List of EASA Supplemental Type Certificates

B747-300 in the applicability listRev. 2: Incorporationof B747-8 in the applicability list and STCoriginal number EASA.A.S. 00701 replaced by new number 10013967Rev. 3: Extension of 747-8 ALI task, based on reassessment of DTAanalysis w... The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. B747-300:Supplemental Type Design Document STDD53-12/20M Issue 01 rev 05Maintenance requirements document C- AAL900-MR rev IRB747-400:Supplemental Type Design Document STDD53-12/20M Issue 01 rev 05Instruction for Continued Airworthiness ICA53-0215-01 rev IRB747-8:Supplemental Type Design Document ST... Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product. 09/11/2020 Active 10013967 10013970 (EASA.A.S.00741) PROTOPLANE SPECIAL MISSION AIRCRAFT REV. 3 BEECH 200 B200 Photo Conversion (creation of two hatches for camera).Rev. 3: Transfer of EASA.A.S.00741 Issue 1 for S/N BB-1181and EASA.A.S.00741 Revision 2 for S/N BB221 and BB1607 The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... . For S/N BB-1181: EISA-16-PRE-F045 Rev 3 dated 18/12/2008.For S/N BB-221 and BB-1607: - EISA-16-MDL-F050 Rev 1 dated 17/12/08 - EISA-16-AFM-F050 Rev 3 dated 18/12/08- EISA-16- AMM-F050 Rev 1 dated 17/12/08 - EISA-16-ICA- F050 Rev 1 dated 17/12/08or later revisions of the above liste... Applicable to B200 S/N BB-1181, BB-221, BB-1607;Utilisationof Intercom prohibited in dense traffic areas.Prior to installation of this change/repair it must be determined thattheinterrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no a... 16/04/2024 Active 10013970 10013975 (EASA.A.S.00774) SMA AERO ENGINES GMBH REV. 15 F182P, F182Q B) F182P, F182Q A) 182M, 182N, 182P, 182Q,182R 182M, 182N, 182P, 182Q, 182R Installation of SMA Diesel Engine SR305-230 or SR305—230E andMT- Propeller MTV-9-BS/198-58B.Rev. 14: Transfer of STC 10013975 rev 12 from Safran Aircraft EnginesSAS to SMA Aero Engines GmbH.Rev. 15: Update of annex 1 for typos and incorrectreferences. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval without any im... - SMA Mod. AM 16-082- Flight Manual Supplements: see Appendix dated 17/02/2021- Airworthiness Limitation Information asper Aircraft Service ManualC182-ASMS-01E, Rev. 6, Section 2SMA-AL- Installation Instructions: see Appendix dated 17/02/2021- Aircraft Service Manual C182- ASMS-01E, latest revision.... Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 28/09/2023 Active 10013975 10013976 (EASA.A.S.0097) SCANDINAVIAN AVIONICS DESIGN ApS REV. 2 S550 (CITATION S/II) 560 (CITATION V) 560 (CITATION ULTRA) 550 (CITATION II) 550 (CITATION BRAVO) Installation of an L3 Digital Flight Data RecorderRevision 2 was raised due to missing technical document references inRevision 1 EASA TCDS IM.A.207The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalJAR 25 at change 15The requirements for environmental protection and the associatedcertificated noise and/ or emissionsu... - Master Documents List 2018778-01 DOC issue 8, dated 27 Sept. 2010- Engineering Order 2018778-EO-01 Issue 5, dated 26 Sept. 2010- Airplane Flight Manual Supplement 2018778- AM-01A, issue 5 from 19January 2010 for 115 VAC or alternative Airplane Flight ManualSupplement 2018778-AM-01B, issue 2 from 19... Limited to:S/N 550-0001 through 550-0733 (Citation II)S/ N 550-0801 through 550-1136 (Citation Bravo)S/N 560-0001 through 560-0259 (Citation V)S/ N 560-0260 through 560-0538 (Citation Ultra)S/N S550-0001 through S550-0160 (Citation S/ II) 05/10/2010 Active 10013976 Page 2 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10013987 (EASA.A.S.01019) H4 AEROSPACE (UK) Ltd. REV. 1 CAA UK RESPONSIBIL ITY 737-700 Replacement of a Lufthansa Technik IFE System with an ITAN IFE SystemRevision 1: certificate re-issued after DOA changed its name to H4Aerospace -BBJ383 Issue 2 dated 21 February 2005 or later approved revision-Flight Manual Supplement BBJFMS014 Issue I/R 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. 14/11/2013 Active 10013987 10013993 (EASA.A.S.01024) AERODATA AG REV.11 DORNIER 328-100 Installation of Maritime Surveillance System on Dornier 328-100including SAR Radar, FLIR, and optional IR/UV ScannerRevision 4:Functional/optional upgrade to the radar system and mission software tooptimize search and rescue operation. Hardware upgrade to components ofthe ELTA weather & mission rada... The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. - Master Document List ref MDL-A/C-089 Rev. 13.- Flight Manual Supplement ref AFM-077 Rev. 10.- Aerodata Maintenance Manual Supplement AMM-782 Rev. 9 dated September2012or later revisions of the above listed documents approved by EASA Applicable to Aircraft Serials 3051, 3052, 3053, 3057 and 3059 asmodified by Aerodata Modification D328-2.xx for AMSA Mission Purpose.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change... 29/01/2013 Active 10013993 10014001 (EASA.A.S.01038) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 1 757-200 Installation of Enhanced Mode S TranspondersRev. 1: Transfer of STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... -Aviation Traders Ltd Definition Document DD/ 021/9162 Issue2-Aviation Traders Ltd AFM Supplement Number 31 Issue 1or later revisions of the above listed document (s) approved/ acceptedunder the EASA system. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 08/11/2021 Active 10014001 10014002 (EASA.A.S.01039) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 1 737-700 Installation of Enhanced Mode S TranspondersRev. 1: Transfer of STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... -Aviation Traders Ltd Definition Document DD/ 022/9218 Issue2-Aviation Traders Ltd AFM Supplement Number 29 Issue 1or later revisions of the above listed document (s) approved/ acceptedunder the EASA system. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 08/11/2021 Active 10014002 10014003 (EASA.A.S.01040) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 1 737-300 Installation of Enhanced Mode S TranspondersRev. 1: Transfer of STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... -Aviation Traders Ltd Definition Document DD/ 023/9219/ Issue 2-Aviation Traders Ltd AFM Supplement Number 30 Issue 1or later revisions of the above listed document (s) approved/ acceptedunder the EASA system. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 08/11/2021 Active 10014003 10014007 (EASA.A.S.01047) GROWING ENGINEERING PARTNERS GmbH REV. 2 B747-400 Reconfiguration of Virgin Atlantic Airways B747-400 from LHR to LGWconfiguration in accordance with SR Technics Master Data ListC747-25-1001-MDL-01, Rev 3 or later approved revisionsRev. 2: Transfer of STC from SR Technics Switzerland to groWINGEngineering Partners GmbH The Certification Basis for the original product remains applicable tothis certificate/ approval. C747-25-1001-CCS, Rev 3.C747-25-1001-MDL-01, Rev 3or later revisions of the above listed documents approved by EASA Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 20/04/2021 Active 10014007 Page 3 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014011 (EASA.A.S.01054) airplus engineering GmbH REV. 1 PA-23-250 Installation of1. COM/VOR/ILS/GPS- System Garmin GNS 4302. ELT Kannad 406AF Engineering Order 003-04 Rev 1EASA approved FMS Emergency Locator Transmitter Kannad 406AF Doc No PO0011-000406 Rev 0 or later EASA approved issuesEASA approved FMS Garmin GNS 430VHF Communications Transceiver/VOR/ILS Receiver/GPS ReceiverDoc-No. PO 0011-000430 Rev. 0 or later EASA approved issues... 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/ engineconfigurations shall be determined by the installer. 17/02/2021 Active 10014011 10014012 (EASA.A.S.01055) BABCOCK MISSION CRITICAL SERVICES FMANAGEMENT S.A.U. REV. 1 337G Change to the complete avionics set installed by a new one last generation GARMIN and HONEYWELL The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. "Documento Técnico CMA014, Issue 1" (Aircraft Flight ManualSupplement"CMA01 4-AFMS, Issue 1" included) or later revisions of the above listed document(s) approved/acceptedunder theEASA system. Restricted to: s/n FTB3370020, FTB3370021, FTB3370022, FTB3370023, FTB3370024 & FTB3370025 15/01/2019 Active 10014012 10014013 (EASA.A.S.01056) LUFTHANSA TECHNIK AG REV. 3 A321-271NX/-272NX A321-271N/-272N A321-251NX/-252NX/-253 NX A321-251N/-252N/-253N A321-211/-212/-213/-231/- 232 A321-111/-112/-131 A320-271N/-272N/-273N A320-251N/-252N/-253N A320-231/-232/-233 A320-211/-212/-214/-215/- 216 A319-151N/-153N/-171N A319-131/-132/-133 A319-111/-112/-113/-114/- 115 A318/A319/A320/A321 A318-111/-112/-121/-122 Installation of non-electrical Floor Path Marking System-Configuration 1: All GuideU series; all models except NEO- Configuration 2: GuideU series 1000, all modelsRevision 01 and 02: Editorial correctionsRevision 03: Extended applicability (A320 family NEO models) The Type and OSD Certification Bases for the original product as amendedby the following additional or alternative airworthiness requirements:the following paragraph(s) at a lateramendment:For Configuration 1: EASA CS 25.029(a), 25.301(a) (b)(c), 25.303,25.305(a)(b)(c), 25.307 (a)(d), 25.561(a)(b)(c... Supplemental Type Design Definition STDD33-04/03M issue 03 rev. 00Instructions for Cont. Airworthiness ICA33-04/03M issue 01 rev. 01Airplane Flight manual Supplement A-33-04/4621-AFM issue 01 rev. 01Master Minimum Equipment List SupplementA-33-04/4621- MMEL rev. 01Flight Crew Data A-33-04/4621-FCD i... Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 04/04/2023 Active 10014013 10014023 (EASA.A.S.01078) AIRBUS S.A.S. REV. 2 A319-133 Airbus Corporate Jet Centre Modification CJ2072 - AL SALAM - CONVERSIONPRIVATE TO PUBLIC AND VICE VERSA. The Certification Basis for the original product as amendedby theadditional or alternative airworthiness requirements as listed in theGeneral CRI G-4103 “ACJC Project Certification Basis”.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the... - Modification Approval sheet CJ2072 issue 01 - CONVERSION PRIVATE TOPUBLIC AND VICE VERSA, Issue 01, dated 30th May 2016- AFM Supplement FM-S MOD SOG-00-1030 dated MAY 01/16or later revisions of the above listed documents approved by EASA. This STC approval is limited to A319-133 MSN 2421.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness of the produc... 30/05/2016 Active 10014023 10014034 (EASA.A.S.01107) RUAG AEROSPACE SERVICES GmbH REV. 1 CESNA 550 Introduction of TCAS II Change 7.1 The Certification Basis (CB) for the original product remains applicableto this certificate/ approval. The requirements for environmentalprotection and the associated certified noise and/or emissions levels ofthe original product are unchanged and remain applicable to thiscertificate/ approval Master Document List, RUAG Aerospace document No. 0147C-MDL, Revision 0,dated 9 February 2015.Aircraft Flight Manual Supplement, RUAG Aerospace document No.0147C- AFMS, Revision 0,dated 6 February 2015.or later revisions of the above listed documents approved by EASA. None 20/02/2015 Active 10014034 Page 4 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014040 (EASA.A.S.01114) SAFRAN SEATS REV. 1 767-300 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) The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. -Heath Tecna Modification document C935 and associated DDP dated26/01/2005 or later approved revisions Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product. 12/03/2019 Active 10014040 10014046 (EASA.A.S.01128) MT-PROPELLER ENTWICKLUNG GmbH REV. 1 CESSNA 208, 208B 1. Installation of the MTV-16-1-E-C-F-R (P)/CFR250-55 full feathering andreversible 4-blade constant speed propeller2. Extension of Installation 1 on MTV-16-1-E-C-F-R(P)/ CFR250-55propellers equipped with fluid deice system. The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.FAR 23 includingamendment 34 (not required by 21A.101, elected tocomply by the applicant).This certificate/ approval involves a change t... Installation 1:-Instructions for Continued Airworthiness and Installation InstructionsNo E-1169- Airplane Flight Manual Supplement No E-1168Installation 2:-- Instructions for Continued Airworthiness and Installation InstructionsNo E-1169, Revision 2- Airplane Flight Manual Supplement No E-1168, Revisio... None 12/04/2011 Active 10014046 10014049 (EASA.A.S.01131) BUSINESS AND COMMUTER AIRCRAFT REV. 1 BEECH B300 BEECH 300 Installation of KLN 900 GPS with EFIS-85 according to STCEASA.A.S.01131. The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval:FAR 23 Amdt . 23-62The certificated noise and/ or emissions levels of the original productare unchanged and remain applicable to this cer... File ref.: BCA 26 Rev 2 dated 03/10/2011AFM SUPPLEMENT FOR GPS BENDIX / KING KLN-900 Ed. 01/12 - P/N BCA26 Rev2SMV. BEECH 300 /B300 - F-GPRH - SN FA 226. 06/02/2012 Active 10014049 10014059 (EASA.A.S.01143) DOA AESGLOBAL LIMITED REV. 3 757-200 Introduction of Pegasus Flight Management Computers & MultiModeReceivers (MMRs)Rev 3: Transfer from AES Ltd. to new STC holder AES Global Ltd. The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:the following paragraph(s) at a later amendment: CS-25 Initial Issue25.581(b) - 25.601, 25.603, 25.605(a), 25.607, 25.609(a), 25.613(a)(b),25.789(a), 25.869(a) (4), 25.899... AES Flight Manual Supplement No. 71 Issue 2or later revisions of the above listed documents approved by EASA.AES Modification No. AES-757-376 Issue 8AES Master Data List AES-757-376MDL Issue 15 Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product. 27/04/2021 Active 10014059 10014066 (EASA.A.S.01153) MAGNETIC MRO AS REV. 2 747-400 Modification of Cabin to Install Zone B Cabin Class Dividers, Zone BStowage & Dogbox, Door 2 Port & Starboard Dividers & Upper Deck Dogbox.Revision: Transfer of Certificate to Magnetic MRO AS The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. - Modification Leaflet 04ML110. 1. Compliance with the following Requirements has not been established.:1.1. Viewing of all apllicable placards & signage to in compliance withFAR/JAR 25.791.1.2. Weight, centre of Gravity & Weight Distribution, to be incompliance with JAR25.1519.1.3. Compliance with JAR/FAR25.785 (d)(3). The elimin... 19/09/2019 Active 10014066 10014074 (EASA.A.S.01166) ALAMO ENGINEERING GmbH REV. 3 JETSTREAM 3200 SERIES JETSTREAM 3100 SERIES Installation of Airborne Collision Avoidance System (ACASII).Revision 1: Transfer to 328 DESIGN GmbHRevision 2: Transfer to 328 SUPPORT SERVICES GmbHRevision 3: Transfer to ALAMO Engineering GmbH The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:JAR-25 Change 12:JAR 25.301, JAR 25.303, JAR 25.305, JAR 25.307, JAR 25.571, JAR 25.603,JAR 25.605, JAR 25.607, JAR 25.609, JAR 25.611, JAR 25.1301, JAR25.1309, JAR 25.132... - Avionics Mobile Services Definition Document Part 21-002/1485-01 Issue1- Avionics Mobile Services AFM Supplement Part21-008/011 Issue 1or later revisions of the above listed document(s) approved/acceptedunder the EASA system. This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this change/repair it must be determined thatt... 05/11/2024 Active 10014074 Page 5 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014078 (EASA.A.S.01170) SAFRAN SEATS REV. 1 747-400 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. The Certification Basis for the original product remains applicable tothis certificate/ approval, except where amended by additional or lateramendments if indicated on FAA STC.Therequirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original pro... Heath Tecna Modification document C933 and associated DDP dated 21/6/05or later approved revisions. As defined in DDP, Aircraft Serial MSN 26548. Zero Occupancy. For thismodification to be accepted on an EU registered aircraft, requires theoperator to confirm that all the associate FAA and Hong Kong CDAmodifications have been EASA approved.Prior to installation of this design change it must be det... 14/03/2019 Active 10014078 10014090 (EASA.A.S.01187) ROEDER PRAEZISION GMBH REV. 1 SA227-BC, SA227-DC, SA227-TT SA226-TC, SA227-AC, SA227-AT, SA226-AT, SA226-T(B), SA226-T, Installation of Thommen Air Data Display and Altimeter. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Flight Manual Supplement Doc No SA226/227- NY-0212-08, Rev. 0, or laterEASA approved revision. Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/or repair will introduce noadverse effect upon the airworthiness of the product. 25/09/2017 Active 10014090 10014097 (EASA.A.S.01195) SAFRAN SEATS REV 2 767-300 Introduction G3 Wardrobe to British Airways aircraft as defined in the modification definition document and Declarationof Design and Performance (DDP) The Certification Basis for the original product remains applicable tothis certificate/ approval, except where amended by additional or lateramendments if indicated on FAA STC.Therequirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original pro... Heath Tecna Modification Document C936 and associated DDP, dated 24March 2005, or later approved revisions. As defined in the DDP.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness of the product. 14/03/2019 Active 10014097 10014122 (EASA.A.S.01232) DOA AESGLOBAL LIMITED REV. 2 767-300 Introduction of 258 Passenger Configuration & Associated Cabin Changes.Rev. 1: FAR Part 26 Validation for EASA STC EASA.A.S.01232.Rev. 2: Transfer from AES Ltd. to new STC holderAES Global Ltd. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. AES Ltd. Master Data List No. AES-767-330MDL Issue 6 dated 14 December2012;or later revisions of the above listed documents approved by EASA. Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product.This Supplemental Type Certificate is approved o... 27/04/2021 Active 10014122 10014123 (EASA.A.S.01233) DOA AESGLOBAL LIMITED REV. 1 767-300 Introduction of Matsushita in-Flight Entertainment SystemRev 1: Transfer from AES Ltd. to new STC holder AES Global Ltd. AES Master Data List AES-767-355MDL Issue 2 or later EASA approved revision Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 28/04/2021 Active 10014123 10014125 (EASA.A.S.01235) SABENA TECHNICS BGC REV. 1 A321-213/-231/-232 A321-111/-112/-131/-211/- 212 A320-233 A320-211/-212/-214/-231/- 232 A319-131/-132/-133 A319-111/-112/-113/-114/- 115 ELT Antenna InstallationInstallation of an Emergency Locator Transmitter external RAYAN antennaP/N: 2624-82, structuralelements only. The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:The following paragraph(s) at a later amendment: Applicable regulationsat CS 25 Initial Issue (refer to associated Certification Plan0243-01-A-2101-R02 section 5).The requ... Master Data List, ref : 0243-01-A-2103- R02Instructions for Continued Airworthiness, ref : 0243-01-A-2211-R02. Airworthiness Limitations inspection requirements apply forExtendedService Goal aircraft, as described in section 3 ofInstructions forContinued Airworthiness (Supplement), ref: 0243-01-A-2211-R02.Prior to installation of this change/ repair it must be determined thatthe interrelationship between th... 08/02/2019 Active 10014125 10014138 (EASA.A.S.01249) ACC COLUMBIA Jet Service GmbH REV. 2 35/ 35A Installation of Honeywell MST-67A dual Mode S XPDR/CAS-67A TCAS II System. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. 1. ACC Master Document List ACC-LR35-50096, Revision 0, or later EASAapproved revisions.2. ACC AFMS LR35-50096-820-S-MF, Revision 0, or later EASA approvedrevisions.3. ACC AFMS LR35-50096-830-S- MF, Revision 0, or later EASA approvedrevisions. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 19/01/2022 Active 10014138 Page 6 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014139 (EASA.A.S.01252) ALAMO ENGINEERING GmbH REV. 3 650 550 AND 650 550 Installation of an Airborne Collision Avoidance System (ACAS II).Revision 1: Transfer to 328 DESIGN GmbHRevision 2: Transfer to 328 SUPPORT SERVICES GmbHRevision 3: Transfer to ALAMO Engineering GmbH The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:JAR-25 Change 17:JAR 25.301, JAR 25.303, JAR 25.305, JAR 25.307, JAR 25.571, JAR 25.603,JAR 25.605, JAR 25.607, JAR 25.609, JAR 25.611, JAR 25.1301, JAR25.1309, JAR 25.132... Avionics Mobile Services Project Certification Plan AM/1493. AvionicsMobile Services AFM Supplement Number Part21-008/008.or later revisions of the above listed document(s) approved/acceptedunder the EASA system This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this change/repair it must be determined thatt... 05/11/2024 Active 10014139 10014142 (EASA.A.S.01256) ROEDER PRAEZISION GMBH REV. 2 A330-322 Cabin reconfiguration from a 18 B/C + 331 Y/C layout to a 18 B/C +343Y/C layout.This STC installs a new cabin arrangement. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.As per EASA TCDS A. 004Elect to Comply with CS25 (Original Issue) requirements: 25.0811(d)/ 25.812(d)(e)/ 25.813 (a)(b)(e)/ 25.851(a)/25.853(a)(c)(f) (h)/ 25.869(a)(b)(c).The requirements for environmen... Master Document List, ref. MDL330-25-01-05 Revision 2, dated 27 Apr.2005<(>,<) >or later revisions of the above listed documents approved by EASA. 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. 15/06/2018 Active 10014142 10014143 (EASA.A.S.01261) SAFRAN SEATS REV. 1 747-400 Heath Tecna Modification C943 - Cathay Interiors Modification. The Certification Basis for the original product remains applicable tothis certificate/ approval, except where amended by additional or lateramendments if indicated on FAA STC.Therequirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original pro... Heath Tecna Modification Document C943 & associated DDP, dated 1 August2005 or later approved revision. As defined in DDP Aircraft Serial Numbers 25172 & 25128. Zero Occupancy.For this modification to be accepted on an EU registered aircraftrequires the operator to confirm that all the associated FAA & Hong KingCAD modifications have been EASA approved.Prior to installation of this design change it mu... 14/03/2019 Active 10014143 10014147 (EASA.A.S.01266) ATELIER CHABORD REV. 3 DR 400/2+2 DR 400/120, DR 400/120 D DR 400/120 D, DR 400/2+2 DR 400/100, DR 400/120 DR 300/108, DR 315, DR 400/100 DR 300/108, DR 315 Installation of exhaust system according to Chabord modificationSTC- DR420-2015-01Rev. 3:,,- Enhanced silent blocks- Alternative anti corrosion surface treatment- Enhanced materialon different parts- Enhanced shape of central structural part in muffler- Additional bracket on double rod tube. The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- The following paragraph(s) at a later amendment:CS 23 Amdt 3 § 607,611, 783, 807, 867, 1101, 1121, 1123, 1125, 1529.The requirements for environmental protection and th... Technical Dossier ref. STC- DR420-2015-01 Revision D dated 04 January2022< (>,<)>Or later revisions of the above listed document (s) approved/ acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21.A.109.Prior to installation of this change/ repairit must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffect upon the airworth... 24/01/2022 Active 10014147 10014148 (EASA.A.S.01268) SCANDINAVIAN AVIONICS DESIGN ApS REV. 1 2. SA227-TT 2. SA226-T(B), SA227-AT 2. A226-T, SA226-AT 1. SA227-BC 1. SA226-TC, SA227-AC Installation of Honeywell CAS 67A ACAS II System with dual Mode STransponder Design:Non-significant changeThe Certification Basis of theoriginal product and the followingadditional /,,alternativeair worthiness requirements are applicable tothis changeFor the change CS-23 has been elected to comply with where possible.Environmental Protection:The certificated noise and/ or e... EASA approved Engineering Order, Doc. No. 2027046-EO, issue2, dated25-Oct-2010, or later approved issueEASA approved Aircraft Flight Manual Supplement, Doc. No.2027046-AM-01A, Issue 2, dated 07-Jun-2005<(>,<) > or later approvedissue, andEASA approved Aircraft Flight Manual Supplement, Doc. No.20270... This change is limited to the configuration of aircraft / equipment typeas listed under Chapter 4. in EASA approved Engineering Order, Doc. No. 2027046-EO, Issue 2, dated 25- Oct-2010, or later approved issue. 08/11/2010 Active 10014148 10014159 (EASA.A.S.01290) TELEDYNE UK LIMITED REV. 2 CAA UK RESPONSIBIL ITY BOEING 767-300 767-300 Installation of Teledyne Controls OQAR (Controls Optical Quick AccessRecorder) Rev. 1: Transfer of Approval Certificate to new Certificate Holder (fromTeledyne Ltd to Teledyne UK Ltd).Rev. 2: Correction of the Applicant name and address. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval without any im... Master Data List STC- MDL-015-02 dated 27 September 2005<(>,<)>or later revisions of the above listed document(s) approved/acceptedunder the EASA system. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 20/11/2020 Active 10014159 Page 7 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014160 (EASA.A.S.01292) ACC COLUMBIA Jet Service GmbH REV. 1 F27MK500 Installation of an ARTEX ELT C406-1/-2.Rev. 1: Transfer of STC from Gomolzig Aircraft Services GmbH to ACCColumbia Jet Service GmbH The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. None. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 03/03/2022 Active 10014160 10014163 (EASA.A.S.01295) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 1 767-300 Installation of Teledyne Flight Data Acquisition Unit P/N 2233000-811 toprovide parameters to the FDRRev. 1: Transfer of STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... None This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this change/repair it must be determined thatt... 08/11/2021 Active 10014163 10014175 (EASA.A.S.01310) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 1 114B Wing auxiliary Spar RepairRev. 1: Transfer of STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... Modification Summary Sheet - ALT/COM/M001or later revisionsof the above listed document(s) approved/acceptedunder the EASA system. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 09/11/2021 Active 10014175 10014184 (EASA.IM.A.S.01322) ALAMO ENGINEERING GmbH REV. 3 HAWKER 800XP Installation of an Airborne Collision Avoidance System (ACAS II).Revision 1: Transfer to 328 DESIGN GmbHRevision 2: Transfer to 328 SUPPORT SERVICES GmbHRevision 3: Transfer to ALAMO Engineering GmbH The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:JAR-25 Change 17:JAR 25.301, JAR 25.303, JAR 25.305, JAR 25.307, JAR 25.571, JAR 25.603,JAR 25.605, JAR 25.607, JAR 25.609, JAR 25.611, JAR 25.1301, JAR25.1309, JAR 25.132... - Avionics Mobile Services Project Certification Plan AM/1498 ReferencePART21-003/149 8-01- Avionics Mobile Services AFMSupplement reference AFM PART21-008 Issue2or later revisions of the above listed document(s) approved/ acceptedunder theEASA system. This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this change/repair it must be determined thatt... 05/11/2024 Active 10014184 10014191 (EASA.A.S.01333) LUFTHANSA TECHNIK AG REV. 2 767 SERIES Installation of non-electrical Floor Path Marking System. STDDNo. 33-05/02M, Issue 2AFMS Doc. No.A-33-05/314-AFMAFM Supplement for Boeing 767 SeriesLHT Doc. No. A-33-05/331-AFM,dated October 31/05 or later approved revision 05/03/2014 Active 10014191 10014198 (EASA.A.S.01341) ALAMO ENGINEERING GmbH REV. 3 HAWKER 800XP Installation of an Airborne Collision Avoidance System (ACAS II).Revision 1: Transfer to 328 DESIGN GmbHRevision 2: Transfer to 328 SUPPORT SERVICES GmbHRevision 4: Transfer to ALAMO Engineering GmbH The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:JAR-25 Change 17:JAR 25.301, JAR 25.303, JAR 25.305, JAR 25.307, JAR 25.571, JAR 25.603,JAR 25.605, JAR 25.607, JAR 25.609, JAR 25.611, JAR 25.1301, JAR25.1309, JAR 25.132... - Avionics Mobile Services Project Certification Plan AM/1498 ReferencePART21-003/149 8-01- Avionics Mobile Services AFMSupplement reference AFM PART21-008/001Issue 2or later revisions of the above listed document(s) approved/ acceptedunderthe EASA system. This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this change/repair it must be determined thatt... 05/11/2024 Active 10014198 Page 8 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014208 (EASA.A.S.01360) DOA AESGLOBAL LIMITED REV. 1 767-300 Introduction of 279 passenger configurationRev 1: Transferfrom AES Ltd. to new STC holder AES Global Ltd. Aerospace Engineering Solutions Modification AES-767-426 dated April 13 2005 or later approved revision. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 28/04/2021 Active 10014208 10014214 (EASA.A.S.01374) ACC COLUMBIA Jet Service GmbH REV. 2 CESSNA F182-Q CESSNA F182-P CESSNA 182Q CESSNA 182P CESSNA 182N CESSNA 182M CESSNA 182L CESSNA 182K CESSNA 182J CESSNA 182H CESSNA 182G CESSNA 182F CESSNA 182E Installation of Noise Reduction Kit C182-606650 - Anhang zum Flughandbuch SPOH_12498_IO550_HM- Anhang zum Flughandbuch SPOH_12498_IO550_NQ- Anhang zum Flughandbuch SPOH_12498_O550_EM- Anhang zum Flughandbuch SPOH_12498_O550_NQ- Umrüstungsanweisung II_12498 1. The approval is valid only in combination with the installation of FAA STC SA009133SC (Texas Skyways Inc) or STC SA00152WI (Air Plains Services Corp.) Both with own EASA approval.2. The approval for the models Cessna 182 E, F and G is not valid for the combination with the installation of S... 03/02/2022 Active 10014214 10014215 (EASA.A.S.01376) ALAMO ENGINEERING GmbH REV. 3 650 550 AND 560 550 Avionics Mobile Services Modification AM/1478. Installationof anAirborne Collision Avoidance System (ACAS II).Revision1: Transfer to 328 DESIGN GmbHRevision 2: Transfer to 328 SUPPORT SERVICES GmbHRevision 3: Transfer to ALAMO Engineering GmbH The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:JAR-25 Change 12:JAR 25.301, JAR 25.303, JAR 25.305, JAR 25.307, JAR 25.571, JAR 25.603,JAR 25.605, JAR 25.607, JAR 25.609, JAR 25.611, JAR 25.1301, JAR25.1309, JAR 25.132... - Avionics Mobile Services Ltd Project Certification Plan AM/1478reference PART21-003/1478-01.- Avionics Mobile Services Ltd AFM Supplement PART21-008/008 dated April08 2005or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this change/repair it must be determined thatt... 05/11/2024 Active 10014215 10014218 (EASA.A.S.01379) LUFTHANSA TECHNIK AG REV. 1 AIRBUS A340-600 Installation of Antenna, Receiver Transmit System, and Network services.This STC installs through the cabin a set of equipment to allow dataexchange.The Revision 1 has introduced some modifications through the initial STCdesign by upgrading the existing Wireless Access Points (WAPs) tosupport the IE... The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Supplemental Type Definition Document, ref. STDD46-11/14, Issue 1;Instruction for Continued Airworthiness, ref. R-00-04/120, Revision 5;Aircraft Fligth Manual Supplement, ref. A-00-04/133-AFM, Revision 2;or later revisions of the above listed documents approved by EASA. Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product. 27/02/2013 Active 10014218 10014219 (EASA.A.S.01380) CEAPR REV. 12 DR 400/RP DR 400/200 R DR 400/180 R, DR 400/200 R DR 400/180 R DR 400/140 B DR 400/120 D, DR 400/140 B DR 400/120 D 1. Installation of TAE 125 engine2. Installation of TAE 125-02-99 engine and installation of FADEC BackupBattery3. Installation of TAE 125-02-1 14 engineRevision 9 follows implementation of DET 211005 Amdt F dated 12/03/2024.Revision 10 follows implementation of DET 211005 Rev1 dated 17/07/2024.Revi... The Type and OSD Certification Bases for the original product as amendedby the following additional oralternative airworthiness requirements:The following paragraph(s) at a later amendment: JAR 23, Amdt. 1 InitialIssue(not required by 21A. 101, elected to comply by the applicant)This certificate! app... For TAE 125-01 engine:1. Type Design Definition TDD-60-01 Issue 4 Revision 102. Supplemental Pilot’s Operating Handbookfor DR400/120D/140B/180R/ 200Requipped with TAE 125-01 or TAE 125-02-99 n °1001639 Issue 3 Revision 0dated July 20143. Supplemental Aircraft Maintenance Manual AMM-60-01 Issue 3 Revi... Installation of TAE 125-02-114 is limited to DR 400 models with S/N 2574and upwards.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffect upon the... 13/10/2025 Active 10014219 10014238 (EASA.A.S.01402) MT-PROPELLER ENTWICKLUNG GmbH REV. 2 1. DV20 & 2. DA20-A1 Extension of EASA STC EASA.A.S. 01402Installation of the 2-blade MTV-21- A/170-05 The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CS-VLA, Amendment 1 (not required by 21A.101, elected to comply by theapplicant)This certificate/ approval involves a change to the requi... - Aircraft Flight Manual Supplement, Doc. No. E-1909, rev 0, 14.09.2010- Instructions for Continued Airworthiness, Doc.No. E-1911, rev. 0,14.09.2010or later revisions of the above listed documents approved by EASA none 04/11/2010 Active 10014238 Page 9 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014248 (EASA.A.S.01470) AEROTEC & CONCEPT REV. 4 SEE EASA APPROVED MODEL LIST Cabin Baby Bassinet InstallationRev. 4: Revision of EASA Approved Model List (AML) to cover followingA/C Type: A350, B787 & EMB-190. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. - MASTER DATA LIST AE19081MDL Rev. 2- INSTRUCTION FOR CONTINUED AIRWORTHINESS AE19081ICA Rev. 1- INSTRUCTIONS FOR CCOM SUPPLEMENT AE19081ST Rev. 1- MASTER DRAWING LIST AE19081MDWLRev. 1or later revisions of the above listed document(s) approved/acceptedunder the EASA system. Configuration: A/C with provision for Baby Bassinet Installation.Prior to installation of this change/repair it must bedetermined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repairwill introduce no adverseeffect upon the airworthiness of th... 31/01/2022 Active 10014248 10014250 (EASA.A.S.01472) FTI ENGINEERING NETWORK GmbH REV. 3 B200 Installation of cloud research and seeding system.Rev 2 reflects the transfer of EASA.A.S.01472 Rev 1 from ScandinavianAvionics GmbH to Beechcraft Berlin Aviation GmbH.Rev 3 reflects the transfer from Beechcraft Berlin Aviation GmbH to FTIEngineering Network GmbH. The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... Airplane Flight Manual Supplement, Document 2023287-AM-01 Issue 5, datedAugust 2005;Continued Airworthiness Document 2023287- CA-01;Engineering Order Document 2023287- EO-01or laterrevisions of the above listed document (s) approved/ acceptedunder the EASA system. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 27/03/2025 Active 10014250 10014254 (EASA.A.S.01479) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 1 707-300 Avionics UpgradeRev. 1: Transfer of STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... 1. ATL Modification ATL/ 707/M127.2. Compliance Plan CP/032/9501 Issue 63. Flight Manual Supplement ATL AFM Supplement Number 34 Issue 1or later revisions of the above listed document (s) approved/ acceptedunder the EASA system. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 09/11/2021 Active 10014254 10014256 (EASA.A.S.01483) LUFTHANSA TECHNIK AG REV. 2 FOKKER F.28 MARK 0100 FOKKER F.28 MARK 0070 Installation of non-electrical Floor Path Marking System 1. Supplemental Type Definition Document STDD33-05/01M, issue 01 dated03.03.20062. Airplane Flight Manuel Supplement A-33-05/328-AFM3. Applicant's Declaration of Compliance dated 17.03.2006or later revisions of the above listed documents approved by EASA 05/03/2014 Active 10014256 10014266 (EASA.A.S.01495) TROYES AVIATION S.A.R.L. REV. 4 F177RG Rev 4: Provisions for three attachments in the right side of theinstrument panel in accordance with the STC EASA.A.S. 01495R1: Additionof applicability to F177RG S/N 047 The Certification Basis (CB) for the original product remains applicableto this certificate/ approval. -Supplement Flight Manual Rev.1 dated 16/11/2005or later revisions of the above listed documents approved by EASA.-Troyes Aviation REF 51.-Minor Change Troyes Aviation REF 51 Revision 2 July 2009-Minor Change Troyes Aviation REF 45 approved under EASA.A.S.01495Revision 1 FR177RG S/N 0112, 0065, 103, 153 and 087 F-BURU; S/N 051 D-EMEN; S/N 047The installation of this modification by third persons is subject towritten permission of the approval holder and holding and disposal ofthe approved appropriate documentationThe approval holder shall fulfill the obligations of2... 07/05/2018 Active 10014266 10014271 (EASA.A.S.01501) CESSNA DUESSELDORF CITATIONSERVIC E CENTER GmbH REV. 1 525, 525A Installation of Honeywell KMH 880 or KMH-980 The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.FAR-23The requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original productu... Installation Procedure 2003-10-1, Rev. CFlight Manual Supplement 2003-10-8, Rev. DMaintenance Manual Supplement 2003-10-10, Rev. Bor later revisions of the above listed documents approved by EASA none 27/06/2011 Active 10014271 Page 10 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014281 (EASA.A.S.01518) LUFTHANSA TECHNIK AG REV. 3 737 SERIES 737-900/-900ER/-8/-9 737-500/-600/-700/-800 737-100/-200/-200C/-300/- 400 Installation of non-electrical FPM SystemRev. 1: product name updatedRev. 2: applicability extended to the “Max” models737-8 and 737-9.Rev. 3: typos corrected The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval without any im... Supplemental Type Definition Document STDD33-05/03M Issue 2Rev 1Airplane Flight Manual Supplement A-33-05/324-AFM Issue IR Rev 0Instructions for Continued Airworthiness ICA33-05/03M Rev 2Master Minimum Equipment List Supplement A-00-19/68-MMEL Rev 2or later revisions of the above listed document(s)... Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 15/03/2021 Active 10014281 10014282 (EASA.A.S.01519) LUFTHANSA TECHNIK AG REV. 1 BOEING 747-400 747-400 VVIP Cabin installationRev. 1: Replacement of conductive oxygen flex- hoses with non- conductiveones.Renumbering the certificate from EASA.A.S.01519 to 10014282. The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- Special Condition (s): CRI D-1.1 “Isolated Compartments” Issue 1, CRID-1.2 "Integration of large nonstructural” Issue 1.- Deviation(s): CRI D-1.3 “Firm Handhold” Issue 1... Generic Documents:STDD 25-05/06M Issue 2 Rev. 2Cabin installation documents: STDD 25-05/19 Issue 1AFM Supplement A-00-06/181- AFM Issue 1 rev 5ICA document A-00-06/137 Issue 1 rev 0Oxygen flex hoses replacements: CPL 35-20/07M Rev 0or later revisions of the above listed document(s) approved/ acceptedun... As per AFM Supplement A-00-06/181-AFM.Prior to installationof this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffect upon the airworthiness of the product. 18/11/2020 Active 10014282 10014287 (EASA.A.S.01527) CONTINENTAL AEROSPACE TECHNOLOGIES REV. 15 LBA EMZ SA1295 F172L, F172M, F172N, F172P F172F, F172G, F172H, F172K 172R, 172S 172L, 172M, 172N, 172P 172F, 172G, 172H, 172I, 172K Major Change to STC EASA.A.S.01527, Revision 5:1. Installation of engine TAE 125-01 in accordance with InstallationManual IM-20-01 and Type Design Definition Doc. No. TDD-20-01;2.Installation of engine TAE 125-02-99 in accordance with InstallationManual IM-20-02 and Type Design Definition Doc. No.3... The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- Special Condition (s): CRI A-01lssue 7 (Dec 13, 2007).- Equivalent Safety Finding (s): CRI A-01lssue 7 (Dec 13, 2007).- The following paragraph (s) at a later amendment: JA... Instructions for operation:Cessna (F) 172- N, -P with TAE 125-01 installation:- Anhang Flughandbuch für (Reims) Cessna (F) 172 N & P mit TAE 125Installation, TAE Nr: 20-0310-20011,Ausgabe 1, LBA anerkannt am31.10.2002 oder jede spätere LBA/EASA- anerkannte Ausgabe.- Supplement Pilot's Operating Handb... This STC supersedes LBA-EMZ SA 1295.Limitations for TAE 125-01 & TAE 125-02-99:- Take off power: 99 KW at 2300 min-1 (Propellerspeed)- Max. continuous power: 99 KW at 2300 min-1 (Propellerspeed)- Fuel: Service Bulletin TM TAE 601-0005For Cessna 172S and for increased weight versions of 172R (perLuft... 21/01/2020 Active 10014287 10014292 (EASA.A.S.01534) LUFTHANSA TECHNIK AG REV. 1 B737-700 IGW Revision of EASA.A.S.01534 IR per Major Change 0010002739-001:Operationat 8.99 psi maximum cabin differential pressure (Lower Cabin Altitude,LCA)Original STC Title: B737-700 IGW VIP Cabin 19 Pax. The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval:-CRI-D01 (Doors between Passenger Compartments)-CRI D-02 (Isolated Compartments)-CRI F-01 (Executive Power System)- TGL No.17 (Passenger S... - Supplemental Type Definition Doc STDD00-05/07M Issue 03, dtd Oct 22,2012;- AFM Supplement Doc A-00-06/100-AFM, Revision 03, dated Jul 18/06;- Instructions for Continued Airworthiness (ICA) Doc A-00-06/100-ICAIssue 01, dated June 2, 2010;or later revisions of the above listed documents approved by... Once LCA is activated (installation of FAA STC ST01697SE asvalidatedper EASA STC 10042295) on an individual aircraft, the maintenancerequirements defined in Doc A-00-06/100-ICA will apply for the life ofthis aircraft. This limitation remains valid also in case ofdeactivation of FAA STC ST01697SE as... 03/12/2012 Active 10014292 10014298 (EASA.A.S.01542) SAFRAN SEATS REV. 1 767-300 Business Class Footstool Assemblies on British Airways Boeing 767-300 The Certification Basis for the original product remains applicable tothis certificate/ approval, except where amended by additional or lateramendments if indicated on FAA STC.Therequirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original pro... Heath Tecna Modification document C973 & associated DDP<(>,<)> Issue 1<(>,<)> or later approved revision. This STC is limited to S/N 24340, 24341, 25204, 25444, 25442, 25732,25826, 25828, 25829, 27140, 24335, 24336, 25831 and25834.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or... 14/03/2019 Active 10014298 Page 11 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014302 (EASA.A.S.01546) ACC COLUMBIA Jet Service GmbH REV. 3 DR400/2+2, DR400NGL, DR400/100 DR400/180S DR400/180, DR400/180R DR400/160, DR400/160D DR400/140, DR400/140B DR400/120, DR400/120A DR400/120D, DR400/125 DR315, DR340, DR360, DR380 DR300/140, DR300/180R DR300/125 DR300/108, DR300/120 DR300/400 MOGAS OperationInstallation of a modification kitto allow the operation with MOGASi.a.w. EN228 to aircrafts models and variants as listed above. Theinstallation can be performed to aircrafts of the existing fleet and toaircraftsin production. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. General: Master Document List MDOCL_2030326_rev1_20 130815Model DR300() and DR315 - no wing tanks; retrofitFlight ManualSupplement SPOH_8696_DR300_ rev1_20130415Installation Instruction II_2030326_DR300_RF_FT _rev0_20130415Maintenan ce Manual Supplement MMS_2030326_rev0_2013 0415Model DR340; DR360 and... According limitation section of AFMMust be maintained iaw. Original MM and in addition iaw SupplementalMaintenance Manual MMS_2030326_rev0_2013041 5 or later approved revisionsPrior to installation of this modification it must be determinedthatthe interrelationship between this modification and anyi... 03/02/2022 Active 10014302 10014303 (EASA.A.S.01547) ALAMO ENGINEERING GmbH REV. 3 PA-31T2 (CHEYENNE IIXL) Certification of FAA Approved field modifications for the issue of anEASA C of A.Revision 1: Transfer to 328 DESIGN GmbHRevision 2: Transfer to 328 SUPPORT SERVICES GmbHRevision 3: Transfer to ALAMO Engineering GmbH The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:EASA Certification Specification CS-23 Initial Release Sections: 23.301,307, 23.365, 23.441, 23.603-609, 23.625, 23.1301, 23.1309, 23.1321,23.1322, 23.1351(a), 23.1357, 23... Avionics Mobile Services AFM supplement Part 21-008 014 GNS-530.Avionics Mobile Services AFM supplement Part 21-008 015KMH-880.Avionics Mobile Services AFM supplement Part 21-, 008 016 SN3308.or later revisions of the above listed document(s) approved/ acceptedunder the EASA system This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this change/repair it must be determined thatt... 05/11/2024 Active 10014303 10014305 (EASA.A.S.01549) FOKKER SERVICES B.V. REV. 2 737 SERIES Number 1 Cockpit Windshields. Addition of layers of polyurethaneinterlayer to the existing qualified designs to improvein- servicereliability.Rev. 2: Transfer from GKN Aerospace to Fokker Services The Certification Basis (CB) for the original product remains applicableto this certificate/ approval. The requirementsfor environmentalprotection and the associated certified noise and/ or emissions levelsof the original product are unchanged and remain applicable to thiscertificate/ approval. GKN Aerospace Modification C/R 014or later revisions of theabove listed documents approved by EASA. None. 17/07/2017 Active 10014305 10014312 (EASA.A.S.01557) TENENCIA Ltd. REV. 1 CAA UK RESPONSIBIL ITY 3. BEECH G58 2. BEECH 58/58A 1. BEECH 58PA Hawker Beechcraft Baron Steep Approach Landing CertificationThis Certification at Revision 1 of the STC ref. EASA.A.S.01557 includesadditional aeroplane models compared to the initial issue of the STC The Certification Basis for the original product remains applicable tothis certificate/ approvalThe certificated noise and/ or emissions levels of the original productare unchanged and remain applicable to this certificate/ approval Tenencia Ltd Modification TEN 426, "Hawker Beechcraft BaronSteepApproach Landing Certification", Issue 4 dated 20 May 2010.Tenencia Ltd AFM Supplement 1 Issue 2 to the Beech 58PAPilot'sOperating Handbook and FAA Approved Airplane Flight Manual P/ N102-590000-41Tenencia Ltd AFM Supplement 1 Issue 1P... Hawker Beechcraft Model 58PA S/N TJ-256 andHawker Beechcraft Model 58 S/N TH-1967 only. 26/05/2010 Active 10014312 10014320 (EASA.A.S.01571) MAP AIRCRAFT PART 21 AS REV. 3 737-800 Change of the cabin layout to Swedish National Air Medevac (SNAM) SASProject number737-2520-01 and SAS Project number 737-2520-02Revision 2: Transfer of STC from Scandinavian Airlines System to SASTechnical Services AB.Revision 3: Transferof STC from SAS Technical Services AB to MAPAircraft Part 21... The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. SAS Project number 737-2520-01-SAS Technical Order MTO-255155E-SAS Technical Order MTO-255491A-SAS Flight Manual Supplement for Boeing 737-800 Supplement No.SAS-737- SNAM, Project No. SAS-737-2520-01-SAS drawing "737-800 Air Medevac Cabin Configuration", No. GE-737-1010SAS project number 737-2520-01-... SAS Project Number 737-2520-01: s/n 28318, 28324, 28325, 28326, 28327,28328, 30195, 30196, 30197, 30469, 30470, 30471, 32276, 32277 and 32278.SAS Project Number 737-2520-02: s/n 28318, 28323, 28324, 28325, 28326,28327, 28328, 30194, 30195,30196, 30197, 30467, 30468, 30469, 30470,30471, 32276, 32277... 14/12/2017 Active 10014320 Page 12 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014322 (EASA.A.S.01575) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 2 A300 B4-103, A300 B4-203 Introduction of Enhanced Mode S TransponderRev. 2: Transferof STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... -Aviation Traders Limited Modification 9613<(>,<)>- ATL AFM Supplement 35 Issue 3, SSR Mode S Elementary & EnhancedSurveillance (Without LHAS-STC ST01149LA Installed)<(>,<) >-ATL AFM Supplement 47 Issue 1, SSR Mode S Elementary EnhancedSurveillance (With LHAS-STC ST01149LA Installed).or later revision... This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this change/repair it must be determined thatt... 09/11/2021 Active 10014322 10014323 (EASA.A.S.01576) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 1 727 SERIES Introduction of Terrain Awareness & Warning System (TAWS)Rev. 1: Transfer of STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... -Aviation Traders Modification ATL/727/M165 Issue 3-Aviation Traders AFM Supplement No 37or later revisions of the above listed document(s) approved/acceptedunder the EASA system. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 09/11/2021 Active 10014323 10014325 (EASA.A.S.01578) LUFTHANSA TECHNIK AG REV. 3 747-400, 747-400F Installation of non-electrical Floor Path Marking System Supplemental Type definition Document STDD33-02/05M, issue 03 dated21/03/2006Airplane Flight Manual Supplement A-33-05/340- AFMApplicant's Declaration of Compliance dated 30/03/2006or later revisions of the above listed documents approved by EASA 05/03/2014 Active 10014325 10014330 (EASA.A.S.01583) SAAB AB REV. 1 LEARJET 35A 35A Installation of Target Mission Operators ConsoleRev. 1: Transfer from Saab Nyge Aero AB to SAAB AB. The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval wi... Saab Nyge Aero Technical Directive-Modification, TDM03-03. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 06/12/2023 Active 10014330 10014357 (EASA.A.S.01622) GAMA ENGINEERING Ltd. REV. 2 CAA UK RESPONSIBIL ITY 200, 300 Installation of a Ground Use Battery (GUB) system Gama Aviation Mod refHL/ MOD/1370. The Certification Basis for the original product remains applicable tothis certificate/ approval.The requirements for environmental protection and the associatedcertificated noiseand/or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Installation in accordance with GAMA Aviation Modification HL/MOD/ 1370,as defined by Master Drawing List (MDL) ref MDL-1370 Issue 1, dated 5January 2015, and installation instructions IPI-1370 Issue 1, dated 5January 2015.Operation in accordance with GAMA Aviation Flight Manual Supplement refAFMS-13... Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product. 10/02/2015 Active 10014357 10014358 (EASA.A.S.01623) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 1 757-200 Introduction of Enhanced Mode S TransponderRev. 1: Transferof STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... Aviation Traders Modification 9673 ATL AFM Supplement 36or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 09/11/2021 Active 10014358 Page 13 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014362 (EASA.A.S.01629) SEGELFLUG GRUPPE SIEMENS MÜNCHENE.V. REV. 1 HK 36 TC Optional operation with skis with directional control and breakingsystem instead of wheels in winter The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Ergänzung 1 zum Wartungshandbuch, Version 2 vom 04.02.2012Ergänzung 5 zum Flughandbuch, Version 2 vom 30.11.2012or later revisions of the above listed documents approved by EASA. Limited to S/N 36730 fitted with Skis.Prior to installationof this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness of the product. 29/01/2014 Active 10014362 10014364 (EASA.A.S.01632) CONTINENTAL AEROSPACE TECHNOLOGIES REV. 17 LBA-EMZ SA 1377 PA-28-181 (ARCHER III) PA-28-180 (CHEROKEE) PA-28-180 (ARCHER) PA-28-161 (WARRIOR II) PA-28-161 PA-28-160 (CHEROKEE) PA-28-151 (CHEROKEE WARRIOR) PA-28-150 (CHEROKEE) PA-28-140 (CHEROKEE CRUISER) 1. Installation of engine TAE 125-01 in accordance with InstallationManual IM-40-01 and Type Design Definition Doc. No.: TDD 40-01.2. Installation of engine TAE 125-02 in accordance with InstallationManual IM-40-02 and Type Design Definition Doc. No.:TDD 40-02.3. Installation of a FADEC Backup Batte... The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- Special Condition (s): CRI A-01 Issue 7 (March 07,2008)- Equivalent Safety Finding(s): CRI A-01 Issue 7 (March 07,2008)- The following paragraph(s) at a later amendment:T... Instructions for operation:1. For PA-28-161 with TAE 125-01installation:Anhang Flughandbuch für Piper PA-28-161 mit TAE 125 Installation;Ausgabe 1, Rev. 0 Approved March 8, 2004 or each later EASA approvedissue (see TM TAE 000-0004).Supplement Pilot's Operating Handbook for the Piper PA-28-161 Equi... 1. This STC supersedes LBA- EMZ SA 1377 and former EASA STC A.S.01632.2. Power/Rotational Speed:For TAE 125-01 and 125-02-99 installations:Take off power: 99 KW at 2300 min-1 (Propeller speed)Max. continuous power: 99 KW at 2300 min-1 (Propeller speed)For TAE 125-02-114 installations:Take off Power:M... 12/08/2019 Active 10014364 10014371 (EASA.A.S.01645) 365 AEROSPACE DDS LIMITED REV. 3 737-600/-700/-800/-900/-9 00ER Installation of an Enhanced Surveillance Mode S SystemRev 3: Transfer of STC from 365 Aerospace Ltd. to 365 Aerospace DDS Ltd. The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS 25 Amendment 1225.869, 25.1301, 25.1307, 25.1309, 25.1321, 25.1333, 25.1351, 25.1353,25.1355, 25.1357, 25.1431, 25.1529, 25.1581, 25.1701, 25.1703, 25.1705,25.1707, 25.... Aerospace Design & Engineering ConsultantsAFM Supplement 1 FMA-0014-001 Issue AAerospace Design & Engineering ConsultantsFlight Manual Supplement FMA- 1370-083 Revision 1or later revisions of the above listed document(s) approved/ acceptedunder the EASA system.Aerospace Design & Engineering Consultan... Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product. 05/08/2019 Active 10014371 10014372 (EASA.A.S.01646) AVIATION TRADERS LIMITEDEUROPE S.A.S. REV. 1 747-200 Introduction of a Litton 72R INS in a Boeing 747-200 seriesaircraftRev. 1: Transfer of STC The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... 1. Compliance Plan Inertial Navigation System - Litton LTN-72R, ATLdocument CP/037/9732, Issue 1.2. AFL AFM Supplement Number 39 Inertial Navigation System, ATL documentATL/747/M032, Issue 13. Engineering Order Inertial Navigation System -Litton LTN-72R, ATLdocument ATL/747/ EO032, Issue 14. Supplem... A copy of this Certificate and the EASA Approved Flight ManualSupplement (AFMS) must be maintained as part of the permanent recordsfor the modified aircraft.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviouslye... 09/11/2021 Active 10014372 10014373 (EASA.A.S.01647) LUFTHANSA TECHNIK AG REV. 3 DC-9, MD-88, MD-90-30 B717-200 Installation of non-electrical Floor Path Marking System Supplemental Type Definition Document STDD33-05/05M, issue 02 dated27/03/2006Airplane Flight Manual Supplement A-33-05/326- AFMApplicant's Declaration of Compliance dated 28/03/2006or later revisions of the above listed documents approved by EASA 31/01/2017 Active 10014373 Page 14 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014379 (EASA.A.S.01657) TUI AIRLINES BELGIUM N.V. REV. 1 757-200 MOD/757/1272, Installation of Security Cameras in accordance withThomson Airways Modification Summary MOD/ 757/1272 at issue 3.History: the EASA STC A.S.01657 (based upon CAA-UK Approval Note No.28803 issue 2) was granted to Britannia Airways Ltd on the 07 Dec. 2005.The STC Holder name then changed f... The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Thomson Airways Modification Summary MOD/757/1272 at issue 3or later revisions of the above listed documents approved by EASA. The FlightVu camera system must be selected ‘OFF’ for take- off andlanding.Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the air... 23/12/2016 Active 10014379 10014387 (EASA.A.S.01673) BUSINESS AND COMMUTER AIRCRAFT REV. 1 1900D Installation of a TCAS II System in accordance with Business & CommuterAircraft document BCA53-00, at revision 2, datedJune 25, 2015. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Aircraft Flight Manual Supplement Business & Commuter Aircraft documentBCA53-AFMS, at revision 1, dated April 02, 2015;or later revisions of the above listed documents approved byEASAInstructions for Continued Airworthiness Business & Commuter Aircraftdocument BCA53- ICA, at revision 0, April 04, 20... Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product. 25/06/2015 Active 10014387 10014389 (EASA.A.S.01675) GAMA ENGINEERING Ltd. REV. 1 CAA UK RESPONSIBIL ITY BAE.125 SERIES 800 Title: Upgrade of the dual Flight Management System (FMS).Description of change: The original dual Honeywell FMZ-900 FMS isupgraded to a dual Honeywell FMZ-2000 FMS. CS-25The Certification Basis for the original product remains applicable tothis certificate/ approval.The certificated noise and/ or emissions levels of the original productare unchanged and remain applicable to this certificate/ approval. Installed in accordance with Gama Engineering Ltd modificationHL/MOD/689, reference the Master Documents List (MDL), documentreference: MDL-689-01, Issue 1. Other technical documentation:Operation in accordance with Aircraft Flight ManualSupplement, documentreference: AFMS689001, Issue 2.Maintaind... The installer must determine whether this design change is compatiblewith previously approved modifications. 05/10/2012 Active 10014389 10014392 (EASA.A.S.01681) TÄBY AIRMAINTENANC E AKTIEBOLAG REV. 3 SAAB SF340A SAAB 340B Saab 340 Class E Cargo Compartment (as defined in document S21MDL-0033). This is a major change of the EASA STC EASA.A.S.01681. It isdesigned by STC Twenty One Limited and will document changes to thelocation of rapid decompression vents for planned future bulk cargoloading operations.This STC appro... The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval without any im... -,,S21 FMS-0013 issue 2 Flight Manual Supplement-,,S21 MMEL-0005 issue 1 Master Minimum Equipment List Supplement-,,S21TREP-00 64 issue 1 Mass and Balance Report-,,S21.TEC-0027 Supplement Manual lssue 4 - lnstructions for ContinuedAirworthiness-,,M aintenance Programme-,,Maintenance Manual-,,Wiring/S... This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraphs "Description" and"Associated Technical Documentation". Compatibility with otheraircraft/engine configurations shallbe determined by the installer. 17/02/2020 Active 10014392 10014398 (EASA.A.S.01692) LUFTHANSA TECHNIK AG REV. 2 BOEING 747-400 747-400 “Bahrain Royal Flight” VIP cabin installationRev 1: Replacement of conductive oxygen flex-hoses with non- conductiveones. Certificate renumbering from EASA.A.S.01692.Rev. 2: typo corrected The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:As per CRI A-1 Issue 1The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain appli... Generic documents:STDD 00-03/17M Issue 02 Rev 02VIP Cabin installation documents:AFM supplement A-00-05/319- AFM rev 02Instructions for continued airworthiness ICA-0-03/17 IssueOxygen hoses replacement documents:CPL-35-20/06M Rev 0or later revisions of the above listed document (s) approved/acceptedun... As per AFM supplement A-00-05/319-AFMPrior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviouslyinstalled change and/ or repair will introduce no adverseeffect upon the airworthiness of the product. 15/01/2021 Active 10014398 Page 15 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014403 (EASA.A.S.01698) GROWING ENGINEERING PARTNERS GmbH REV. 1 737-300 Reconfiguration of six Boeing 737-33V from 149TC to 16BC/100TC includinginstallation of G2, G7 and LAV ERev.1: Transferof STC from SR Technics Switzerland to groWINGEngineering Partners GmbH SR Technics (Irl) documentsC737-25-1024- CCS, Rev 3C737-25-1024- MDL-01, Rev 3 Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair willintroduce no adverseeffect upon the airworthiness of the product. 20/04/2021 Active 10014403 10014405 (EASA.A.S.01700) 365 AEROSPACE DDS LIMITED REV. 2 737-200/-300/-400/-500/-6 00 Installation of Dual High Frequency (HF) Communications SystemRev 2: Transfer of STC from 365 Aerospace Ltd. to 365 Aerospace DDS Ltd. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Aerospace Design <(>&<)> Engineering Consultants Modification SummaryMOD-0001 Revision B dated 16th May 2007 Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product. 05/08/2019 Active 10014405 10014408 (EASA.A.S.01703) AIRBUS TRANSPORT INTERNATIONAL SNC REV. 1 A300F4-608ST Installation of ISIS on A300-600STInstallation of two Integrated Stand-by Instrument System (ISIS) in replacement of the stand by speed, attitude and altitude. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Change Approval Sheet, ref: ST34MOD015 Issue 1AFM Supplement ref: ST34MOD015, dated 19 October 2006Change CertificationSynthesis: ST34MOD044_CCS Issue 3, dated 07.07.2016or laterrevisions of the above listed documents approved by EASA. This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.This certificate shall remain valid unless otherwise surrendered orrevo... 11/07/2016 Active 10014408 10014409 (EASA.A.S.01705) RUAG AEROSPACE SERVICES GmbH REV. 1 CESSNA 650 Upgrade of two existing Mode S transponders, Rockwell CollinsTDR-94D byRockwell Collins SB 501.Replacement of Mode S Controller CTL-92 by CTL-92E along withinstallation of new wiring for Enhances SurveillanceRevision 1 to include EASA AD 2009-0173, Rockwell Collins SBTDR-94D-34-509 to ensure correct... The Certification Basis for the original product remains applicable tothis certificate/ approvalThe requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval Master Document List 163A-MDL, Rev. A from 27 October 2010Airplane Flight Manual Supplement 163A-AFMS, Rev. A from 26 October 2010or later revisions of the above listed documents approved by EASA Aircraft Serial Numbers 650-7001 through 650-7119 29/10/2010 Active 10014409 10014411 (EASA.A.S.01708) TUI AIRLINES BELGIUM N.V. REV. 1 767-300 Introduction of BE Aerospace Spectrum Seat in accordance with ThomsonflyLtd Modification Summary MS/767/1462 issue 3.History: The STC certificate A.S. 01708 is re-issued because ThomsonAirways (previously known as Thomsonfly Ltd) part of the TUI Group,relinquishes and transfers the STC to another TUI... The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approvalThise... Thomsonfly Ltd Modification MOD/ 767/1462 issue 3or later revisions of the above listed documents approved by EASA. Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness ofthe product. 23/12/2016 Active 10014411 10014417 (EASA.A.S.01738) TÄBY AIRMAINTENANC E AKTIEBOLAG REV. 3 SAAB SF340A SAAB 340B Introduction of Alternate Cargo Net Location LayoutRev 1: to add an additional configuration that extends bay lengths byutilising nets installed only in five of the eight positions.Rev. 2: correction of typeRev. 3: Transfer of Certificate The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. EASA Approved:- STC Twenty One Ltd Flight Manual SupplementNo. S21.FMS-0014 Issue 6;- STC Twenty One Ltd Supplement Manual – ICA No. S21.TEC-0116 Issue 8;EASA Accepted:- STC Twenty One Ltd Master Document List No. S21. MDL-1508 Issue 2;orlater revisions of the above listed document(s) approved/ acc... This design change is applicable only to Saab SF340A and 340B aircraftconverted to Class E under STC Twenty One Limitedmajor changeS21.25-63-1015 approved under EASA STC 10014392(formerlyEASA.A.S. 01681).Prior to installation of this change/repair it must be determined thatthe interrelationship bet... 17/02/2020 Active 10014417 Page 16 of 1,974 12/11/2025 An agency of the European Union easa.europa.eu List of EASA Supplemental Type Certificates EASA STC no. STC Holder Rev. level Foreign/NAA STC ref. Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status System Record 10014422 (EASA.IM.A.S.01771) RUAG AG REV. 2 PILATUS PC-12/47 PILATUS PC-12/45 PILATUS PC-12 PC-12, PC-12/45 PC-12/47, PC-12/47E Installation of Dual Garmin GNS-530 COM/NAV/GPS SystemNote:This STC is the Revision 2 of EASA STC 2004-4674, dated 03/05/2004 The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval without any im... Engineering Technical Order TSA PC12-34.60.02EO Revision Cor later revisions of the above listed document(s) approved/acceptedunder the EASA system. This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph “Description”.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and... 01/02/2021 Active 10014422 10014423 (EASA.IM.A.S.02039) ISRAEL AEROSPACE INDUSTRIES, LTD.IAI REV. 5 CAA ISRAEL STC SA152 747-400 Conversion from Passenger to Special Freighter Configuration.Revision 1: Boeing 747-400SF conversion from PAX to Freighter CAAI STCSA152/EASA STC EASA.IM.A.S.02039Revision 2: Increase of Max. Taxi Weight and Max. Take-Off Weight from873.000 / 870.000 Lbs to 878.000 / 875.000 Lbs for aircraft with GE... The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Israel Civil Aviation Authority STC SA152 dated October 27,2006<(>,<)>- MDL: IAI MDL-366-00-00- A3673 Revision AL<(>,<)>- AFM-S 1: IAI Doc. No. 366-00-00-A3663-481 revision 1, October 24, 2012-Supplement to Airplane FlightManual D6U10002.481 for IAI B747-400SF with GE engines<(>,<)>- AFM-S 2: IAI Do... Refer to the limitation section of the applicable AFM Supplement asapproved for this STC depending on the serial numberof the aircraftPrior to installation of this design change it must be determined thatthe interrelationship between thisdesign change and any otherpreviously installed design chang... 08/04/2019 Active 10014423 10014426 (EASA.A.S.02471) ROEDER PRAEZISION GMBH REV. 1 441 Installation of Dual Mode S Transponder GTX 330D The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. - Engineering Order C441- NY-0124- AFM-S C441- NY-0124-08, Rev. 0, approved 14. February 2006, or laterEASA approved revision- Maintenance Procedures C441-NY-0124-07, Rev. 0, or later approvedrevision. 1. Limitation according AFM-S C441-NY-0124-082. Prior to installation of this design change it must be determinedthat the interrelationship between this design change and any otherpreviously installed design change and/or repair will introduce noadverse effect upon the airworthiness of the product.... 25/09/2017 Active 10014426 10014427 (EASA.A.S.02472) RHEINLAND AIR SERVICE GmbH REV. 3 208, 208B Installation of a FLIR System, Inc. Ultramedia III/HD television camera.New Pilot Operating Handbook Supplement PO-0023-250000.Rev. 3: Revision to account for the transfer from airplus engineeringGmbH to Rheinland Air Service GmbH. The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the product are unchangedand remain applicable to this certificate/ approval w... Master Document List MD-0023-000000 of 05 Feb. 2006 and test and certification reports listed in it.DOA Declaration of compliance DC-0023-250000 of Feb. 2006. VFR; no AP, Max speed (camera operation) 115 KIAS, 2 pilotsand max 4passengers (see POH Supplement for full Limitations text). 23/07/2025 Active 10014427 10014431 (EASA.A.S.02479) ALAMO ENGINEERING GmbH REV. 3 1124A Installation of Airborne Collision Avoidance System (ACAS II).Revision 1: Transfer to 328 DESIGN GmbHRevision 2: Transfer to 328 SUPPORT SERVICES GmbHRevision 3: Transfer to ALAMOEngineering GmbH The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:CS-25 Amdt. 1:CS 25.301, CS 25.303, CS 25.305, CS 25.307, CS 25.571, CS 25.603, CS25.605,CS 25.607, CS 25.609,CS 25.611, CS 25.1301, CS 25.1309, CS 25.1321, CS25.1322, CS... Avionics Mobile Services Modification AM/ 1486.Avionics Mobile Services AFM Supplement No. PART21-008/017 Revision -dated April 08 2005or later revisions of the above listed document(s) approved/acceptedunder the EASA system. This STC is approved only for the product configuration as defined inthe approved design data referred to in the paragraph "Description".Compatibility with other aircraft/engine configurations shall bedetermined by the installer.Prior to installation of this change/repair it must be determined thatt... 05/11/2024 Active 10014431 10014439 (EASA.A.S.02489) ROEDER PRAEZISION GMBH REV. 2 HAWKER 800/-800XP/-850XP BAE.125 SERIES 800A/-800B BAE.125 SERIES 1000A/-1000B Installation of wing mounted Xenon Taxi/ Landing Light and/or Radommounted Taxi Light The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. - Engineering Order H800- NY-0125-05- AFM-S H800- NY-0125-08,Rev 0 approved 07/04/2006- Maintenance Procedures H800-NY-0125-07, Rev 0or later revisions of the above listed documents approved by EASA. Prior to installation of this design change it must be determined thatthe interrelationship between this design change and any otherpreviously installed design change and/ or repair will introduce noadverse effect upon the airworthiness