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 10038867 CONCORDE BATTERY CORPORATION FAA STC 03930AT ATR 42-200 /-300 /-320 /-500 Installation of a Lead Acid BatteryThis STC None. Prior to installation of this modification it 20.03.2012 ATR 72-101 / -102 installs a Lead Acid battery in replacement of must be determined thatthe ATR 72-201 / -202 / -211 the existingNickel-Cadmium battery. interrelationship between this modification ATR 72-212 / -212A and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10040738 CONCORDE BATTERY CORPORATION FAA STC NO. SA01633WI EMB 500 Installation of Concorde RG-390E VRSLA Batteries in the Embraer 500 inaccordance with Concorde Battery Corporation Master Drawing List, DWGNo. 5-0359, Revision NC, dated August 25, 2010 or later FAA approvedrevisions. 10040781 CONCORDE BATTERY CORPORATION FAA STC ST01643WI DHC-8-102, -103, -106 DHC-8-201, -202 DHC-8-301, -311, -314, -315 10042099 CONCORDE BATTERY CORPORATION FAA STC SA01118WI SEE EASA APPROVED MODEL LIST Installation of Concorde RG-380E/44 (42AH) or RG-380E/60L (48AH) SeriesValve Regulated Sealed Lead-Acid (VRSLA) batteries as replacement of OEMbatteries.FAA STC ST01643WI Installation of the Concorde FLA or VRSLA RG series batteries in CessnaSingle Engine Airplanes listed on the attached Approved Model List (AML)in accordance with Concorde Battery Corporation, Master Drawing ListDwg. No. 5-0148, Revision A, dated August 16, 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. 24.07.2012 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. 26.07.2012 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. 08.11.2012 10014097 CONTOUR AEROSPACE LIMITED EASA.A.S.01195 REV 1 BOEING 767-300 SERIES Introduction G3 Wardrobe to British Airways aircraft as defined in the modification definition document and Declaration of Design and Performance (DDP) As defined in the DDP. 20.05.2005 10016274 CORPORATION LOGIC AIR Inc. EASA.IM.A.S.02560 REV 1 TC STC C-LSA07-205/D ISSUE 2 BOEING 767-300 Installation of In-Flight Entertainment System. 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 install 10016283 CORPORATION LOGIC AIR Inc. EASA.IM.A.S.02578 TCCA SA07-210/D ISSUE 1 BOEING 767-300 Installation of 270 Pax Interior Configuration. 02.11.2007 10016284 CORPORATION LOGIC AIR Inc. EASA.IM.A.S.02579 REV 1 TCCA STC SA07-12 ISSUE 2 BOEING 767 Tire pressure Indication System De-activation, Boeing 767-300. 10016285 CORPORATION LOGIC AIR Inc. EASA.IM.A.S.02580 TCCA STC C-LSA07-091/D BOEING 767-300 installation of Mode S ATC Transponder with Elementary and Enhanced Surveillance Modes. 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 install 10016290 CORPORATION LOGIC AIR Inc. EASA.IM.A.S.02585 C-LSA03-498/D BOEING 767-300 Changes to Altitude Callout Configuration, Honeywell Mark V EGPWS. 02.11.2007 10033973 CRANE AEROSPACE & ELECTRONICS FAA STC ST02316LA LEARJET 60 Installation of Tire Pressure Sensor FAA STC None Prior to installation of this modification it 23.02.2011 ST02316LA (Date of issuance: September 28, must be determined thatthe 2010) interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10014384 CRANFIELD AEROSPACE LTD EASA.A.S.01669 Installation of a Honeywell Global GNS-XLS 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. 20.02.2006 10027822 CRANFIELD AEROSPACE LTD P-EASA.A.S.03734 BAE JETSTREAM 3100 Installation of Satcom System None None 09.11.2009 04/01/2013 Page 158/462 10.04.2008 07.08.2008 02.11.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10037359 CRANFIELD AEROSPACE LTD CESSNA 421C Installation of Initial Role Change Equipment in S/N 421C-0218. This STC requires installation of System 22.11.2011 a Civil ContingencyAircraft - Cessna 421C as and Structural provisions asdefined in defined in Cranfield Aerospace Cranfield Aerospace document documentCAeM/Cessna/1327. CAeM/Cessna/1326. 10037360 CRANFIELD AEROSPACE LTD CESSNA 421C System and Structural Provisions for a Civil Contingency Aircraft -Cessna 421C as defined in Cranfield Aerospace document CAeM/Cessna/1326. S/N 421C-0218. None. 22.11.2011 10014485 CTT SYSTEMS AB EASA.A.S.02547 REV. 2 CAA NL STC SA0009NL BOEING 767-300 Replacement of Zonal Dryer related to EASA Instruction for the installationInstallation 14.04.2009 AD 2006-0140-E.The above reference EASA instructions II767-2 and II767B-2, latest AD required the de-activation of Zonal Drying issue.KLM MO 21-0476 and Martinair MO Systems installed via CAA NL STC SA 0009 76730MP-003.Instructions for operationNo NL due to the potential for combustion of specific Airplane Flight Manual Supplement is contaminants in the dryer unit. A new dryer neededPrior to installation of this modifica 10015267 CTT SYSTEMS AB EASA.A.S.03738 CAA NL STC SA 0003 NL BOEING MD 11 Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via CAA NL STC SA 0003 NL due to the potential for combustion of contaminants in the dryer unit. A new dryer Instruction for the installation:Installation instruction IIMD11, latest revision, Swissair Engineering Order 510440.Instructions for operation:Airplane Flight Manual Supplement, AFM-98-02, Rev. 0, dated 3-11-98 or latestrevision. Instructions for continue 10016071 CUB CRAFTERS INC. EASA.IM.A.S.02252 REV. 1 FAA STC SA00522SE PA-18-125, PA-18A, PA-18-135, Installation of Lycoming O-320-A2B, O-320- The compatibility of this modification with other 11.12.2006 PA-18A-135, PA-18-150, A2C, O-320-A2D, O-320-B2B, O-320-B2C, O- approved modifications has to be ensured by PA-18A-150 320-D2A, O-320-D2B and O-320-D3G engines the company installing the modification. with Sensenich M74DM-52 through -56 or 74DM6-0-52 through -56 propellers and assocaited hardware, i.a with FAA STC SA00522SE. Approved MTOM up to 794 kg. 10042813 CUSTOM FIBERGLASS MOLDING INC. FAA STC SA02391CH BEE DEE M-4, M-4 Installation of Custom Fiberglass Molding Skis, Installer must check availability of EASA- The installation of this modification by 19.12.2012 M-4-210, M-4-210C Model 3000, according toMaster Drawing List approval for one or morereferenced STC when third persons is subject towritten M-4-220, M-4-220C CFMI 3000-9, Rev D dated 04th April 2011 or airplane is modified per that / those STC(s). permission of the approval holder and M-4-220S, M-4-180V laterFAA approved revision.Installation of disposal of the approvedappropriate M-4C, M-4S, M-4T Custom Fiberglass Molding Skis, Model 3000- documentation. Prior to installation of this M-5-235C, M-5-180C, M-6-235 01(A/B),according to Master Drawin modification it must be determined M-7-235, M-7-235B MX-7-160, MX-7-180 MX-7-180A, MX-7-235 MX-7-180B, MX-7-180C thatthe interrelationship 10014718 CZECH AIRLINES TECHNICS A.S. EASA.A.S.02895 AIRBUS A320-214 Cabin layout modification from 156 pax to 162 pax with seat type change /Removal of the existing seats for 156 passengers and doghouses, installation of new seats for 162 passengers, new doghouses, relocation and addition of PSU’s as required, installation 19.03.2007 10037313 DAHER SOCATA A/S REV. 1 AS 355 F2 Modification STC.34.001.11Version A for VFR - Version A limited to VFR onlyVersion B: for Installation of GNS 430W for IFR-operation refer also to AS355 F2 RFM VHF1/NAV1/ILS1/GPS1,AN/ARC 210 for VHF2, BXP6401 for XPDR Mode S, Sky Connect for IridiumSat Phone, Motorola DM3600 for UHF FMVersion B for IFR - Installation of GNS 430W for VHF1/N Supplement 11.4"IFR Flight". 10026805 DANSK FLY ELEKTRONIK ApS P-EASA.A.S.03944 BEECH 1900D Installation of Skytrac ISAT-100 GPS/Iridium communicator system 10027379 DANSK FLY ELEKTRONIK ApS P-EASA.A.S.03915 PIPER PA-28-140 PIPER PA-28-150 PIPER PA-28-151 PIPER PA-28-160 PIPER PA-28-161 PIPER PA-28-180 PIPER PA-28-181 PIPER PA-28-235 PIPER PA-28-236 PIPER PA-28R-180 PIPER PA-28R-200 PIPER PA-28R-201 PIPER PA-28R-201T PIPER PA-28RT-201 PIPER PA-28RT-201T PIPER PA-28S-160 PIPER PA-28S-180 Installation of ASPEN EFD1000 PRO Flight display Serial numbers 5026, 5299, 5298 and 5156 only. 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 effe 15.12.2008 21.09.2012 None None 11.08.2009 None - Prior to installation of this modification the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product.- The install 25.09.2009 04/01/2013 Page 159/462
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04/01/2013 Page 1/462 - EASA

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