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 10034285 AVIONITEC Ltd. REV. 1 PA-46-310P Avionics Retrofit Removed Equipment: -,,Dual S/N: HB-PJW KX 165 NAV/COM System-,,WX 1000 Stormscope System-,,Argus 5000 Moving Map- ,,KMA 24 Audio Panel -,,PM 2000 Intercom New installed Equipment:-,,GNS 530W NAV/COM/GPS System #1-,,GNS 430W NAV/COM/GPS System #2-,, Not Applicable 25.03.2011 10034590 AVIONITEC Ltd. M20K Avionics RetrofitRemoved: ,,- King KX 165 S/N: 25-1170 HB-DHG The approval holder shall fulfill the 13.04.2011 NAV/COM with King KI 206 CDI,- King obligations of Part 21, KR 87 ADF with King KI 229 Indicator- Garmin Paragraph21.A109.Prior to installation of GNS530 NAV/COM/GPSInstalled: ,,- Garmin this modification it must be determined 530W NAV/COM/GPS- Garmin 430W thatthe interrelationship between this NAV/COM/GPS with GI 106A modification and any other IndicatorVertically guided RNAV previouslyinstalled modification and/ or repai 10037582 AVIONITEC Ltd. PA-28-236 IFR Avionics upgradeRemoved: - King KY S/N: 28-8011011 HB-PEN The approval holder shall fulfill the 08.12.2011 197A COM- King KMA 20Audio Panel- King obligations of Part 21, KN 53 NAV Receiver- King KI 203 NAV Paragraph21A.118A.Prior to installation Indicator- David Clark Isocom Intercom of this modification it must be determined Installed: - Garmin GNS530W GPS/COM/NAV thatthe interrelationship between this with GA35 antenna- Garmin GMA 347 Audio modification and any other Panel- King KR 87 ADF S previouslyinstalled modification and/ or repa 10038996 AVIONITEC Ltd. REV. 1 BEECH 35-C33A Upgrade Garmin GNS430, repl. S/N CE-39, F-BNOI The approval holder shall fulfil the 05.04.2012 NAV/COMRemoved:-Garmin GNS430 System- obligations of Part 21, King KX 155 NAV/COM system-King KR 85 Paragraph21.A118. Prior to installation of ADF SystemInstalled:-Dual Garmin GNS430W this modification it must be determined System-King KR 87 ADF System thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repai 10037702 AZRA LLC EASA.IM.A.S.0116 REV. 2 737-200, 737-200C, 737-300 Modification of Wing Inboard & Outboard Aft Scheduled inspections and repairs are required Prior to installation of this modification it 22.12.2011 737-400, 737-500 Trailing Edge Flaps Revision 2 of the STC with in accordance with thefollowing documents: 1. must be determined thatthe reference EASA.IM.A.S.0116 has been issued Chapter 05 of the "737-200, -200C Aircraft interrelationship between this modification asa result of its transfer from AeroTech Maintenance ManualSupplement”,Report No. and any other previouslyinstalled Services Inc (ATS) to AZRA LLCDBA ATS 52-0008, Issue 4, dated 6/30/05, for 737- modification and/or repair will introduce AeroTech Services. 200and -200C, with this STC modi no adverse effectupon the airworthiness of the product. 10014133 AZUR AERO ASSISTANCE EASA.A.S.01244 CESSNA 500, CITATION Installation of Radar RDR 2000 Bendix/King with radar screen KMD 540/850 Bndix/King in accordance with MDL AAA 08/2004 ed 1 Rev 1 dated 10/10/05 10014134 AZUR AERO ASSISTANCE EASA.A.S.01245 CESSNA 500, CITATION Installation of Mode S Transponder GTX 330 Garmin in accordance with MDL AAA 07/2004 Ed 1 Rev. 1 dated 10/10/2005 10014135 AZUR AERO ASSISTANCE EASA.A.S.01246 CESSNA 500, CITATION Installation of GPS GNS 430 GARMIN in accordance with MDL AAA 06/2004 Ed 1 Rev 1 dated 10/10/2005 10014136 AZUR AERO ASSISTANCE EASA.A.S.01247 CESSNA 500, CITATION Installation of GPS GNS 530 BRNAV GARMIN in accordance with MDL AAA 05/2004 Ed 1 Rev 1 dated 10/10/2005 10016328 B&B PARTNERS EASA.IM.A.S.02637 FAA STC ST03483AT Installation of a portable beverage dispensing system,P/N B43-FA 001 10016351 B&C SPECIALITY PRODUCTS EASA.IM.A.S.02671 FAA STC SA00846WI CESSNA 210L CESSNA 210M CESSNA 210N CESSNA P210N CESSNA T210L CESSNA T210M CESSNA T210N Addition of Vacuum Pump drive alternator and regulator with associated controls. 10033488 B/E AEROSPACE, INC. FAA STC ST14379LA-T 777-300, 777-300ER Installation of B/E Aerospace Pantry Air Chiller P/N 470-1 This STC is limited to MSN 308. 10.11.2005 This STC is limited to MSN 308. 10.11.2005 This STC is limited to MSN 308. 10.11.2005 This STC is limited to MSN 308 10.11.2005 1. This STC is applicable to the aircraft types as listed in the Approved Model List for FAA STC ST03483AT2. This STC is to be installed in accordance with the Galley Interface Criteria defined in Drawing No. 1178.3. The limitations as defined in Prior to installation of this modification the 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 06.02.2008 28.11.2007 Not Applicable 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. 25.01.2011 04/01/2013 Page 108/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10036542 B/E AEROSPACE, Inc. FAA STC ST02876CH B777-200, B777-200LR Installation of B/E Aerospace, Inc., Vacuum None Prior to installation of this modification it 19.09.2011 B777-300, B777-300ER Toilet Assembly Retrofit Kit must be determined thatthe B777F interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10036558 B/E AEROSPACE, Inc. FAA STC ST02876CH B737-600/700/800/900 Installation of Vacuum Toilet Assembly Retrofit Kit P/N 4100390-003. 10036659 B/E AEROSPACE, Inc. FAA STC ST02876CH B747-400 B747-400F Installation of Vacuum Toilet Assembly Retrofit Kit P/N 4100390-003Validation FAA STC ST02876CH. ,, 10040968 B/E AEROSPACE, Inc. FAA STC ST02876CH B767-200/-300/-300F/-400ER Installation of BE Aerospace Inc. Vacuum Toilet Assembly Retrofit Kit 10016917 BAE SYSTEMS AEROSPACE & DEFENSE EASA.IM.R.S.01302 REV. 1 FAA STC SR01906LA BK117 C-2 Installation of the Folding Utility Seat in Multiple- Place SeatArrangements. The Utility Seating System, as installed in the MBB BK117 C-2 helicopteris multiple-place utility seating system consiting of energy-absorbingUtility Installation of the Folding U 10015952 BARBARA AND ROBERT WILLIAMS EASA.IM.A.S.02094 SA572CE CESSNA 150 CESSNA 150A CESSNA 150B CESSNA 150C CESSNA 150D CESSNA 150E CESSNA 150F CESSNA 150G CESSNA 150H CESSNA 150J CESSNA 150K CESSNA 150L CESSNA 150M CESSNA A150K CESSNA A150L Replacement of Continental O-200A with Lycoming 150 or 160hp Model O-320 engines 10016380 BASIC AIRCRAFT PRODUCTS, INC. EASA.IM.A.S.02704 FAA STC ST00702AT CESSNA 210 Installation of Basic Type mBAE-14/28 Model 2025 Deployable Air Driven Alternator System 10016497 BASIC AIRCRAFT PRODUCTS, INC. EASA.IM.A.S.02859 FAA STC SA02747AT CESSNA 182 Stand-by Alternator – Installation of Basic Type BAE-14/28 Deployable Air Driven Alternator System. 10014838 BAYO S.A.S. EASA.A.S.03055 MOONEY M20K Modification of radio electric installation for B- RNAV capacity with AP/FD coupling. 10014903 BAYO S.A.S. EASA.A.S.03138 CESSNA P210N 53/2006 - IFR B-RNAV certification extension of the GNS530 already installed. 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. 19.09.2011 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. 27.09.2011 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. 09.08.2012 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. 14.12.2009 As defined in FAA STC SA572CEModified engine mounting structure and relocated battery installation must be inspected every 500 flight hours or annually, whichever occurs earlier for any cracking or corrosion and if found rectified with an EASA approved re This approval should not be extended to other aircraft of this moel on which other previously approved modifcations will produce noadverse effect upon the airworthiness of that aircrat. EASA approved Supplemental Airplane Flight Manual or EASA approved Air 20.09.2006 18.01.2008 As per FAA STC SA02747AT limitations. 29.08.2008 Modification limited to serial number 250508AFMS must be on board for any flight. STC Bayo 36/2006 must be already installed.The aricraft must be equipped with HSI KI525A and S-TEC 55X autopilot. 04/01/2013 Page 109/462 31.05.2007 21.01.2008
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04/01/2013 Page 1/462 - EASA

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