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 10016392 DUNCAN AVIATION, INC. EASA.IM.A.S.02721 FAA STC ST00914WI-D LOCKHEED 1011-385-1 Installation of Dual IS&S Air Data/ Altimeter approval may be extended to aircraft models 26.05.2008 System along with two inch standby pneumatic Lockheed 1329-23, previously modified iaw altimeter (FAA STC ST00914WI-D). FAA STC SA2326SW, when this STC has been EASAvalidated.Lockheed 1329-25 Group Approval for RVSM requirements can be shown in conjunction with FAA STC ST01082SE (AeroMech 10016393 DUNCAN AVIATION, Inc. EASA.IM.A.S.02722 FAA STC ST01059WI LOCKHEED 1011-385-1 Installation of Honeywell MK VII Enhanced This Design Approval may be extended to Ground Proximity Warning System (EGPWS). Airplanes Model Lockheed 13-29-23, FAA STC ST01059WI. previously modified iaw FAA STC SA2326SW, when validatedby EASA.Prior to installation of this modification the installer must determine that the interrelationship between this modif 10026867 DUNCAN AVIATION, INC. P- EASA.IM.A.S.03211 10028927 DUNCAN AVIATION, INC. P- EASA.IM.A.S.03046 FAA STC ST00703WI CESSNA 650 Installation of an AlliedSignal Enhanced Ground According to associated technical Proximity Warning System(EGPWS) documentation, FAA STC, AFMS and ICA FAA STC ST01409WI-D MYSTERE FALCON MF900 EASA Validation of FAA STC ST01409WI- Validation limited to Basic Mystere Falcon DInstallation of an L3 Communications, GH- 3100 Electronic StandbyInstrument System (ESIS) in accordance with Duncan Aviation Inc MasterDocument List No 06062208, Revision C, dated February 19th, 2008or later revisions a MF900 aircraft model 10040935 DUNCAN AVIATION, INC. FAA STC ST00600CH-D MF 900 & F900EX EASA validation of FAA STC ST00600CH-D As per FAA STC ST00600CH-D issue dated issue dated 12 Sept 2008Installation of Honeywell Enhanced Ground Proximity Warning System withWindshear Detection and optional Terrain Display (S/W level -218- 218)and optional Runway Advisory Awareness System (RAAS) 12 Sept 2008 10028837 DUNLOP AIRCRAFT TYRES LIMITED P-EASA.A.S.03864 REV. 1 EMBRAER ERJ 190-100 ECJ EMBRAER ERJ 190-100IGW EMBRAER ERJ 190-100LR EMBRAER ERJ 190-100STD EMBRAER ERJ 190-200IGW EMBRAER ERJ 190-200LR EMBRAER ERJ 190-200STD 10038094 DUNLOP AIRCRAFT TYRES LIMITED 0010014209-001 TCCA STC SA02-29 CL-600-2B19 Installation, Dunlop Aircraft Tyres Ltd P/N DR27921T Main and DR15112TNose Gear Tyres This STC is issued in order to reflect the transfer of ownership fromACS-NAI Ltd to Dunlop Aircraft Tyres Ltd. This STC has previously been validated in the following Eur 10039387 DUNLOP AIRCRAFT TYRES LIMITED ATR 42-200/-300/-320/-400/-500 Installation of Dunlop Aircraft Tyres on ATR 42 seriesThe STC installs Dunlop Aircraft Tyres Ltd P/N DZ33012T (Main LandingGear) and P/N DR15520T (Nose Landing Gear). 10041486 DUNLOP AIRCRAFT TYRES LIMITED ERJ 170-100 LR, ERJ 170-100 STD, ERJ 170-200 LR, ERJ 170-200 STD. Dunlop Aircraft Tyres Limited P/N DZ32816T Radial Nose Landing Gearinstallation on ERJ 170. Different nose landing gear part number tires may not be intermixed onthe same axle. 13.10.2008 Prior to installation of this modification it 18.08.2009 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. Prior to installation of this modification it 19.02.2010 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. Prior to installation of this modification it 06.08.2012 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. 29.06.2009 Prior to installation of this modification it 18.01.2012 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. 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. 02.05.2012 It is not allowable to mix different tyre types (radial and bias) in thenose landing gear leg. Prior to installation of this modification it 20.09.2012 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 190/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10030818 DYN'AVIATION DR300/108, DR300/180R, MD09F0001 050210 - New flaps and control None None 08.07.2010 DR300/120, DR400/120, DR300/140, DR300/125, DR340, DR315, DR360, DR380, DR400/100, DR400RP, DR400NGL, DR400/120A, DR400/160D, DR400/120D, DR400/180S, DR400/125, DR400/140, DR400/125I, DR400/140B, DR400/160, DR400/180, DR400/180R, DR400/2+2, DR400/200R, DR400/500 system 10031522 E & B HELICOPTERS LTD. TCCA STC SH07-38 407 Audio Alert System 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. 27.08.2010 10013998 E A D AEROSPACE EASA.A.S.01035 BEECH 1900C, AIRLINER BEECH 1900D ELS/EHS mode S installation on B1900 series. The Airplane Flight Manual Supplement DC107- 0886-00B or later approved revisions must be used with this modification. 10013999 E A D AEROSPACE EASA.A.S.01036 BOEING 737 Installation of a Honeywell EGPWS Mark V. 14.06.2005 10014000 E A D AEROSPACE EASA.A.S.01037 BEECH 1900 Installation of a Traffic Alert and Collision Avoidance System, model Hoenywell CAS- 67A TCASII installation on B1900 Series. 10014124 E A D AEROSPACE EASA.A.S.01234 AIRBUS A300-600 Modification of ELT ADT406 AF on AIRBUS A310 A300/A310Installation of ELT ADT 406 AF 10014314 E A D AEROSPACE EASA.A.S.01562 REV. 1 FAIRCHILD SWEARINGEN SA 227 SE 10014315 E A D AEROSPACE EASA.A.S.01563 AEROSPATIALE ATR 42-300 SERIES 10014749 E.I.S. AIRCRAFT GMBH EASA.A.S.02934 CESSNA 525 CESSNA 525A 10014931 E.I.S. AIRCRAFT GMBH EASA.A.S.03185 BEECH C90 A BEECH C90KING AIR All wiring required for TCAS II activation must be installed.ATC Mode S Transponders must be installed. Installation of TCAS II on SA 227 series This STC is approved only for the product aircraftTCAS II installation in accordance with configuration as defined in the approved design EAD Supplemental Type Design Definition data referred to in the paragraph "Description". Document 01043-EAS-A-STD-01 rev. A :• Compatibility with other aircraft/engine Removal of existing TCAS and associated tray configurations shall be determined by the in forward avionics• Installation of TCAS II installer. Installation of a calibration antenna in accordance with 01050-EAS-A-MDL. Avionic Upgrade TO DUAL GTX 330D and installation of SAT-COM Antenna. Avionics Upgrade to Garmin GTX330D diversity Mode S Transponder. 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 10015148 E.I.S. AIRCRAFT GMBH EASA.A.S.03508 BOEING 737-700 Cabin reconfiguration. Applicable for B737-700 MSN 28609. 15.04.2008 10015187 E.I.S. AIRCRAFT GMBH EASA.A.S.03571 SOCATA TBM 700 Avionics Upgrade to Garmin GTX330D Prior to installation of this modification the 14.08.2008 diversity Mode S Transponder. 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 10015188 E.I.S. AIRCRAFT GMBH EASA.A.S.03572 BEECH C90 A BEECH C90KING AIR Installation of dual Rockwell/Collins TDR 94D diversity mode-s transponder. 10013951 E.I.S.A. EASA.A.S.00439 REV 1 CESSNA 551 Installation of two Rockwell / Collins TDR 94D instead of two TDR 90 according to FDM EISA 05FDM F055 rev. 4 dated November 2004 and associated documents.New transponder location 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 1. Compatibility of this modification with other previously approved modifications must be determined by the installer.2. Applicability Cessna 551 S/N 551-0133 and S/N CE551- 0174.3. EASA approved Airplane Flight Manual Supplement, dated 23 November 2004 is 04/01/2013 Page 191/462 12.04.2005 18.07.2005 28.07.2005 03.04.2006 21.04.2006 23.01.2007 21.08.2007 19.12.2008 30.10.2006
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04/01/2013 Page 1/462 - EASA

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