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 10015375 ACSS, AVIATION COMMUNICATION EASA.IM.A.S.01045 FAA STC ST01583LA BOEING 737-300 Installation of ACSS T2CAS System according 1. According to limitations section in FAA STC 17.08.2005 AND BOEING 737-400 to FAA STC ST01583LA dated 20th January ST01583LA dated 20th January 2004.2. This 2004.- ACSS Index of Master Data Lists, STC is approved only for the product Document No. 8900034, Revision "A" dated configuration as defined in the approved design 3rd September 2004, or later FAA approved data referred to in the paragraph "Description". revision- ACSS Airplane Flight Manual Supplement, Compatibility with other aircraft 10015406 ACSS, AVIATION COMMUNICATION EASA.IM.A.S.01117 FAA STC ST01702LA BOEING 747-200 Installation of ACSS T2CAS 1. in accordance with Approval Report 01.08.2005 AND BOEING 747-300 DL/LVT/05.5325422. T2CAS Airplane Flight Manual Supplement (AFMS), ACSS document number 8003638-001 revision A, approved by the FAA on May 25, 20053. This STC is approved only for the product configuration as defined i 10015573 ACSS, AVIATION COMMUNICATION EASA.IM.A.S.01480 FAA STC SA4839NM BOEING 757-200 Installation and activation of TCAS and the XS- 07.11.2005 AND 950 Mode S Transponder (including ELS/EHS). 10015650 ACSS, AVIATION COMMUNICATION EASA.IM.A.S.01625 FAA STC SA5061NM DC-9-81 (MD-81) Installation of Honeywell Traffic Alert & 30.01.2006 AND DC-9-82 (MD-82) DC-9-83 (MD-83) DC-9-87 (MD-87) MD-88 Collision Avoidance System (TCAS II) 10015651 ACSS, AVIATION COMMUNICATION EASA.IM.A.S.01626 FAA STC SA5541NM BOEING 767-200 Installation of Honeywell Traffic Alert & 1. TCAS Airplane Flight Manual Supplement 12.12.2005 AND BOEING 767-300 Collision Avoidance System (TCAS) (Change 7) TCAS-APPS-0294, Rev A.2. 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/engin 10015731 ACSS, AVIATION COMMUNICATION AND 10015838 ACSS, AVIATION COMMUNICATION AND 10031364 ACSS, AVIATION COMMUNICATION AND 10032094 ACSS, AVIATION COMMUNICATION AND 10042297 ACSS, AVIATION COMMUNICATION AND 10042553 ACSS, AVIATION COMMUNICATION AND EASA.IM.A.S.01753 - AIRBUS A320-200 Installation of Honeywell TCAS II system 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. EASA.IM.A.S.01932 FAA STC SA4882NM BOEING 747-100 BOEING 747-100B SUD BOEING 747-200B BOEING 747-200C BOEING 747-200F BOEING 747-300 BOEING 747-400 BOEING 747-SP BOEING 747-SR Installation of a Honeywell Traffic Alert and Collision Avoidance System (TCAS II) in accordance with FAA approved Honywell Master Data List number ML4071598 FAA approved Flight Manual Supplement required for this configuration is listed on the appropriate approved Honeywell and ACSS Master Index List. FAA STC ST01911LA B747-400 Installation of ACSS Mode S Transponder with See Limitation Section of FAA approved ACSS None 11.08.2010 ELS/EHS capability toreplace Mode S Transponder in existing ACSS Traffic Alert and CollisionAvoidance system TCAS II in accordance with FAA approval ACSS MasterData List Document No. 8900019-001, Revision B, dat Master Data List No. 8900019 FAA STC NO. ST00411LA B747-400 Installation of Honeywell Traffic Alert and Collision Avoidance System(TCASII) EASA.IM.A.S.01059 FAA ST01646LA ATR 42/72 ALL MODELS Installation of ACSS T2CAS in accordance with FAA Approved ACSS Index ofMaster Data List for installation of TCAS II and TAWS, Document No8900038, rev. B, dd. August 2004, or later FAA approved revision and inaccordance with ACSS Summary of Data Submittals EASA.IM.A.S.01044 REV. 1 FAA STC SA5530NM B737-100/200/300/400/500 FAA STC SA5530NM validation - Installation of the ACSS TCAS II Systemwith Change 7.1 software 25.11.2005 31.07.2006 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. 07.10.2010 1- This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer. This certificate shall None. Prior to installation of this STC it must be determined that theinterrelationship between this modification and any other previouslyinstalled modification and / or repair will introduce no adverse effectupon the airworthiness of the product. 04/01/2013 Page 6/462 21.06.2005 14.12.2012
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10042711 ACSS, AVIATION COMMUNICATION FAA STC ST02406LA SEE EASA APPROVED MODEL Installation of Traffic Alert and Collision none Section 1.2.2.3 of Installation Instruction, 14.12.2012 AND LIST Avoidance Systems (TCAS II)version 7.1 ref. doc. 8008571-001, Rev.G, is not applicable to this EASA STC. It is replaced by:Confirm the existing ACSS TCAS Change 7.0 system was approved by EASAPrior to installation of this modification it must be dete 10033485 ADAC LUFTFAHRT TECHNIK GmbH EC135P2 (CPDS), EC135 P2+, EC135T2 (CPDS), EC135 T2+ 10035671 ADAC LUFTFAHRT TECHNIK GmbH EC135 T1(CDS) EC135 T1(CPDS) EC135 T2(CPDS) EC135 T2+ EC135 P1(CDS) EC135 P1(CPDS) EC135 P2(CPDS) EC135 P2+ 10036349 ADAC LUFTFAHRT TECHNIK GmbH EC135 P2(CPDS), EC135 P2+ EC135 T2(CPDS), EC135 T2+ Installation of Dual Garmin GNS 430W into EC 135 with MEGHAS cockpitInstallation of two GNS430W linked with indication on the FCDSas definedin the Master Drawing List EC135-01 066-005-LIN and based on ALT MajorChange EC135-01066. Installation of fixed Landing Lights on the forward crosstube. Installation of a second fixed landing light on the forward cross tubeas defined in the MDL EC135-01072-001-LMD and based on ALT changeproject EC135- 01072. 10039230 ADAC LUFTFAHRT TECHNIK GmbH BK117 C-2 NVIS Certification of mission equipment on an Eurocopter BK117 C2 10028594 ADVANCED AVIONICS TECHNOLOGIES P- EASA.IM.A.S.03223 10028595 ADVANCED AVIONICS TECHNOLOGIES P- EASA.IM.A.S.03220 10028911 ADVANCED AVIONICS TECHNOLOGIES P- EASA.IM.A.S.03222 10029263 ADVANCED AVIONICS TECHNOLOGIES P- EASA.IM.A.S.03221 REV. 1 FAA STC ST09365SC DHC-8-201, DHC-8-202 Installation of dual Collins Mode S TranspondersFAA STC ST09365SC, IR, August 14, 1997 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 25.01.2011 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. 08.07.2011 Installation of a NVIS lighting system into an None. -,,The first installation of this kit must be Eurocopter EC135(MEGHAS).Installation of a supervised by the STCholder. -,,This NVIS lighting system into an Eurocopter EC135 rotorcraft employs Night Vision Imaging withMEGHAS cockpit as defined in the MDL System lighting,commonly named NVIS EC135-01065-001-LMD, based on ALTchange lighting, that has been certified to ensure project EC135-01065. theaircraft is compatible with night vision goggles ( Required pre-modification EASA approval 10038241 (ECD major change 2237) The first installation of this kit must be supervised by the STC holder. This rotorcraft employs Night Vision Imaging System lighting, commonlynamed NVIS lighting, that has been certified to ensure the aircraft iscompatible with night vision goggles (NVG). 02.09.2011 19.04.2012 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. 19.07.2011 REV. 2 FAA STC ST09326SC DHC-8-201, DHC-8-202 Installation of Dual Universal Navigation UNS- None Prior to installation of this modification it 20.07.2011 1C Flight ManagementSystemFAA STC must be determined thatthe ST09326SC, Rev. 1, dated 14 November 2000 interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. REV. 2 FAA STC ST09347SC DHC-8-201, DHC-8-202 DHC-8-401, DHC-8-402 Installation of Coltech ATSCALL SystemFAA STC ST09347SC, Rev. 1, dated May 08, 2001. 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. 20.07.2011 REV. 2 FAA STC ST09346SC DHC-8-201, DHC-8-202 Installation of Honeywell Traffic Alert and none Prior to installation of this modification it 20.07.2011 Collision Avoidance System,TCAS IIFAA STC must be determined thatthe ST09326SC, Rev.1, dated 14 November 2000. interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 04/01/2013 Page 7/462
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04/01/2013 Page 1/462 - EASA

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