1900series, or later EASA-approved revision approved by the FAA on October 27, 300LW B200 B200C B300 B300C 1993 and amended onJune 21, 19 10014725 FRANCE AVIATION EASA.A.S.02902 BEECH F33 Installation and BRNAV approval of Garmin GNS-480. 05.12.2006 10014839 FRANCE AVIATION EASA.A.S.03056 BEECH B200 Installation of Honeywell MST-67A Mode S Prior to installation of this modification the 18.06.2007 Transponder. installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10014914 FRANCE AVIATION EASA.A.S.03159 PIPER PA-32 Rudder Hand Control installation for lower Limbs.The "SD1" system consists in a control for rudder that is handled by the pilot while seated in the LH (Left Hand) station. This "SD1" RHC system is mountained on existing manufacturing rudder system. The sy 10015002 FRANCE AVIATION EASA.A.S.03302 BEECH F90 Installation of 2 Collins 8.33 KHz COMM System and GTX330D mode S diversity transponder. 10015014 FRANCE AVIATION EASA.A.S.03316 BEECH F90 IFR/RNAV classification of the GNS530AW AFMS No. AFM-35-2007-001, dated 26/09/2007 or later approved revision must be used with the modification. The following AFMS must be used when coupled to the autopilot; basic IFR classification modification is applied:Aircraft Flight Manual of the GNS430AW and Mode S transponder Supplement for GTX330/330D, # AFM-38- GTX330 installation. 2007-001 revision 1, dated 10/04/2008, or later approved revisions.Aircraft Flight Manual Supplement for GMX200, # AFM-38-2007-002 revi 10015028 FRANCE AVIATION EASA.A.S.03335 PIPER PA-28 Rudder hand control and brake system Prior to installation of this modification the forlower limbs disabled pilot. The "LPS" rudder installer must determine that the hand control and brake system installation is to interrelationship between this modification and permit LLD pilot to operate the aircraft without any other previously installed modification will safety pilot or flight instructor in the right hand introduce no adverse effect upon the pilot station. The "L airworthiness of the product. 10017205 FRANCE AVIATION EASA.R.S.01357 EUROCOPTER DEUTSCHLAND Installation of Avidyne Adivsory System TAS- Installation limited to EC 135 T2 s/n 274. 30.11.2007 EC-135 620. 10033540 FRANCE AVIATION P-EASA.A.S.03527 BEECH A36 FA 06/2008 Rev. 2 - Avionic change with B- None Prior to installation of this modification it 06.07.2009 RNAV/SID/STAR/GNSS andconventional non- must be determined thatthe precision approaches privileges with AP interrelationship between this modification coupling. and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 04/01/2013 Page 225/462 23.11.2007 10.12.2007 23.05.2008 24.06.2008
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04/01/2013 Page 1/462 - EASA

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