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 10031460 BLACKHAWK MODIFICATIONS Inc. EASA.IM.A.S.03209 FAA STC SA01248SE PA-31T EASA Validation of FAA STC SA01248SE - none Prior to installation of this modification it 17.08.2010 PA-31T1 Installation of two HartzellHC-E4N- must be determined thatthe 3N/D8990SB propellers interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10031462 BLACKHAWK MODIFICATIONS Inc. EASA.IM.A.S.03208 FAA STC SA00863SE PIPER PA-31T PIPER PA-31T1 PIPER PA-31T2 10031945 BLACKHAWK MODIFICATIONS Inc. FAA STC SA10816SC 425 Installation of Ultra Electronics engine torque indicators in Cessna 425in accordance with FAA STC SA10816SC EASA Validation of FAA STC SA00863SE- none Prior to installation of this modification it 17.08.2010 Installation of two Pratt &Whitney PT6A-135 or must be determined thatthe PT6A-135A engines and two HartzellHC-B3TN- interrelationship between this modification 3B/T10178B-8R or HC-E4N-3N/D8990SB and any other previouslyinstalled propellers modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 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. 24.09.2010 10036326 BLACKHAWK MODIFICATIONS Inc. FAA STC SA01946LA PA-31T, PA-31T1, PA31T2 Installation of Powerplant Indication System. None. Blackhawk Modifications Inc, FAA STC’s 01.09.2011 ref SA00863SE (PT6A- 135(A)Installation) or SA10956SC (PT6A- 28 Installation) are prerequisite forthis modification. It is the installer’s responsibility to ensure thesereferenced STC’s are EASA approved prior to instal 10036469 BLACKHAWK MODIFICATIONS Inc. FAA SA02357LA CESSNA 208B Replacement of the original P&W PT6A- 1. AeroAcoustics Aircraft Systems, Inc., 114(A) engine and propellerwith P&W PT6A-42A and 4-blade Hartzell PropellerHC- E4N-3P/D9900(K) and associated equipment in accordance with FAA STCSA02357LA. "Aircraft Payload Extender STOLSystem", 10014731 BLOM COMPAGNIA GENERALE RIPRESE AER 10028772 BLOM COMPAGNIA GENERALE RIPRESE AER 10029675 BLOM COMPAGNIA GENERALE RIPRESE AER EASA.A.S.02913 CESSNA 172P CGR P001-00 "Structure & Exhaust System REIMS AVIATION CESSNA F-172 Modification for Camera Installation". If the STC holder agrees to permit other person to use this certificateto alter the STC SA01805SE (EASA STC No. 10029821) product, the holder shall give the other 12.09.2011 is required as part ofthis alteration.2. This person writtenevidence of that modification is not compatible with Cessna permission.Prior to installation of this Model 208B SerialNumber 208B1190, modification it must be determined 208B1216, and thatthe interrelationshi Applicable to S/N 172-7631 only. 04.06.2008 EASA.A.S.03636 PARTENAVIA P68 PARTENAVIA P68C 17.07.2009 PA 31-350 GPS Garmin 430 for IFR The installation of EASA approved modification Prior to installation of this modification it 12.04.2010 EASA.A.C.07903 isrequired. 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. 10015918 BLR AEROSPACE, L.L.C. EASA.IM.A.S.02051 REV.2 FAA STC SA01615SE BEECH 200, 200C BEECH 300, 300LW BEECH B200, 200C BEECH B200GT, B200CGT Installation of winglets and associated changes in wing and aileronstructures and related system changes on Raytheon Model 200 200C, B200,B200C, 300 and 300LW airplanes.Revision 1 adds models B200GT, B200CGT. 10029451 BLR AEROSPACE, L.L.C. REV. 1 FAA STC SA02054SE C90A, C90GT, C90GTI Installation of winglets and associated changes Eligible Serial Numbers are defined in BLR in wing and aileronstructures and related system changes on Hawker Beechcraft Model C90A.C90GT and C90GTi. 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 Master Drawing List, DocumentReference BLR KA90W-002, rev. J, dated March 02, 2010, or later approvedrevisions.Structural life limit of the wing structure as expressed in flight hoursare reduced to, 15,590 hours b Prior to installation of this modification the 18.05.2010 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. 04/01/2013 Page 116/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10038758 BLR AEROSPACE, L.L.C. FAA STC SA02131SE KING AIR B200GT AND Installation of a BLR Aerospace Ultimate Approval of this change in type design applies Performance Enhancement Package 22.03.2012 B200CGT Performance Package (UPP). to the above listedaircraft models only. This requires the installation of thefollowing approval should not be extended to Supplemental Type Certificates otheraircraft of this model series unless the (STC):STC Number installer determines that therelationship ,,DescriptionSA01615SE,,BLR between this change and any other previ Aerospace Winglet Installation (STC refEASA.IM.A.S.02051)SA3366NM,,Rais beck Ram Air Recovery System (RARS) 10039059 BLR AEROSPACE, L.L.C. REV. 2 FAA STC SR01865SE 1- BELL 212 2- BELL 204B, BELL 205A1 10040783 BLR AEROSPACE, L.L.C. FAA SR00798SE / LBA RC 1163 1- 204B, 205A-1 2- 212, 412, 412EP 10017218 BOGGI S.R.L. EASA.R.S.01375 EUROCOPTER FRANCE AS 365N3 Installation of Dual Tailboom Strakes and Day/Night VFR only, flight into known icing FastFin.Revision 1 adds Model 204B and conditions prohibited. changes the reference to LBA STC RC 1163to EASA STC 10040783.Revision 2 adds additional Bell 212 and 412 FMSs. Installation of Dual Tailboom Strakes. This STC Day/Night VFR only, flight into known icing revises and supersedesLBA STC RC 1163 to conditions prohibited. add the Bell Helicopter Textron Inc. Model 204B, 412and 412EP. The AB 212 is removed as it is not included in the FAA STC. KIT MDS365-P001-00, Additional seat fitting for Eurocopter AS365N3 Helicopter in Hems configuration. 10033945 BOGGI S.R.L. AS 365 N3 Kit P/N MDS365-P002-00 ,External rear view mirror. Limited to AS 365N3 S/N 6609 and 6356, previously modified by the kit Bucher P/N ARA- AS365N2-AC50. - as defined in -Boggi s.r.l. Rotorcraft Flight Manual Supplement,Owner Manual,section 4, Edition 2,Rev. 0 dtd 12/01/2011 10035798 BOGGI S.R.L. AS365N3 Installation of Draeger TI 500 "Globetrotter" Limited to:-Incubator model Draeger TI 500 incubator on AS 365N3(ref. Change 365-M003- P/N TI 500, S/N 002-Helicopter model 00). AS365N3 S/N 6609 & 6356 10015497 BOMBARDIER AEROSPACE EASA.IM.A.S.01260 REV. 1 TCCA STC C-LSA05-294/D CHALLENGER CL-600-2B16 Aircraft Completion 9 Passenger Interior Configuration. (ASN 5595) 10015564 BOMBARDIER AEROSPACE EASA.IM.A.S.01463 C-LSA05-181/D, ISSUE 2 BOMBARDIER BD-100-1A10 Installation of Equipment Ladder (Aft (CHALLE Equipment Bay) in accordance with MDL380801, rev. 1 dated 11 June 2005 and compliance report BAS68380004 10015565 BOMBARDIER AEROSPACE EASA.IM.A.S.01464 C-LSA05-212/D, ISSUE 1 BOMBARDIER BD-100-1A10 (CHALLE Installation of a Satellite Telephone System Interfaced to an existing Flight Telephone System in accordance with MDL BAS68010010 Revision A dated 30 May 2005 and Compliance Report BAS68380005 dated Must be installed in conjunction with FAA 19.11.2012 STC SR00798SE (EASA STC10040783).Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair wi Prior to installation of this modification it 26.07.2012 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. The approval holder shall fulfil the obligations of Part 21, Paragraph21A.118A. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or 04.12.2007 21.02.2011 repa Prior to installation of this modification it 19.07.2011 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. Restricted to Aircraft Serial Number 5595 04.04.2006 1. Limited to: S/N 200132. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the install 1. This STC is limited to BD-100-1A10 (Challenger 300) SN 20013 10015567 BOMBARDIER AEROSPACE EASA.IM.A.S.01474 REV 1 TCCA STC C-LSA06-015/D ISSUE 2 BOMBARDIER CL-600-2B16 10/09/2005 Aircraft Completion Restricted to ASN 5605 27.09.2006 10015603 BOMBARDIER AEROSPACE EASA.IM.A.S.01539 TCCA STC C-LSA05-314/D BOMBARDIER CL-600-2B16 Aircraft Completion 11 PassengerInterior 1. Restricted to Aircraft Serial Number 28.11.2005 Configuration 5599.2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall b 10015674 BOMBARDIER AEROSPACE EASA.IM.A.S.01654 REV 1 TCCA STC C-LSA06-025/D BOMBARDIER CL-600-2B16 Aircraft Completion, 10 Passenger Interior. 1. Restricted to ASN 5613.2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the insta 26.10.2006 04/01/2013 Page 117/462 23.09.2005 05.10.2005
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04/01/2013 Page 1/462 - EASA

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