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 10026943 DECRANE AEROSPACE PATS P- B737-800 Installation of Auxiliary Fuel System in the None. - Prior to installation of this modification 26.08.2009 AIRCRAFT, EASA.IM.A.S.03257 forward and aft cargocompartments.Validation the installer mustdetermine that the of STC ST01713NY-D as amended June 29, interrelationship between this modification 2009 and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product.- The install 10027297 DECRANE AEROSPACE PATS AIRCRAFT, 10027298 DECRANE AEROSPACE PATS AIRCRAFT, 10027299 DECRANE AEROSPACE PATS AIRCRAFT, 10028092 DECRANE AEROSPACE PATS AIRCRAFT, 10028093 DECRANE AEROSPACE PATS AIRCRAFT, EASA.IM.A.S.03026 REV. 3 FAA STC ST01727NY-D ERJ 190-100ECJ Major Change to FAA STC ST01727NY-D: Project DAS-GED-P072 / ODA-GED-001- Installation of Executive Interior (A/C #4) EASA.IM.A.S.03027 REV. 1 FAA STC ST01728NY-D ERJ 190-100ECJ Major Change to FAA STC ST01728NY-D: DAS-GED-P067 - Modification of theClass C Forward Cargo Compartment EASA.IM.A.S.03028 REV. 1 FAA STC ST01729NY-D ERJ 190-100ECJ ST01729NY-D: Installation of a Passenger Gaseous Oxygen Supply System 10015980 DEL-AIR EASA.IM.A.S.02132 FAA STC SA5733SW CESSNA 150 CESSNA 150A CESSNA 150B CESSNA 150C CESSNA 150D CESSNA 150E CESSNA 150F CESSNA 150G CESSNA 150H CESSNA 150L CESSNA 150M CESSNA 152 CESSNA A152 FAA STC ST00405LA-D 737-700 IGW Alteration of Fire Protection Systems, Lower Cargo Compartments. This STC revises and supersedes LBA STC LBA.21NE1.TA0682. The revisionwas issued to reflect the transfer from Hollingshead International toDecrane Aerospace PATS Aircraft. FAA STC ST01184LA B737-800 Alteration of Fire Protection Systems, Lower Cargo Compartments. This STC revises and supersedes LBA STC LBA.21NE1.TA0511. The revisionwas issued to reflect the transfer from Hollingshead International toDecrane Aerospace PATS Aircraft. Configuration 1: - Concurrent installation of STC ST01728NY-D (Class "C" CargoCompartment) iaw. Master Drawing List 6071-0000-MDL Rev. IR dtd.7.October 2008 is required. -Commercial operation under EASA rules requires installation of PATS SBST0172NY-D-25-S Configuration 1: - Concurrent installation of STC ST01727NY-D (Installation of anExecutive Interior) iaw. Master Drawing List 5950-0000-MDL revision Gdtd. 16.April 2009 is required Configuration 2: - Concurrent installation of STC ST01727NY-D (Installation Not Applicable 26.03.2010 Not Applicable 18.09.2009 - Concurrent installation of STC's ST01727NY- Not Applicable D (Installation of anExecutive Interior) and ST01728NY-D (Class "C" Cargo Compartment) isrequired - For aircraft under FAA jurisdiction this modification may not beinstalled after 30.August 2010 unless:(1) previ 18.09.2009 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.The ins 18.11.2009 Installation of Longe Range Wing Fuel Tanks 1. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.2. This STC is approved only for the product configuration as defined in the app 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.The ins 18.11.2009 04/01/2013 Page 182/462 14.08.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015984 DEL-AIR EASA.IM.A.S.02136 FAA STC SA01388SE CESSNA 170A Installation of a 7 Gallon extended range tank in This STC is approved only for the product 18.09.2006 CESSNA 170B each wing. configuration as defined in the approved design CESSNA 172 data referred to in the paragraph "Description". CESSNA 172A Compatibility with other aircraft/engine CESSNA 172B configurations shall be determined by the CESSNA 172C CESSNA 172D CESSNA 172E CESSNA 172F CESSNA 172G CESSNA 172H CESSNA 172I CESSNA 172J CESSNA 172K CESSNA 172L CESSNA 172M CESSNA 172N CESSNA 172P installer. 10015503 DELASTEK AERONAUTIQUE INC. EASA.IM.A.S.01266 TCCA STC SA04-116 ISSUE 1 BOMBARDIER CL-600-2B19 Installation of Delastek Bleed Lead Monitoring For s/n 7003 through 7212 Bombardier Service 23.07.2007 (SERIES System p/n DK-329-001. Bulletin 601R-30-022 Part C must be integrated prior to the installation. 10015800 DELTA AIR LINES, INC EASA.IM.A.S.01864 SA3305SO BOEING 767-200 Installation of a Delta modified forward trunnion bearing housing & a Delta manufactured bearing retainer bolt to allow forced lubrication of the respective joints. 01.06.2006 10015363 DELTA ENGINEERING CORPORATION EASA.IM.A.S.00677 REV. 1 FAA STC ST01523SE BOEING 747-400 1. Configuration 1:Installation of Interior 1. The approval holder shall fulfill the 09.09.2008 Components in accordance with Delta obligations of Part 21, Paragraph 21 .Al 09;2. Engineering Master Data List 0107-05983- Configuration 1:- This STC must be installed 2128, Revision A, dated March 26, 2007 or concurrent with Jamco America ST01455SE, later DAS approved;2. Configuration EJM Aerospace Services ST03078AT, STG 2:Installation of Interior Components in accordance Aerospace ST02993AT and Boeing Serv 10015393 DELTA ENGINEERING CORPORATION EASA.IM.A.S.01094 REV. 2 FAA STC ST01507SE BOEING 747-400 Description of Design Change:Installation of 1.This STC is approved only for the product 01.11.2007 Interior Equipment:1.ConfigurationInstallation of configuration as defined in the approved design interior components in accordance with Health data referred to in the paragraph "Description". Tecna, Inc. Drawing List HPD-DL-55, Rev. BF, Compatibility with other aircraft/engine dated February 11, 2005 or later approved configurations shall be determined by the revision.2.ConfigurationMod installer.2.Configuration 1:TThi 10015421 DELTA ENGINEERING CORPORATION EASA.IM.A.S.01151 FAA STC ST01895NY DC-9-87 (MD-87) MD-88 10015443 DELTA ENGINEERING CORPORATION EASA.IM.A.S.01183 FAA STC ST01310NY AEROSPATIALE ATR 42-200 AEROSPATIALE ATR 42-300 AEROSPATIALE ATR 42-320 AEROSPATIALE ATR 42-500 AEROSPATIALE ATR 72-101 AEROSPATIALE ATR 72-102 AEROSPATIALE ATR 72-201 AEROSPATIALE ATR 72-202 AEROSPATIALE ATR 72-211 AEROSPATIALE ATR 72-212 AEROSPATIALE ATR 72-212A Validation of FAA STC No ST01895NY.Replacement of Dual Transponders with ACSS 7517800-10005 ATDL Transponders with ELS and Gobles G7490-58 Control Head. Configuration 1: Installation of Delta Engineering sensors, brackets and wiring harnesses in accordance with Delta Engineering Master Drawing List 0101-04808- 2030 revision F dated August 5, 2004Configuration 2: Installation of the SFIM Inc. Auxiliary Fligh 1. This installation does not include EHS or ADS-B functionality.The Delta Engineering MMS No 0758-05312-2076 dated 19 April 2004 is required. 1. Configuration 1; this approval is for structural provisions only2. Configuration1 is required for Configuration 23.This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". 10016039 DELTA ENGINEERING CORPORATION EASA.IM.A.S.02208 REV. 1 FAA STC ST02223NY-D BOEING 767-200 Heath Tecna NuLook Interior 17.09.2007 10016094 DELTA ENGINEERING CORPORATION EASA.IM.A.S.02283 FAA STC ST02227NY-D AIRBUS A340-300 Panasonic Aviation Corporation System 3000i ¿ Delta Engineering Instructions for 05.07.2007 IFE Installation /Installation of a Panasonic Continued Airworthiness, Ref. No. 0752-05945- Avionics Corporation System 3000i In- 2135 Revision A, dated March 8th 2007.¿ FlightPassenger Entertainment System with Delta Engineering Airplane Flight Manual Astronics Empower ® In-Seat PowerSupply Supplement, Ref. No. 0652-06023-2135, System in accordance with Delta Engineering dated June 21st 2007.¿ Cabin configuration Mas mus 10016134 DELTA ENGINEERING CORPORATION EASA.IM.A.S.02330 FAA ST01767NY BOEING 747-200 Update of seat components for System 2000E This STC is approved only for the product per DAS project DAS-2056-03 on a B747-400. configuration as defined in the approved design data. Compatibilitty with other aircraft/engine configuraitons shall be determined by the installer. 25.03.2008 04/01/2013 Page 183/462 22.07.2005 30.05.2005
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04/01/2013 Page 1/462 - EASA

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