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 10034640 EAD INC. EASA.IM.A.S.01715 REV. 1 FAA STC ST03205AT BOEING DC-9-82 (MD-82) Installation of Rockwell Collins CMU-900 None Prior to installation of this modification the 31.07.2009 Communications Management Unit,VHF-920 installer must determinethat the VDL Mode 2 Radio, Gables Mode 2 VDR interrelationship between this modification Control Panel and ACARS TP4429 Printer to and any otherpreviously installed provide Controller Pilot Data Link modification will introduce no adverse Communications(CPCDL) Baseline 1 service in effect uponthe airworthiness of the accordance with EAD product. The installati 10029272 EADS CASA P-EASA.A.S.02790 REV. 3 A330-203 WEIGHT VARIANT 052 Conversion of A330-200 Series A/C to A330 Approval of this STC is limited to compliance to This STC can only be installed in 21.12.2011 FOR CONFIGURATION 1 Multi Role Transport Tanker(MRTT) RAAF selected CertificationStandards as defined in conjunction with the modificationsdefined A330-202 WEIGHT VARIANT 052 (Royal Australian Air Force), RSAF (Royal CRI A-01. CRI G-01 defines in by: - Airbus Change G-MRTT-01 certified FOR CONFIGURATION 2 Saudi Arabian AirForce) and UAE (United particularrestrictions relating to Maintenance under EASA ref. 10029273 and- Airbus A330-243 (WEIGHT VARIANT Arabic Emirates Force)Rev. 1 of this STC has Tasks and AirworthinessLimitations, ref JAR Change G-MRTT-02 certified under 052) been issued in order to add Configuration 25.571a(3) and 25.1529.Therefore, the fo EASA ref. 10029276- Airbus Change G- FOR CONFIGURATION 3 2.Rev. MRTT-04 certified under EASA ref. 10034690 EADS CASA P-EASA.A.S.03608 REV. 2 A330-243 A330 MRTT FSTA Modification STC1With the Revision 1 of this STC a previous limitation on the occupationof medical stretchers has been deleted.With the revision 2 of this STC the role change capability isintroduced. Therefore, it is possible for an aircraft None This approval includes the possibility for aircraft and aircraft parttransfer from military operation (INTA Technical Certificateconfiguration) to civil operation (this STC's configuration). For aircraft transfer from military to civil operation:- 10035945 EADS CASA P-EASA.A.S.03607 REV. 2 A330-243 A330 MRTT FSTA Modification STC2 Revision Based on the conditions established in CRI G- The condi 1. This STC can only be installed in 02.08.2012 1Remark: This revision 1 of the STC introduces 01 with respect to thedefinition of the conjunction with the modificationsdefined the following changes:- Deletion of previous Airworthiness Limitation Section of the by: - Airbus Change G-MRTT-01 certified limitation no. 4 on Autoland / CAT III function- Instructionsfor Continued Airworthiness the under EASA ref. 10029273*- Airbus Replacement of temporary conservative Noise following limitations apply:1. As the Change G-MRTT-02 certified under levels by final values- Parti modifications of this STC are intended for EASA ref. 10029276*and - Airbus milita Change G-MRTT-03 certified under EASA 10042436 EADS CASA A330-243 Installation of a Cockpit Door Surveillance None Prior to installation of this modification it 30.11.2012 System in the A330 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. 10014980 EADS ELBE FLUGZEUGWERKE GmbH EASA.A.S.03272 AIRBUS A310-304 A310-304 Cabin ReconfigurationTransfer of the STC holder, from ASL Aircraft Services Lemwerder GmbH to EADS Elbe Flugzeugwerke GmbH.Former LBA STC ref TA0721Cabin Reconfiguration from 265 seats to 225 seats (18 Business Class + 207 1. This STC is limited to A310-304 aircraft model MSN 448.2. Prior to installation of this modification the installer must determine that the interrelationship between this modification andany other previously installed modification will introduce no adver 10014981 EADS ELBE FLUGZEUGWERKE GmbH EASA.A.S.03273 AIRBUS A310-304 Economy Class). A310-304 Floor Path Marking System 1. This STC is limited to A310-304 aircraft 08.10.2007 installationTransfer of the STC holder, from model MSN 448.2. Prior to installation of this ASL Aircraft Services Lemwerder GmbH to modification the installer must determine that EADS Elbe Flugzeugwerke GmbH.Former the interrelationship between this modification LBA STC ref TA0719The modification related andany other previously installed modification to this supplement concerns the installation of a will introduce no adver photolu 10014982 EADS ELBE FLUGZEUGWERKE GmbH EASA.A.S.03274 AIRBUS A320-214 A320-214 Cabin ReconfigurationTransfer of 1. This STC is limited to A320-214 aircraft 08.10.2007 the STC holder, from ASL Aircraft Services model MSN 1081 and MSN 1370.2. Prior to Lemwerder GmbH to EADS Elbe installation of this modification the installer must Flugzeugwerke GmbH.Former LBA STC ref determine that the interrelationship between TA0717 Issue 2Cabin Reconfiguration from this modification andany other previously 156 seats (90 Business Class + 66 Economic Class) to 180 seats ( installed modification will intr 10031745 EADS ELBE FLUGZEUGWERKE GmbH P-EASA.A.S.03661 A300B4-601/ -603/ -620/ -622 Courier Stowage installationThis STC consists The current STC needs specific aircraft Prior to installation of this modification it 09.09.2010 A300B4-605R/ -622R in modifying the Courier Area of aircraft configuration as aprerequisite:- To install this must be determined thatthe A310-304/ -308/ -324/ -325 converted byAirbus Pax to Freighter STCs by STC on A310 aircraft models, embodiment of interrelationship between this modification installing a Courier Stowage EASA STCref: 10013945, Rev 4 (or any and any other previouslyinstalled further EASA approved revision) isrequired.- modification and/ or repair will introduce To install this STC on A300-600 aircraft m no adverse effectupon the airworthiness of the product 04/01/2013 Page 194/462 02.08.2012 08.10.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10013940 EADS SOGERMA EASA.A.S.00376 REV 1 AIRBUS A310-304 Royal Jordanian ATC Mode S Enhanced 1. The Aircraft Flight Manual Supplement No 07.01.2008 Surveillance installation according to EADS AFM-34-974 issue B dated 29 November Sogerma Modification Approval Sheet SOG-34- 2004, or later EASA-approved revision, is a 974 issue 3 dated 29 November 2004.Note: required part of this STC.2. Prior to This revision reflects the transfer of this STC installation of this modification the installer must from EADS Sogerma Services to Sogerma Servic determine that the interrelationsh 10013941 EADS SOGERMA EASA.A.S.00377 REV 1 AIRBUS 310-325 Cabin Modification from 18F/C-180Y/C to Prior to installation of this modification the 07.01.2008 18B/C-188Y/C according to the modification installer must determine that the approval sheet MAS No SOG-25-957 issue 1 interrelationship between this modification and dated 6October 2004 or later EASA-approved any other previously installed modification will revision.Note: This revision reflects the transfer introduce no adverse effect upon the of this STC from EADS Sogerma Services airworthiness of the product. The install 10013950 EADS SOGERMA EASA.A.S.00432 REV 1 AIRBUS 310-325 Modification of ATLAS/KSSU galleys into full Prior to installation of this modification the ATLAS standard in accordance with installer must determine that the Modification Approval Sheet reference SOG-25-interrelationship between this modification and 958 Issue 01 dated 14 October 2004. All any other previously installed modification will documents related to this STC are listed in the introduce no adverse effect upon the Master Drawing List reference MDL-25-958 Iss airworthiness of the product. The install 10014005 EADS SOGERMA EASA.A.S.01042 REV 1 AIRBUS A340-300 Installation of an upper class with side facing Britax Malcom seats with inflatable restraints, monument, bar and chandelier, and modification of the premium and economy class by repitching.Note: This revision reflects the transfer of this STC from EADS So 1. This STC is limited to Airbus A340-300 MSN 214, 002, 003, 164 and 225.2. A copy of this STC and of the MAS/MDL must be enclosed in the files of each modified aircraft. 10014022 EADS SOGERMA EASA.A.S.01077 REV 1 AIRBUS A330-203 Qatar Airways - Cabin Modification. 1. The approval of this modification is limited Modification number: SOG-25-886 issue to the identified aircraft. The limitations and 1Note: This revision reflects the transfer of this conditions defined in the EASA Datasheet are STC from EADS Sogerma Services to also applicable. A copy of the STC approval Sogerma Services.Model: Airbus A330-203 and the MDL must be enclosed in the files of MSN 463 and 504 each modified aircraft. 10014076 EADS SOGERMA EASA.A.S.01168 REV 1 AIRBUS A330-243 Cabin configuration for Gulf Air. All documents Prior to installation of this modification the related to this STC are listed in the Modification installer must determine that the SOG-25-1075 iss. 01 (or later EASA-aproved interrelationship between this modification and revision).Note: This revision reflects the transfer any other previously installed modification will of this STC from EADS Sogerma Services to introduce no adverse effect upon the Sogerma Services.Mod airworthiness of the product. The install 10014077 EADS SOGERMA EASA.A.S.01169 REV 1 AIRBUS A310 Installation of an ATC Mode S EHS. ATC mode S modification for compliance with Enhance Surveillance. Replacement of the Rockwell Collins TRP-720 ATC by TRP-901 ATC.Note: This revision reflects the transfer of this STC from EADS Sogerma Services to Sogerma 07.01.2008 10014087 EADS SOGERMA EASA.A.S.01179 REV 1 DC-9-21 ELT Kannad 406 AF modification (SOG-25- 1106)Note: This revision reflects the transfer of this STC from EADS Sogerma Services to Sogerma Services. 1. This STC is limited to the DC-9 MSN 4708 04.01.2008 10014113 EADS SOGERMA EASA.A.S.01219 REV 1 ATR 42-320 SERIES Pseudo-Lisse configuration; RESSAC 1. In RALI configuration:-the mass of under 04.01.2008 configuration and RALI configuration.Note: This wing POD is limited to 72kg (POD equipped);- revision reflects the transfer of this STC from the new design for the titanium pin on POD EADS Sogerma Services to Sogerma rear attachment must be applied according to Services.Model: Aerospatiale ATR 42-320 the EADS Sogerma Services waiver No. MSN 078 A3002.2. The lighting issues are cert 10014114 EADS SOGERMA EASA.A.S.01220 REV 1 AEROSPATIALE ATR 42-320 ELT Kannad 406 AF ModificationNote: This revision reflects the transfer of this STC from EADS Sogerma Services to Sogerma Services. Model: Aerospatiale ATR 42-320 MSN 078 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 10014169 EADS SOGERMA EASA.A.S.01302 REV 1 AIRBUS A321-200 A321 Livingston - Cabin Modification from 196 Prior to installation of this modification the Y/C to 210 Y/C with relocation of two attendant installer must determine that the seats.Note: This revision reflects the transfer of interrelationship between this modification and this STC from EADS Sogerma Services to any other previously installed modification will Sogerma Services.Model: Airbus A321-200 introduce no adverse effect upon the MSN 1950 & 1970 airworthiness of the product. The install 04/01/2013 Page 195/462 07.01.2008 07.01.2008 07.01.2008 07.01.2008 04.01.2008 04.01.2008
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04/01/2013 Page 1/462 - EASA

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