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 10015753 TRIAD INTERNATIONAL MAINTENANCE EASA.IM.A.S.01786 FAA STC ST03200AT BOEING 737-800 Complete interior reconfiguration in accordance with TIMCO Aviation Services, Inc MDL, report 04T101L500, revision “D”, dated December 08, 2005, or later EASA approved revision 20.07.2006 10029274 TRIUMPH INSTRUMENTS BURBANK Inc. EASA.IM.A.S.03255 REV. 1 FAA STC ST02236LA CL-600-2B19, CL-600-2C10 CL-600-2D15, CL-600-2D24 Triumph Replacement Hydraulic Accumulators. 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. 17.03.2010 10034472 TRIUMPH INSULATION SYSTEMS, L.L.C. REV. 1 FAA STC ST02013LA B767-200 Insulation Blanket Installation 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. 11.04.2011 10026913 TROLLTUNE CORPORATION P- EASA.IM.A.S.03179 FAA STC SA03608AT 182P AND 182Q (SEE ATTACHMENT) Increased Maximum Gross Takeoff Weight (MGTOW). This STC allows a 150 lbIncrease in MGTOW from 2950 to 3100 lbs. There is no change to themaximum landing weight of 2950 lbs. 10013953 TROYES AVIATION EASA.A.S.00493 REV. 2 CESSNA F177-RG Installation of sliding panel on the front left and right door windows amd rear right window.Addition of new S/N 087 F-BURU on None. 1. Prior to installation of this modification 21.08.2009 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 insta Limited to F177RG S/N 0112, 0065 and S/N 087 F-BURU. 10013954 TROYES AVIATION EASA.A.S.00494 REV. 3 CESSNA F177RG STC EASA.A.S.00493. Installation of a camera sight door under the Applicability F177RG S/N 0112, 0065, 103, The approval holder shall fulfil the 29.03.2010 fuselage.Addition of new aircraft to STC EASA.A.S.00494 Revision 2. 087 F-BURU and S/N 51 F-HBAG. obligations of Part 21,Paragraph21.A109. 10014266 TROYES AVIATION EASA.A.S.01495 REV. 3 REIMS CESSNA F177-RG Provisions for three attachments in the right Limited to: F177RG S/N 0112, 0065, 103, 153 1) Prior to installation of this modification 06.10.2009 side of the instrumentpanel in accordance with and 087 F-BURU; S/N 051D-EMEN the installer mustdetermine that the the STC EASA.A.S.01495R1: adjunction of a interrelationship between this modification newserial number "S/N 051" and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product. 2) The inst 10014285 TROYES AVIATION EASA.A.S.01522 CESSNA 340A FAM n° 47 - Limitation of MTOW to 2699 kg s/n 340A-0451 23.02.2006 10014642 TSA TRANSAIRCO S.A. EASA.A.S.02792 PILATUS PC-12 PILATUS PC-12/45 PILATUS PC-12/47 AFT Refreshment Galley and OvenRefer to master certification documents list TS PC12- 25.30.02MCL 10015718 TTF AEROSPACE, LLC EASA.IM.A.S.01716 FAA STC ST00231BO BOEING 737-800 Installation of Yokohama forward Lavatory E and Yokohama aft lavatory K and attendant seat in accordance with TTF Aerospace MDL TTF-05T026-01 Rev B, dated February 24, 2006 1. Limited to serial number 321 and later;2. Galley power and microwave oven use is not approved during take-off and landing phases of flight and during emergency or abnormal procedures;3. When aft refreshment galley is installed, the luggage area Limited to installation on Boeing 737-800 S/N 28325, 30470, 32277 and 32278 only.Installation of FAA STC 01533LA requiredInstruction for airworthiness 9ICA, TTF Aerospace Document TTF-05T026-18 revision new, dated February 13, 2006 or later FAA accepted re 10016453 TTF AEROSPACE, LLC EASA.IM.A.S.02799 FAA STC ST01195SE BOMBARDIER DHC-8-100 SERIES BOMBARDIER DHC-8-200 SERIES BOMBARDIER DHC-8-300 SERIES Installation of a Reinforced Flight Deck Door. 16.06.2008 10015250 TUIFLY GmbH EASA.A.S.03692 B737-800 Cabin Configuration Change to 52BC plus 6YC 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. 05.11.2008 04/01/2013 Page 452/462 28.02.2008 21.11.2006 06.04.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015258 TUIFLY GmbH EASA.A.S.03711 B737-700, B737-800 Installation of Water Boiler P/N: 66601-101- 1. Prior to installation of this modification the 15.04.2009 0001 as an alternative to Coffee Maker P/N: installer must determine that the 64753-001-003. interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. 10017090 TURBOMECA EASA.R.S.00753 REV. 2 AS350B, B1, BA, B2, B3 Installation of Sand Filter (Engine air inlet None. Prior to installation of this modification it 17.06.2010 EC130B4 protection)Notes: Revision 1 to this STC must be determined thatthe reflects:1. the transfer of EASA STC interrelationship between this modification EASA.R.S.00753 from CGTM to and any other previouslyinstalled Turbomeca;2. updates of the Associated modification and/ or repair will introduce Technical Documentation package no adverse effectupon the airworthiness followingDOA minor changes of the product. 10017287 TURBOMECA EASA.R.S.01536 DGAC FRANCE STC NO 84-SF-1122 EUROCOPTER FRANCE AS 350 B EUROCOPTER FRANCE AS 350 B1 EUROCOPTER FRANCE AS 350 B2 EUROCOPTER FRANCE AS 350 Installation of HESIS thermic camera system manufactured by SAGEM 1. Only Turbomeca personal or specifically trained mechanics are allowed to install fixed parts and components of the HESIS kit.2. Prior to installation of this modification the installer must determine that the interrelationship between this modificati 10016861 TYLER CAMERA SYSTEMS EASA.IM.R.S.01237 REV. 1 FAA STC SR01272LA BA R44, R44 II Installation of Tyler ROB-001 Universal Mount 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. 04.12.2007 10016594 U.S. TECHNICAL CONSULTANTS, INC. EASA.IM.A.S.03005 FAA STC ST02409CH-D DC-9-83 (MD-83) DC-9-87 (MD-87) FAA STC No. ST02409CH-D “NavAero t- BagC22 Electronic Flight Bag” 10029398 U.S. TECHNICAL CONSULTANTS, INC. FAA STC ST02161LA B757-200, B757-300 Installation of navAero t.BagC2 Electronic Flight Bag 10033897 U.S. TECHNICAL CONSULTANTS, INC. FAA STC ST02320LA B767-200, -300, -300F, -400ER Installation of Class 2 Electronic Flight Bag (EFB) provisions. 10014236 UNI AIR ENTREPRISE EASA.A.S.01399 CORVETTE SN 601 SN 028 & 008 10013932 UNI AIR ENTREPRISE SAS EASA.A.S.00305 REV. 1 CITATION 550 - Installation of Digital Data Recorder SSUFDR Allied Signal (TSO-C124) in accordance with Master Data List No. UAE.011.02 Issue0 dated 16 August 2004, or later EASA approved Revision.- Installation of a Digital Flight Data Recorder.Note: 10014004 UNI AIR ENTREPRISE SAS EASA.A.S.01041 BEECH C90A Revision 1 Installation of a Concorde RG-380E Sealed Lead Acid Battery. 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 installa 05.01.2009 16.01.2009 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. 23.03.2010 Any equipment that is connected to the Prior to installation of this modification it 17.02.2011 electrical power provisionscertified by this STC must be determined thatthe must be tested in accordance with interrelationship between this modification therequirementsof navAero Inc.’s Electrical and and any other previouslyinstalled EnvironmentalSubstantiation for Lithium based modification and/ or repair will introduce battery in navAero t-bag C22 EFB SystemD no adverse effectupon the airworthiness of the product. Deviation to SB 34-12 replacement of mount 1. This STC applies to MSN 028 and MSN 008 C24-C25 in accordance with MDL UAE 008.05 only.2. This STC is approved only for the Rev. 1 dated 8/07/2005. Installation of product configuration as defined in the horizontal mount between frames C24 and approved design data referred to in the C26 instead of vertical one between frames paragraph "Description". Compatibility with C24 and C25. other aircraft/engine configurations shall be 1. AFM Supplement UAE No. 46 Revision 0 dated 16 August 2004 or later EASA approved revision is a required part of this STC.2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph 1. Supplemental Airplane Fight Manual No UAE/52 (French language) must be used with this modification.2. Modification limited to Beechcraft C90A s/n LJ-1361.3. This STC is approved only for the product configuration as defined in the approved design data r 04/01/2013 Page 453/462 25.07.2005 06.02.2009 11.04.2005
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04/01/2013 Page 1/462 - EASA

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