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 10014066 MACCARTHY AVIATION HOLDINGS Ltd. EASA.A.S.01153 BOEING 747-400 Modification of Cabin to Install Zone B Cabin 1. Compliance with the following Requirements 22.04.2005 Class Dividers, Zone B Stowage & Dogbox, has not been established.:1.1. Viewing of all Door 2 Port & Starboard Dividers & Upper apllicable placards & signage to in compliance Deck Dogbox. with FAR/JAR 25.791.1.2. Weight, centre of Gravity & Weight Distribution, to be in compliance with JAR25.1519.1.3. Co 10014966 MACCARTHY AVIATION HOLDINGS Ltd. EASA.A.S.03241 BOEING 757 Installation of Galley 1B and Forward RH Wardrobe. 10032016 MACCARTHY AVIATION HOLDINGS Ltd. REV. 1 A319-133 CJ Revision of EASA STC 10032016.Removal of the G1, G2 & G5 galleys’ loads established on initial issueof EASA STC 10032016 date of issue 01.10.2010 granted to MacCarthyInteriors Ltd . 10039505 MACH TECHNICAL DESIGN S.L. BELL 412 Surveillance Camera Installation according to MDL-FAA-0110 Rev. B(The modification consists in the installation of a camera to captureimages and the associated equipment to process and send them to a groundstation.) 10013933 MADELEC AERO - F9503 EASA.A.S.00318 REV 2 FOKKER F.28 MARK 0070 Installation of photoluminescent Floor Proximity Emergency Escape Path Marking system 10013949 MADELEC AERO - F9503 EASA.A.S.00426 REV 3 AIRBUS A319-320-321 Replacement of the powered floor proximity emergency escape path marking system by a FPEEPM photoluminescent system 04.12.2007 Approval limited to MSN4114. 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 25.10.2010 The installation of this STC is compatible with the installation of theTCCA STC SH96-57 (LBA STC RC.1182): Installation of Heli- Access StepsP/N D205-0633-011 in accordance with Dart Aerospace Ltd. DrawingIIN-D205-633, Rev A.Prior to installation of this m 1. Photoluminescent system charge time: 10 minutes.2. Photoluminescent Tape life time: 8 years.3. MSN 11290-11296-11323-113294. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "De 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 10015268 MAP AIRCRAFT PART 21 AS EASA.A.S.03739 REV 1 BOEING 737-400 Auxiliary Fuel Tank Removal, B737-400. installer. 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. 10017123 MAP AIRCRAFT PART 21 AS EASA.R.S.01210 EUROCOPTER FRANCE AS Installation of Polycon wireless communication Service Bulletin Polycon SB-03 Issue B shall 332L2 system in AS332L2 helicopter be implemented before installing this STC 10014154 MARSHALL OF CAMBRIDGE AEROSPACE 10031215 MARSHALL OF CAMBRIDGE AEROSPACE 10031227 MARSHALL OF CAMBRIDGE AEROSPACE 10035677 MARSHALL OF CAMBRIDGE AEROSPACE EASA.A.S.01275 SOCATA MS 894A Marshall Aerospace Modification MA 1665. Radio Equipment Upgrade. 26.07.2005 A340-300 Structural Installation of 2 IFF Antennae none This STC only approves the antenna installation from a structural pointof view. Flight dynamic, electrical and functional aspects have not beenconsidered.Prior to installation of this modification it must be determined thatthe interrelationship between thi 02.08.2010 08.05.2012 08.03.2006 31.03.2006 16.02.2009 04.12.2006 A340-300 Structural Installation of a V/UHF Antenna none This STC only approves the antenna installation from a structural pointof view. Flight dynamic, electrical and functional aspects have not beenconsidered.Prior to installation of this modification it must be determined thatthe interrelationship between thi 03.08.2010 REV. 1 A318 CFM Major Change to EASA STC10035677 "Installation of an Auxiliary FuelCentre Tank system on A318 Elite aircraft"This Major Change consists in removing the limitation concerning manualtransfer without pressurization above FL100. Restricted to A318 ELITE CFM aircraft only.This modification is not approved for installation on aircraft fittedwith a Flammability Reduction System Prior to installation of this modification it 08.12.2011 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 04/01/2013 Page 326/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10035729 MARSHALL OF CAMBRIDGE REV. 2 A340-313 Iberia Airways Interior Reconfiguration 1. This STC must be installed in conjunction Prior to installation of this modification it 16.07.2012 AEROSPACE with EASA STC No.EASA.A.S.00654. 2. This must be determined thatthe STC is limited to the aircraft MSN 125, 134, interrelationship between this modification 145, 146, 217, 221,and 329 and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10036381 MARSHALL OF CAMBRIDGE AEROSPACE 10040450 MARSHALL OF CAMBRIDGE AEROSPACE B737-700 737 Medevac Role Change 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. 06.09.2011 REV. 1 A340-312 This modification intends to:This modification will install Seat Electronics Boxes (SEB) (PanasoniceX2) on to modified existing Avio business class seats and will removeexisting Zone Terminators (ZT) (installed under Marshall ModificationMA1951).Modificati 10015787 MASS SYSTEMS, EASA.IM.A.S.01843 FAA STC ST01708LA SD3-30 SD3-60 SD3-SHERPA SD3-60 SHERPA 10015793 MASS SYSTEMS, EASA.IM.A.S.01852 FAA STC ST00952LA 1.AEROSPATIALE ATR 72-101 10.BOEING 757-200 SERIES 11.BOEING 767-200 SERIES 12.BOEING 777-200 13.BOEING DC-10-10 14.BOEING DC-9-81/82 15.LOCKHEED 1011-385-1 2.AIRBUS A300 MODEL B2-1A 3.AIRBUS A310-200 4.AIRBUS A310-300 5.AIRBUS A340-211 6.AIRBUS A340-212 7.BOEING 717-200 8.BOEING 737-200 SERIES 9.BOEING 747-400 SERIES AEROSPATIALE ATR 72-102 AEROSPATIALE ATR 72-201 AEROSPATIALE ATR 72-202 AEROSPATIALE ATR 72-212 AEROSPATIALE ATR 72-212A AIRBUS A300 MODEL B2-1C AIRBUS A300 MODEL B2-203 AIRBUS A300 MODEL B2K-3C AIRBUS A300 MODEL B4-600 AIRBUS A330-301 AIRBUS A340-311 AIRBUS A340-312 BOEING 767-300 SERIES BOEING 777-300 SERIES BOEING DC-9-83 (MD-83) BOEING DC-9-87 (MD-87) BOEING MD-88 BOEING MD-90 Installation of MASS Systems’ fire extinguisher, The approval of this change in type design P/N M57331-009, as a replacement for the applies to the above-noted airplane model. Graviner fire extinguisher, P/N 57331-009in the This approval should not be extended to above-noted airplane model. This fire otherspecific airplanes of these model series extinguisher is in accordance with MASS on which other than noted previously approved Systems’ Drawing No. M57331-009, “Fire E modifications are incorporated, unless Installation of MASS Systems fire extinguisher cartridges as replacement for Walter Kidde Aerospace fire extinguisher cartridge in fire extinguisher bottles 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. 25.10.2012 The approval of this change in type design applies to the airplane models noted on the FAA Approved Model ListA copy of thie STC must be included in the permanent records of the modified aircraft 04/01/2013 Page 327/462 16.04.2007 04.10.2006
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04/01/2013 Page 1/462 - EASA

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