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 10016280 DELTA ENGINEERING CORPORATION EASA.IM.A.S.02572 FAA STC ST02393NY-D BOEING 747-400 Installation of Heath Tecna Cabin Interior 1. TGL 12 complied with.2. 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 airworth 09.10.2007 10016318 DELTA ENGINEERING CORPORATION EASA.IM.A.S.02624 REV. 1 FAA STC ST02404NY-D B767-300 Installation of Panasonic Avionics Overhead In- Flight EntertainmentSystem 10016329 DELTA ENGINEERING CORPORATION EASA.IM.A.S.02638 FAA STC ST02630NY BOEING 777-200 Heath Tecnica Interior 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 10016496 DELTA ENGINEERING CORPORATION EASA.IM.A.S.02858 FAA STC ST02403NY-D BOEING 747-400 Installation of Seat In-Flight Entertainment Components and Software update in accordance with Delta Engineering Master Data List 0107-06195-2172 Revision A, dated 4 April 2008. Validation of FAA STC ST02403NY-D. 10016540 DELTA ENGINEERING CORPORATION EASA.IM.A.S.02917 FAA STC ST02402NY-D AIRBUS A320 Panasonic IFE a eFXInstallation of Panasonic eFX systemEASA validation of FAA STC No. ST02402NY-D from 28. March 2008. Limited to installation on aircraft already fitted Prior to installation of this modification it 11.02.2011 with HeathTechnaNuLook interior must be determined thatthe (Configuration 4) ref EASA STC IM.A.S.02474 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 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 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.1 The ins 10016675 DELTA ENGINEERING CORPORATION EASA.IM.A.S.03182 FAA STC ST02215NY-D BOEING 747-400 SERIES Installation of Panasonic Avionics Corporation 1. Delta Engineering Instructions for Continued System 3000i In-Flight Entertainment System Airworthiness 0707-05814-2121 Rev. A dated in accordance with Delta Engineering Master Aug 31, 2006 are required with this installation. Data List 0107-05809-2121 Rev. A dated Nov. 2. The cabin configuration of the seats installed 15, 2006 or later approved revisionsValidation in accordance with KLM LOPA KLM3H112780 of FAA STC ST02215NY-D Revision ORG is required 10027744 DELTA ENGINEERING CORPORATION P- EASA.IM.A.S.03198 10027745 DELTA ENGINEERING CORPORATION P- EASA.IM.A.S.03199 10027746 DELTA ENGINEERING CORPORATION P- EASA.IM.A.S.03200 REV. 1 FAA STC ST02643NY-D A340-300 Update of a Panasonic System 2000E In-Flight PassengerEntertainment System to a System 2000E HybridMajor Change to the EASA STC 10027744 to remove EWIS limitation REV. 1 FAA STC ST02642NY-D A330-200 Update of a Panasonic System 2000E In-Flight PassengerEntertainment System to a System 2000E HybridMajor Change to the EASA STC 10027746 to remove EWIS limitation REV. 1 FAA STC ST02642NY-D A330-200 Update of a Panasonic System 2000E In-Flight PassengerEntertainment System to a System 2000E HybridMajor Change to the EASA STC 10027746 to remove EWIS limitation 15.12.2008 14.08.2008 16.07.2008 18.06.2009 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. 04.04.2012 The STC holder shall provide by 7th June 2010 Prior to installation of this modification the 04.04.2012 Instructions for ContinuedAirworthiness on installer must determinethat the Electrical Wiring Interconnection System - interrelationship between this modification EWIS ICA -in accordance with Special and any otherpreviously installed Condition H-01 "Enhanced modification will introduce no adverse AirworthinessProgramme for Aeroplane effect uponthe airworthiness of the Systems - ICA on EWIS". product.The installatio 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. 04.04.2012 10029011 DELTA ENGINEERING CORPORATION EASA.IM.A.S.03196 FAA STC ST01483NY BOEING 747-400 SERIES 23.07.2009 10029012 DELTA ENGINEERING CORPORATION EASA.IM.A.S.03197 FAA STC ST01519NY BOEING 747-400 SERIES 23.07.2009 10029013 DELTA ENGINEERING CORPORATION EASA.IM.A.S.03195 FAA STC ST01482NY BOEING 747-400 SERIES 21.07.2009 04/01/2013 Page 184/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10030011 DELTA ENGINEERING CORPORATION REV. 1 FAA STC ST02654NY-D B757-300 Installation of Panasonic Avionics Corporation Finnair Minor Modifications (EASA.21J.263) Prior to installation of this modification it 25.01.2011 System Digital MPES IIPassenger EO 15330FR 1 and EO 15383 Fmust be must be determined thatthe Entertainment System. installed prior to or concurrent with the interrelationship between this modification installation of thisSTC. and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product 10031836 DELTA ENGINEERING CORPORATION FAA STC ST02755NY A330-300 Update of a Panasonic System eX2 In-Flight Passenger EntertainmentSystem 10033290 DELTA ENGINEERING CORPORATION FAA STC ST01662NY B747-400 Modification of existing Mode S Transponders This approval is for the replacement of the & TCAS by installation ofHoneywell/ACSS P/N Transponder Units and TCAS.This approval 7517800-10004 ATDL Transponders & does not include the transponder and TCAS 4066010-910 TCAS inaccordance with Delta system, wiring,trays, antennas, structural Engineering Master Drawing List 0107-05185- 2059,Rev A, dated April 18,2003.Validation of FAA provisions, etc. 10033430 DELTA ENGINEERING CORPORATION FAA STC ST02647NY-D ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500, ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212, ATR 72-212 A EASA validation of FAA STC ST02647NY-D (as amended by FAA on August31st, 2010) regarding:Installation of Delta Engineering Synchro’s in accordance with DeltaEngineering Master Data List 0101-06413-2166 Revision A dated January13th, 2010 or later approved r Not applicable The Panasonic System eX2 must interface with the following listedrequired existing components/systems that are not approved by this STCand approved under the EASA STC "10031815" of Flight Structures Inc.:1. Cabin Configuration2. Structural Provisions for V 17.09.2010 Delta Engineering Maintenance Manual Supplement Doc. No.0707-05223-2059, dated February 12, 2003 is required for thismodification 11.01.2011 See those of original FAA STC ST02647NY-D. Prior to installation of this modification it 19.01.2011 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 10033596 DELTA ENGINEERING CORPORATION P- FAA STC ST00988NY-D BOEING 747-400 Installation of Matsushita Avionics Systems Maintenance Manual Supplement for 747-400 Prior to installation of this modification the 30.07.2009 EASA.IM.A.S.03098 Corporation 2000E with AVOD1.5 Cabin with Matsushita AvionicsSystems Corporation installer must determinethat the Entertainment System in accordance with 2000E Cabin Entertainment System, Delta interrelationship between this modification Delta Engineering,L.P. Master Drawing List EngineeringDoc. No. 707-04403-250, must be and any otherpreviously installed 107-04323-250, Revision C, dated Sept. 24, incorporated into the operator’smaintenance modification will introduce no adverse 1999or later FAA approved revisions.Validation instructions. effect uponthe airworthiness of the of product.The installatio 10036548 DELTA ENGINEERING CORPORATION REV. 1 FAA STC ST02668NY-D A330-301, -302, -303 Provision of a Panasonic Ex Phone This STC approval only certifies the provisions Prior to installation of this modification it 10.11.2011 A330-321, -322, -323 System(Validation of FAA STC ST02668NY- for the PanasoniceXPhone. This device must be determined thatthe A330-341, -342, -343 D)This STC installs provisions (antenna and activation, for which these provisions interrelationship between this modification wiring) for Panasonic eX phoneSystem. The areintended, will be certified separately. and any other previouslyinstalled Revision 1 of this STC corrects the applicability modification and/ or repair will introduce by adding twoaircraft models, omitted at the in no adverse effectupon the airworthiness of the product. 10037166 DELTA ENGINEERING CORPORATION A330-301, A330-302, A330-303 A330-321, A330-322, A330-323 A330-341, A330-342, A330-343 10037167 DELTA ENGINEERING CORPORATION REV. 1 FAA STC ST02884NY-D A330-201 / -202 / -203 A330-223 / -243 A330-301 / -302 / -303 A330-321 / -322 / -323 A330-341 / -342 / -343 Panasonic Global Communication System - System installationThis STC covers the installation of Panasonic Global CommunicationSystem (GCS) and activates the wireless portion. Panasonic Global Communication System - Antenna installation This STC installs a large antenna for the future use of Panasonic GlobalCommunication System (GCS), on A330- 300 aircraft models.Revision 1 of this STC extends the applicability to the A330-200air 10037970 DELTA ENGINEERING CORPORATION FAA STC ST02888NY-D 777-300ER STC ST02888NY-D: Activation of Panasonic nMAP's (Wi-Fi) None Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalledmodification and/ or repair will introduce no adverse effect upon theairworthiness of the product. 07.11.2011 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. 16.03.2012 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. 10.01.2012 04/01/2013 Page 185/462
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04/01/2013 Page 1/462 - EASA

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