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 10013970 E.I.S.A. EASA.A.S.00741 REV. 2 BEECH 200 Photo Conversion / based on existing STC No. 1 The application of this STC is limited to the 27.02.2009 EASA.A.S.00741r1 S/N BB221 and BB16072 Utilisation of Intercom prohibited in dense traffic areas3 Prior to installation of this modification the installer must determine that the interrelationship between this modifi 10014075 E.I.S.A. EASA.A.S.01167 REV 1 FALCON 10 Installation of a TCAS 4000 unit from Rockwell/CollinsInstallation of a TCAS 4000 unit from Rockwell/Collins 30.06.2006 10014530 E.I.S.A. EASA.A.S.02615 CESSNA 404 Installation of a video under Cessna 404 Applicable to Cessna 404 04.10.2006 10014643 E.I.S.A. EASA.A.S.02795 MYSTERE FALCON 20 Addition of Enhanced Surveillance Capacity on existing TDR 94 Mode S Transponder installation. Major Design Change applicable to aircraft Fan Jet Falcon and Falcon 20 equipped with:• Rockwell Collins Proline IV avionics suite.• Mode S Elementary Transponder TDR-94D- 008.• FMS-6000.• Air Data Computer ADC- 850C.• An Input/Output Concentr 10014736 E.I.S.A. EASA.A.S.02919 REV 1 CESSNA 525A Installation of SAT-COM Antenna 24.01.2007 10014786 E.I.S.A. EASA.A.S.02986 FALCON 50 ADDITION OF ENHANCED SURVEILLANCE This STC is approved only for those Mystere 29.05.2007 CAPACITY ON EXISTING ELEMENTARY Falcon 50 aircraft previously equipped to this MODE S TRANSPONDER INSTALLATION modification with:• Option 1: Rockwell Collins Proline IV, FMS FMC-6000 and Mode S Elementary Surveillance Installation with Transponder Rockwell Collins TDR 94D 10014908 E.I.S.A. EASA.A.S.03151 FALCON 10 MODE S TRANSPONDER WITH ENHANCED SURVEILLANCE CAPACITY 31.05.2007 10015021 E.I.S.A. EASA.A.S.03327 CESSNA 525B S134 - Maximum Takeoff/Landing Weight reduction. None 05.02.2008 10015364 E.J. MLYNARCZYK & CO. INC. EASA.IM.A.S.00679 REV. 1 FAA STC ST03078AT BOEING 747-400 Installation of a Panasonic Avionics 1. STC No ST01523SE must be 12.10.2005 Corporation System 3000 In-Flight accomplished concurrently with MAS10413-01 Entertainment System in accordance with and MAS10413-02 installations.2. This STC Master Drawing List MDL 10413, Rev. F dated is approved only for the product configuration 14 September 2005. Validation of FAA STC as defined in the approved designdata referred ST03078AT amended 22 September 2005. to in the paragraph "Description". Compatib 10015656 E.J. MLYNARCZYK & CO. INC. EASA.IM.A.S.01632 ST01519AT BOEING DC-9-82 (MD-82) BOEING DC-9-83 (MD-83) FAA STC ST01519ATInstallation of Dual Canadian Marconi Company CMA-900 Flight Management System 10039040 E4C AEROSPACE, Inc. REV. 1 FAA STC ST02110LA B767-300 Seat power, Seat Modifications and Seat track Installation 10013929 EAD AEROSPACE EASA.A.S.00265 REV. 1 BOEING 737-300, 737-400, BOEING 737-500 Compatibility of this design with previously approved modifications must be determined by 01.02.2008 31.07.2006 the installer. 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. 15.05.2012 Installation of Honeywell EGPWS Mark V 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. This STC is approved only for the product 10014201 EAD AEROSPACE EASA.A.S.01351 REV 1 SA 227 SERIES ELS/EHS installation on SA 227 series aircraft - Removal of existing two ATC transponders and configuration as defined in the approved design associated trays in forward avionics- Removal data referred to in the paragraph "Description". of existing ATC Mode S Control Panel from Compatibility with other aircraft/engine Instrument Panel- Disconnection of ATC 2 configurations shall be determined by the Mode S bottom antenna- Installati installer. 10014450 EAD AEROSPACE EASA.A.S.02503 B757 ELT antenna installation as provision only Maintenance Planning Document Supplement 01060-EAS-C-MPD-02, Revision A 10014637 EAD AEROSPACE EASA.A.S.02783 REV 1 BOEING 767 Installation of Panasonic "EFX" Passenger in Flight Entertainment System (IFE). This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraphs "Description" and “Associated Technical Documentation”. Compatibility with other aircraft/engine configurations shall be determined 04/01/2013 Page 192/462 02.02.2009 27.06.2006 10.03.2006 04.04.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014638 EAD AEROSPACE EASA.A.S.02784 BOEING 737-600 Implementation of Honeywell “Link 2000” Compatibility of this design change with other 09.03.2007 BOEING 737-700 Controller-Pilot Data Link Communications previously approved modifications must be BOEING 737-800 BOEING 737-900 (CPDLC) on B 737 determined by the installer. 10014664 EAD AEROSPACE EASA.A.S.02821 BOEING 757-200 SERIES Installation of Thales Integrated Standby Flight System 11.05.2007 10014679 EAD AEROSPACE EASA.A.S.02840 B767-300 Installation of Thales Integrated Standby Flight Display (ISFD) 05.03.2007 10015106 EAD AEROSPACE EASA.A.S.03449 A319 Installation of AMT-3800 High Gain Antenna on 1. Prior to installation of this modification the 17.11.2008 A319 Series Aircraft installer must determine that the interrelationship between this modificationand any other previously installed modification will introduce no adverse effect upon the airworthiness of the produc 10039303 EAD AEROSPACE REV. 1 B747-400 Installation of Cobham SATCOM antenna type HGA-7001 in accordance withAerotec Master Data List AE11110MDL Rev.1, dated 4 April 2012. 10040043 EAD AEROSPACE REV. 1 B747-400 Swift broadband Satcom installation in S/N: 30885, 32337, 32338, 32339, 32340, accordance with Aerotec ConceptMaster Data 28757, 29406 List AE11111MDL Rev 2, dated April 3, 2012 10015302 EAD AEROSPACE AIRWORTHINESS EASA.A.S.03866 REV. 3 A340 Installation of Advanced Mission Display System Phase A- AMDS/ARevision of the EASA STC EASA.A.S.03866 Revision 2 to remove EWISlimitation 10027343 EAD AEROSPACE AIRWORTHINESS P-EASA.A.S.03706 A330 Installation of Advanced Mission Display System - Phase A (AMDS/A) 10031354 EAD AEROSPACE AIRWORTHINESS REV. 1 A320 Installation of Advanced Mission Display System Phase A- AMDS/A on A320Series Aircraft Revision of the EASA STC 10031354 to remove EWIS limitation 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. 03.07.2012 None 06.07.2012 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 02.12.2010 None 1. Prior to installation of this modification 23.09.2009 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 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 29.11.2010 10036787 EAD AEROSPACE AIRWORTHINESS A320 SERIES Cabin Modification 174 to 168 PAX on A320 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 06.10.2011 10016076 EAD INC. EASA.IM.A.S.02260 FAA STC ST02267CH BOEING 747-400 EAD installed Honeywell Weight and Balance System (WBS) on B747-400 in accordance with EAD Master Data List 01021-FAA-A-MDL, rev. E, or later EASA-approved revision.This STC is a validation of FAA STC ST02267CH 10016545 EAD INC. EASA.IM.A.S.02924 FAA STC ST01481CH BOEING 737-400 SERIES TCAS/Mode-S Activation on Boeing 737-400 Series as approved under the STC FAA ST01481CH. 1. This on board weight and balance system is considered an advisory systeem and is not certified as the primary means of calculating the aircraft's weight and balance.2. EASA approved Airplane Flight Manual Supplement, EAD document 01021-FAA-A-AFM-01, Rev 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. 04/01/2013 Page 193/462 27.04.2007 02.10.2008
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04/01/2013 Page 1/462 - EASA

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