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 10016659 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.03120 FAA STC ST02612CH AIRBUS A318-111 Installation of AD Aerospace Cockpit Door 1. Prior to installation of this modification the 29.04.2009 AIRBUS A318-112 Monitoring System installer must determine that the AIRBUS A318-121 interrelationship between this modificationand AIRBUS A318-122 any other previously installed modification AIRBUS A319-111 will introduce no adverse effect upon the AIRBUS A319-112 AIRBUS A319-113 AIRBUS A319-114 AIRBUS A319-115 AIRBUS A319-131 AIRBUS A319-132 AIRBUS A319-133 AIRBUS A320-111 AIRBUS A320-211 AIRBUS A320-212 AIRBUS A320-214 AIRBUS A320-231 AIRBUS A320-232 AIRBUS A320-233 AIRBUS A321-111 AIRBUS A321-112 AIRBUS A321-131 AIRBUS A321-211 AIRBUS A321-212 AIRBUS A321-213 AIRBUS A321-231 AIRBUS A321-232 airworthiness of the produc 10027156 ELECTRONIC CABLE SPECIALISTS, Inc. P- FAA STC ST00646CH L1011-385-1-15, L1011-385-3 Installation of a single or dual None - Airplane Flight Manual Supplement, 10.09.2009 EASA.IM.A.S.01665 L1011-385-1, L1011-385-1-14 Honeywell/Trimble HT900 GlobalNavigation document ECS-960150 shall be System, configurations 1, 2 or 3 in accordance usedonboard the modified aircraftwithElectronic Cable Speciatlists Master Data Aircraft Maintenance Manual List, ECS-960151, Rev. H datedJanuary 8, Supplement, document ECS-960169 1999 or later FAA approved revisions shall bepart of the Instructions for Validation Continued Airworthiness of the aircraft Prior to installat 10027270 ELECTRONIC CABLE SPECIALISTS, Inc. P- FAA STC ST02637CH 737-100, 737-200, 737-200C, Installation of ECS EZMount (TM) mechanical see limitations and conditions on STC FAA Prior to installation of this modification it 17.09.2009 EASA.IM.A.S.03122 737-300, 737-400, 737-500, mounting assemblies ST02637CH must be determined thatthe 737-600, 737-700, 737-800, interrelationship between this modification 737-900, 737-900ER and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10028835 ELECTRONIC CABLE SPECIALISTS, Inc. P- EASA.IM.A.S.03101 FAA STC ST02626CH A318111/-112/-121/-122 A319-111/-112/-113/-114/-115 A319-131/-132/-133 A320-111/-211/-212/-214/ A320-214/-231/-232/ A321-111/-112/-131/-211/-212 A321-213/-231/-232 10033501 ELECTRONIC CABLE SPECIALISTS, Inc. EASA.IM.A.S.03101 REV. 1 FAA STC ST02626CH A318-111, -112, -121, -122 A319-111, -112, -113, -114 A319-115, -131, -132, -133 A320-111, -211, -212, -214 A320-231, -232, -233 A321-111, -112, -131, -211 A321-212, -213, -231, -232 10033754 ELECTRONIC CABLE SPECIALISTS, Inc. P- EASA.IM.A.S.03248 ·,,Electronic Cable Specialists Master Data List, ref. doc. ECS-206919,Revision E, dated 9th September 2008 (*)·,,Airplane Flight Manual Supplement, ref. doc. ECS-206922, RevisionN/C, dated 29th September 2008 (*)·,,Instructions for Continued Airworthiness FAA STC ST02708CH MD-11 Installation of EZMount (TM) Tilt mechanical mounting assembly onsidewalls of cockpit in accordance with Electronic Cable SpecialistsMaster Data List ECS-207476 Rev. A, dated March 4, 2009, or later FAAapproved revisions.Validation of FAA STC ST02708CH 10039706 ELECTRONIC CABLE SPECIALISTS, Inc. FAA STC ST02923CH 737-600/-700/-800/-900/-900ER Validation of FAA STC ST02923CH: EFB Installation of ECS EZMountTMMechanical Mounting Assemblies None 1.,,Prior to installation of this modification 02.06.2009 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 ins Installation of an EZMount Tilt Mechanical Not Applicable Prior to installation of this modification it 26.01.2011 Mounting AssemblyRevision of the EASA STC must be determined thatthe EASA.IM.A.S.03101 to add Configuration 2 interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product AFM Supplement as listed in Appendix A of Electronic Cable SpecialistsMaster Data List ECS-207476, Rev. A, dated March 4, 2009 or later FAAapproved revision, is required on board the modified aircraftThe equipment for which these provisions are intended is Prior to installation of this modification the installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the 1) This approval constitutes approval for the product.The installatio Prior to installation of this STC it must be EZMountTM MechanicalMounting Assemblies determined that theinterrelationship only. The capability of any system attached to between this modification and any other theEZMountTM Mechanical Mounting previouslyinstalled modification and / or Assembly requires additional EASAapproval. repair will introduce no adverse 2) The maximum allowed weight of any device effectupon the airworthiness of the to product. 04/01/2013 Page 202/462 23.06.2009
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10040901 ELECTRONIC CABLE SPECIALISTS, Inc. FAA STC ST02907CH B747-400 Installation of ECS EZMount mechanical The equipment for which these provisions are AFM Supplement ECS 208936 for 02.08.2012 B747-400F mounting assemblies in accordancewith installed has not beencertified. Additional Boeing 747-400 series Aircraft Electronic Cable Specialists, Inc. Master Data approval is required for the installation of equippedwith ECS EZMount tilt is List ECS 209135,Revision H, dated November thisequipment and must be evaluated to assure required on board of the modified 29, 2011 or later approved revisionValidation of satisfactory compliance withapplicable aircraft.Prior to installation of this FAA STC ST02907CH airworthiness standards. modification it must be determined thatthe interrelationship between this modification an 10041328 ELECTRONIC CABLE SPECIALISTS, Inc. FAA STC ST02961CH B737-600/-700/-800/-900/-900ER Validation of FAA STC ST02961CH - None 1) Prior to installation of this STC it must 07.09.2012 Approved configurations are thefollowing:- be determined that theinterrelationship Configuration 1: Replacement of Honeywell between this STC and any other Weather Radar System RDR-4Bwith previously installedmodification and / or Honeywell Honeywell Weather Radar RDR- repair will introduce no adverse effect 4000,-Configuration 2: Software upon theairworthiness of the product. 2) upgrade to Honeywell WRS RDR-4 This STC is EASA 10042532 ELECTRONIC CABLE SPECIALISTS, Inc. FAA STC ST02992CH B737-600/-700/-800/-900/-900ER Validation of FAA STC ST02992CH - Installation of dual Electronic FlightBag (EFB) System Provisions. 10013942 ELECTRONIQUE MAINTENANCE AVIATION 10013968 ELECTRONIQUE MAINTENANCE AVIATION 10014112 ELECTRONIQUE MAINTENANCE AVIATION 10014251 ELECTRONIQUE MAINTENANCE AVIATION 10014341 ELECTRONIQUE MAINTENANCE AVIATION 10014747 ELECTRONIQUE MAINTENANCE AVIATION 10014812 ELECTRONIQUE MAINTENANCE AVIATION EASA.A.S.00378 REV. 1 FAIRCHILD SWEARINGEN SA 226-T( - Installation of VHF 8.33 KHz/VOR/ILS/GPS/STORMSCOPE/VHF 150 MHz/UHF/ICS Passengers according to E.M.A. Modification Approval Sheet (FAM) No EMA/03/002/SA226Serie/VHF.GPSBRNAV.S TORM.UHF dated 22 December 2003.- Installation of GARMIN GNS 530A, STORM 1) The aircraft operator must perform the instructions for continuedairworthiness and comply with the Airworthiness Limitation Items as perthe Instructions for Continued Airworthiness (ICA), ReferenceECS-209337, Revision G, dated 22 August 2012. 2) Additio 1. This modification is applicable only to SA 226 T(B) s/n T298 F-GLPT.2. EASA Approved Airplane Flight Manual Supplements "Supplément au manuel de vol GPS BRNAV" are required.3. This STC is approved only for the product configuration as defined i 1) Prior to installation of this STC it must be determined that theinterrelationship between this STC and any other previously installedmodification and / or repair will introduce no adverse effect upon theairworthiness of the product. 2) This STC is EASA EASA.A.S.00738 REV. 1 FAIRCHILD SWEARINGEN SA Installation of GPS BRNAV, EGPWS, TAS, 1. This STC is limited to MSN T312 F-GRNT2. 20.02.2006 226-T( Stormscope, Radar, MFD- Garmin GNS 530 This STC is approved only for the product VHF.NAV.GPS, Honeywell RDR 2000 Radar, configuration as defined in the approved design BF Goodrich WX 500 Stormscope and Avidyne data referred to in the paragraph "Description". EX 500 MDF installation- BF Goodrich Sky 899 Compatibility with other aircraft/engine TAS and Honeywell KGP 560 EGPWS provision configurations shall be determin EASA.A.S.01217 BEECH C90 Allied Signal KT73 ATC Mode S, Kannad This STC is limited to Beech C90 MSN LJ667 13.06.2005 BEECH E90 406AF ELT 406 and 2 IDC 570 altimeters installation. & Beech E90 MSN LW 278. EASA.A.S.01473 BEECH 200 406 MHz ELT installation Modification applicable on s/n BB616 and BB202 only. 05.08.2005 EASA.A.S.01601 FAIRCHILD SWEARINGEN SA ATC Mode S, ELT 406 MHz, Altimeter, Turn 30.01.2006 226-T( and Bank annunciator installation EASA.A.S.02930 FAIRCHILD SWEARINGEN SA Garmin GNS 530A VHF 8.33KHZ, Honeywell This STC is limited to the SA226 S/N T312 26.02.2007 226 KY 196B VHF 8.33 KHZ, BF Goodrich TAS SKY 899 Installation EASA.A.S.03019 Installation of Avionic Upgrade according EMA/07/001/SA226/VHF8.33-ATC-MFD-RDR 30.04.2007 10014834 ELECTRONIQUE MAINTENANCE EASA.A.S.03050 BEECH 200 Installation of Garmin GTX330D Mode S 21.04.2008 AVIATION Transponder. 10015045 ELECTRONIQUE MAINTENANCE EASA.A.S.03361 BEECH 200 Installation of new COM-NAV-GPS with AFM Supplement must be used when the 04.08.2008 AVIATION BRNAV capacity and coupled to AP. application is applied.Modification limited to sn BB616. 10017146 ELECTRONIQUE MAINTENANCE EASA.R.S.01249 EUROCOPTER FRANCE AS Installation of SAFE FLIGHT Power Line 27.02.2007 AVIATION 355E Detector p/n 7101-5, in accordance with EMA EUROCOPTER FRANCE AS STC file n° 06/001/AS355Serie/PLD revision 0, 355F dated January 2006, or later EASA approved EUROCOPTER FRANCE AS 355F1 EUROCOPTER FRANCE AS 355F2 EUROCOPTER FRANCE AS 355N revision. 10016097 ELISEN TECHNOLOGIES EASA.IM.A.S.02286 TCCA STC SA07-9 BOMBARDIER CL-600-2B19 Iridium Antenna Installation 31.05.2007 10016098 ELISEN TECHNOLOGIES EASA.IM.A.S.02287 TCCA STC SA07-3 BOMBARDIER CL-600-2B19 Aft Equipment Bay Steps 31.05.2007 10016099 ELISEN TECHNOLOGIES EASA.IM.A.S.02288 TCCA STC SA07-4 BOMBARDIER CL-600-2B19 Ladder Stowage 31.05.2007 10016100 ELISEN TECHNOLOGIES EASA.IM.A.S.02289 TCCA STC SA07-5 BOMBARDIER CL-600-2B19 Towbar Head Stowage 31.05.2007 10016101 ELISEN TECHNOLOGIES EASA.IM.A.S.02290 TCCA STC SA07-6 BOMBARDIER CL-600-2B19 Main wheel stowage 31.05.2007 10016168 ELISEN TECHNOLOGIES EASA.IM.A.S.02395 TCCA STC SA07-20 BOMBARDIER CL-600-2B19 Miscellaneous Storage Box, Project No. 29R2- 707 03.07.2007 04/01/2013 Page 203/462 06.12.2012 05.02.2009
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04/01/2013 Page 1/462 - EASA

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