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 10016686 HEAD BALLOONS, INC. EASA.IM.BA.S.01000 SL2263SO HEAD BALLOONS AX7-77 Installatiopn of Aerostar (Raven) Models CW The following Aerostar burners are approved 13.04.2007 HEAD BALLOONS AX7-77B and RW baskets. for usewith the above Head envelope / HEAD BALLOONS AX8-105 Aerostar basket configuration:Rally HP burner HEAD BALLOONS AX8-88 PN 13180HP II Dual burner PN 17395HP II HEAD BALLOONS AX8-88B Single burner PN 17398Rally HP II burner PN HEAD BALLOONS AX9-118 17399HP III Dual burner part number 52350HP 10016687 HEAD BALLOONS, INC. EASA.IM.BA.S.01001 FAA STC SB00463AT HEAD BALLOONS AX7-77 HEAD BALLOONS AX7-77B HEAD BALLOONS AX8-105 HEAD BALLOONS AX8-88 HEAD BALLOONS AX8-88B HEAD BALLOONS AX9-118 10015546 HEADS UP TECHNOLOGIES, Inc. EASA.IM.A.S.01437 FAA STC SA00558DE-D DORNIER 328-100 DORNIER D328-100 MSN 3061 Installation of Cameron Balloons Ltd. baskets and burners underneath Head Balloons, Inc. envelopes Installation of a Pilot and Co-Pilot Digital Air Data Unit 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. Airplane Flight Manual Supplement:AFMS Document 34-07-0002-00, Revision IR, dated 19 August 2004 or Document 34-07-0026-00, Revision IR or later approved revision isrequired on board for the IS&S ADDU installation,or AFMS Document 34-07-0002-01, Revisio 10015476 HEATH TECNA, INC. EASA.IM.A.S.01229 FAA STC ST01532SE B747-400 Cabin Interior Reconfiguration 1. 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. 10015574 HEATH TECNA, INC. EASA.IM.A.S.01484 FAA STC ST00636SE BOEING 737-300 BOEING 737-400 BOEING 737-500 Installation of ATIX Interior retrofit Kit according to FAA STC ST00636SE 10016255 HEATH TECNA, INC. EASA.IM.A.S.02533 FAA STC ST01780SE B747-400 Installation of interior components in accordance with Heath Tecna Inc. Drawing List HPD-DL-105 10016256 HEATH TECNA, INC. EASA.IM.A.S.02534 FAA STC ST008700SE B737-330 Installation of galley supports structure and jumper wire provisions in accordance with Health Tecna Drawing List HPD-DL-76, Revision B, dated 16, January 2004 or later approved revision. 10016601 HEATH TECNA, INC. EASA.IM.A.S.03015 FAA STC ST01154SE B747-200B Installation of interior components in accordance with Britax Heath Tecna Inc. (BHT) Drawing List HPD-DL-81 Revision B, dated December 12, 2002 or later FAA approved revisions 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. Modification of the aircraft per Boeing Service Bulletin 747-00-2004, conversion from passenger to freighter configuration must be performed concurrently with this STC. Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this c 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 installa 10028538 HEATH TECNA, INC. EASA.IM.A.S.03263 FAA STC ST01061SE 27.07.2009 10030956 HEATH TECNA, INC. FAA STC ST02067SE B747-400 LCD Monitor installation on Boeing Model 747- None The Supplemental Instructions for 16.07.2010 400 series aircraft inaccordance with Heath Continued Airworthiness, Heath Tecna, Inc. Master Drawing List HPD-DL- TecnaDocument HTM957, Revision A, 136,Revision E, dated May 5, 2010, or later dated March 1, 2010, or later FAA- FAA approved revisions.Validation of FAA STC acceptedrevision must be incorporated ST02067SE into the operator's maintenance program. 10030973 HEATH TECNA, INC. FAA STC ST02066SE B747-400 Seat Installation and interior reconfiguration on Boeing Model 747-400series aircraft in accordance with Heath Tecna, Inc. Master Drawing ListHPD-DL-137, Revision B dated May 11, 2010, or later FAA approvedrevisions. Validation of FAA STC ST02066SE None The Supplemental Instructions for Continued Airworthiness, Heath TecnaDocument HTM960, Revision E, dated May 20, 2010, or later EASA approvedrevision must be incorporated into the operator's maintenance program.Concurrent installation of Rockwell Collins S 04/01/2013 Page 268/462 19.11.2008 15.08.2005 30.05.2005 01.09.2005 29.08.2007 24.10.2007 16.03.2009 19.07.2010
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10035106 HEATH TECNA, INC. FAA STC ST02072SE A330-201, A330-202, A330-203 Installation of New J Class Crew Rest for none Prior to installation of this modification it 26.05.2011 A330-223, A330-243 Qantas Airlines A330-200seriesThis STC must be determined thatthe installs a removable crew rest curtain and interrelationship between this modification curtain header and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10039535 HEATH TECNA, INC. FAA ST02227SE 747-400 Installation of 2 new avionics racks in the EE Approval of this change applies to Boeing 747- Instructions for Continued Airworthiness bay of a Boeing 747-400series aircraft in 400 aircraft listed inHPD-DL-162 Rev.A, dated Heath Tecna Inc. Doc HTM accordance with Heath Tecna Inc. Master Data April 12, 2012 or later approved revisions only 1004,Revision B, dated April 4, 2012 ListHPD-DL-162 Rev. A, dated April 12, 2012 must be incorporated into the or later approved revision. operatorsmaintenance program. Prior to installation of this modification it must be determined thatthe interrelationship be 10014040 HEATHTECNA EASA.A.S.01114 B767-300 SERIES Introduction of Stowage 4B and infill panel to British Airways aircraft as defined in the modification definition document and Declaration of Design and Performance (DDP) 10014078 HEATHTECNA EASA.A.S.01170 B747-400 Reconfiguration of Cabin Interior from current 387SIA passenger cabin configuration (16F+58B+313Y for RT 514) to a 383 (12F+47B+324Y), Cathy Pacific Boing 747-400 fleet standard passenger cabin configuration. 10014143 HEATHTECNA EASA.A.S.01261 B747-400 SN 25127 & 25128 Heath Techna Modification C943 - Cathay Interiors Modification. 10014298 HEATHTECNA EASA.A.S.01542 B767-300 Business Class Footstool Assemblies on British Airways Boeing 767-300 As defined in DDP, Aircraft Serial MSN 26548. Zero Occupancy. For this modification to be accepted on an EU registered aircraft, requires the operator to confirm that all the associate FAA and Hong Kong CDA modifications have been EASA approved. 1. As defined in DDP Aircraft Serial Numbers 25172 & 25128.2. Zero Occupancy.3. For this modification to be accepted on an EU registered aircraft requires the operator to confirm that all the associated FAA &Hong King CAD modifications have been EASA appro This STC is limited to S/N 24340, 24341, 25204, 25444, 25442, 25732, 25826, 25828, 25829, 27140, 24335, 24336, 25831 and 10014519 HEATHTECNA EASA.A.S.02600 REV 1 B747-400 Cathay Pacific B747 Cabin Re-Configuration 25834. 1. Restricted to MSN 27132, MSN 27069 & 07.04.2008 REV 1 MSN 265522. Zero occupancy3. 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". Compat 10014998 HEATHTECNA EASA.A.S.03298 DC-9 SERIES Meridiana DC-9 Series Stow Bin Extension. Restricted to ASN 49247,49248, 49531, 49669, 49740, 49901, 49902, 49903, 53064, 49808, 53182, 49785, 49792, 49935, 49951, 49854, 53013. 20.11.2007 10016868 HELICOPTER TECHNOLOGY COMPANY EASA.IM.R.S.01244 FAA STC SR01282LA MD HELICOPTERS 369A Installation of a Tail Rotor Blade Assembly. N/A 15.03.2007 MD HELICOPTERS 369D MD HELICOPTERS 369E MD HELICOPTERS 369FF MD HELICOPTERS 369H MD HELICOPTERS 369HE MD HELICOPTERS 369HM MD HELICOPTERS 369HS (STC Classified as Basic by the FAA). 10015311 HELICOPTERES GUIMBAL EASA.E.S.01001 REV. 1 O-360-J2A Low Temperature Extension - STC None Prior to installation of this modification it 22.11.2010 EASA.E.S.01001 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 10039707 HELICOPTERS ITALIA S.R.L. UNIPERSON AS 365N2 Installation of Audio Voice Warning on Radar Altimeter Thales AHV-8(ref. Change HI-365-34- 01). 10.05.2012 11.02.2005 26.07.2005 24.08.2005 11.10.2005 Limited to S/N 6414 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. 18.05.2012 04/01/2013 Page 269/462
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04/01/2013 Page 1/462 - EASA

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