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 10016913 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01294 FAA STC SR02131NY-D SIKORSKY S-76A Installation of Keystone Helicopter Corporation Prior to installation of this modification the 26.07.2007 SIKORSKY S-76B Deluxe VIP Interior. installer must determine that the SIKORSKY S-76C interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10016914 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01295 FAA STC SR02130NY-D SIKORSKY S-76A SIKORSKY S-76B SIKORSKY S-76C 10016915 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01296 FAA STC SR02123NY-D SIKORSKY S-76A SIKORSKY S-76B SIKORSKY S-76C 10016916 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01297 FAA STC SR02122NY-D SIKORSKY S-76A SIKORSKY S-76B SIKORSKY S-76C Installation of Garmin GMX 200 Multi Function Display. This STC has been classified as "BASIC" by the FAA and has been approved under the PTVP. The flight manual has been reviewed and is acceptable. Installation of Provisions for a EuroAvionics EuroNav IV System. STC SR02123NY-D classified as Basic by the FAA through FAA Order 8110.52. Installation of High Intensity Strobe Lights. STC Classified as Basic by FAA. 10016946 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01340 FAA STC SR01976NY-D SIKORSKY S-92A Installation of Keystone Helicopter Auxiliary Gauges and Relocation of Fill Ports for the Low Float Pressure Warning System. 10016981 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01384 FAA STC SR02417NY-D SIKORSKY S-76A SIKORSKY S-76B SIKORSKY S-76C 10016982 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01386 REVISION 1 10016983 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01387 FAA STC SR02426NY-D SIKORSKY S-76A SIKORSKY S-76B SIKORSKY S-76C Installation of Honeywell KHF 1050 HF Communication System. FAA STC SR02152NY-D SIKORSKY S-92A Installation of a Cockpit Pressure Refuelling Control in a Sikorsky S-92A. This STC has been classified as "BASIC" by the FAA and has been approved under the PTVP. Installation of a Replacement Concorde Lead Acid Battery. 10016997 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01406 REV. 1 FAA STC02436NY-D SIKORSKY S-92A Installation of a High Intensity Strobe Lights. This STC has been classified as BASIC by the FAA and has been approved under the PTVP. 10017018 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01436 REV. 1 FAA STC SR01949NY-D EUROCOPTER FRANCE AS 365N1 EUROCOPTER FRANCE AS 365N2 EUROCOPTER FRANCE AS 365N3 Installation of a Honeywell Chadwick Model 15175 VXP System. 10017040 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01464 FAA STC SR02435NY-D SIKORSKY S-92A Installation of a Rockwell Collins SAR-126 Direction Finder System. This STC has been classified as “BASIC” by the FAA and has beenapproved under the PTVP. The FAA has not certified, and EASA has not validated, the equipment for which these provisions are intended. Additional approvals are required to install this equipment. The equipment installation must be evaluated to ensure that it complies with the appl 03.07.2007 19.03.2007 15.03.2007 29.06.2007 Refer to FAA STC SR02417NY-D. 04.12.2007 none 1. Prior to installation of this modification the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product;2. The 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 10017070 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01506 FAA STC SR02577NY-D SIKORSKY S-76C Keystone Helicopters STC SR02577NY-D; 1. Prior to installation of this modification the Introduction of a cockpit digital video recorder installer must determine that the system to meet JAR-OPS 3 flight data interrelationship between this modification and recorder requirements on applicable Sikorsky S-any other previously installed modification will 76C series aircraft. introduce no adverse effect upon the airworthiness of the product. The i 10017076 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01519 FAA STC SR02573NY-D SIKORSKY S-92A Installation of Main Rotor Blade Recognition 1. Prior to installation of this modification the Lights. 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.2. 10017083 SIKORSKY GLOBAL HELICOPTERS Inc. EASA.IM.R.S.01550 FAA STC SR02208NY-D SIKORSKY S-92A Installation of lavatory. 1. 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.2. 04/01/2013 Page 406/462 09.11.2007 05.02.2008 19.03.2008 29.06.2011 10.07.2008 19.02.2009 02.12.2008 30.04.2009
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10029325 SILVERHAWK CONVERSIONS P- FAA STC SA10741SC BEECHCRAFT KING AIR Installation of Pratt and Whitney Canada PT6A - None Prior to installation of this modification the 18.03.2010 EASA.IM.A.S.02962 C90, E90, C90A AIRCRAFT 135A Engines. 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 10015331 SIMMONDS PRECISION PRODUCTS, EASA.IM.A.S.00345 FAA STC ST00089BO BOEING 727-200 SERIES Installation of either the Goodrich Corporation 1. The suppression feature of Fire Detection 30.11.2004 INC Fire Detection and Suppression system, or the and Suppression system has been certified for Fire Detection only system in accordance with a maximum of 60 minutes from the activation Goodrich Corporation Master Drawing List of the suppression agent. Aircraft diversion T3008-MDL-0101, Revision A, dated October time, including landing, should not exceed 60 31, 2003 or later FAA-approved re minutes.2. This STC is 10015770 SIMMONDS PRECISION PRODUCTS, INC 10016158 SIMMONDS PRECISION PRODUCTS, INC 10016338 SIMMONDS PRECISION PRODUCTS, INC EASA.IM.A.S.01809 FAA STC ST00043BO BOEING 737-100 BOEING 737-200 BOEING 737-300 BOEING 737-400 BOEING 737-500 EASA.IM.A.S.02377 FAA STC ST00235BO BOEING 737-400 Installation of the Goodrich Corporation Fire Detection (Class “E”) EASA.IM.A.S.02647 FAA STC ST00092BO AIRBUS A300 In-Tank Fuel Quantity Indicating System (FAA 10016713 SIMPLEX MANUFACTURING CO. EASA.IM.R.S.0078 FAA STC SR00684SE, DGAC SPAIN EUROCOPTER FRANCE AS 350 B EUROCOPTER FRANCE AS 350 B1 EUROCOPTER FRANCE AS 350 B2 EUROCOPTER FRANCE AS 350 B3 EUROCOPTER FRANCE AS 350 10017066 SIMPLEX MANUFACTURING CO. EASA.IM.R.S.01502 FAA STC SR00889SE EUROCOPTER FRANCE AS 355 SERIE BA Installation of a Simmonds Precission 50203 Compatibility of this design change with other series Fuel Quantity Harness in accordance previously approved modifications must be with Simmonds Precision Installation Document determined by the installer. N0 E-3203, dated May 24, 1995, or later approved revision STC ST00092BO validation). This STC installs, within the aircraft fuel tanks, a new FQIS sensors and the associated wire harnesses. Installation of Simplex anti-fire system Model 310-900, 310-1100 and 310-1200 Installation of an agricultural spray system. (This STC has been classified as “BASIC” by the FAA in accordance with FAA Order 8110.52 and has been approved using the PTVP Procedures.) 1. The installation of this equipment is only applicable on 737-400 aircraft modified to full freighter configuration per Pemco STCnumbers SA2968SO, SA2969SO, SA2970SO and SA2971SO inclusively.2. Goodrich Corporation Airplane Flight Manual Supplement T3078 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 1. 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 installer. Rotorcraft to be equipped with an EASA approved high skid landing gear; Essential Crew only; Day/Night VFR only; and Airspeed Limitations per Flight Manual Supplement.Prior to installation of this modification the installer must determine that the 10029552 SINGAPORE TECHNOLOGIES A320 Passenger Compartment Reconfiguration 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. 31.03.2010 10033242 SINGAPORE TECHNOLOGIES A321 Passenger Compartment Reconfiguration 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 06.01.2011 10036609 SINGAPORE TECHNOLOGIES A320-200 SERIES Ural Airlines' A320 Cabin Reconfiguration -,,This design change on Aircraft model Airbus A320-200 is applicable tothe following aircraft serial numbers (MSNs): 203; 220; 735; 1152; 1484;1777; 2175; 2187 and 2327. This STC does not require a revision or supplement to the original TCHolder’s EWIS Instructions for Continued Airworthiness.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other p 04/01/2013 Page 407/462 22.01.2007 07.05.2007 02.10.2008 06.10.2004 26.09.2008 22.09.2011
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04/01/2013 Page 1/462 - EASA

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