Minor Change / Minor Repair

aircraft PARTENAVIAS P68of a console for reading of radio signals in a determined GPS position.These signals will be usedfor checking the accuracy of ground equipmentcalibration. 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 MDL001- Revision 1<(>,<) >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. 05/06/2020 Active 10077231 MINOR CHANGE ADANAIR S.L. B200 Installation of an ASIVE CONSOLE for calibration of external instruments 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... Installed and maintained in accordance with ASIVE SB002 Revision 1<(>,<)>or later revisions of the above listed document(s) approved/acceptedunder the EASA system. This design change only covers the installation of the SIVEconsole,wiring and antennas are installed in accordance with STC EASA 10077176.The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelatio... 09/09/2021 Active 10078273 MINOR CHANGE ADANAIR S.L. P.68 "OBSERVER", P. 68C-TC P.68 "OBSERVER 2", P. 68C P.68B "VICTOR" Installation of upgraded ASIVE console in the interior of Vulcanair P68Series, with the aim of capturing external radiosignals for checkingthe accuracy of ground equipment calibration 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... Installed and maintained in accordance with ASIVE SB003 Rev0 dated30/11/2021<(>,<)>or later revisions of the above listed document(s) approved/acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 08/02/2022 Active 10082031 MINOR CHANGE AERGRIFO S.R.L. 172RG Fireproof identification placard replacement 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... Doc. No. 01/23 – “Programma di Certificazione Progetto 01/23 Rev.1”dated 26/05/2023<(>,<)>or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. This modification is limited to aircraft S/N 172RG1062.The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or re... 01/06/2023 Active Page 2 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10082542 MINOR CHANGE AERGRIFO S.R.L. PA-28RT-201 (ARROW IV) Fireproof identification plate replacement 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... Doc. No. 02/23 – “Programma di Certificazione Progetto 02/23 Rev.0”dated 25/07/2023<(>,<)>or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. This modification is limited to aircraft S/N 28R-7918135.The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ ore... 03/08/2023 Active 10072968 MINOR CHANGE AERO AT Sp. z.o.o. AT-3R100 Removal of the errors noted in AFM 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 product are unchangedand remain applicable to this certificate/ approval without any impact... Revision No 24 dated 04.03 2020 to Airplane Flight Manual (AFM) Doc. NoATL3.03 (Polish language version) and Doc. No ATL3.04 (English languageversion)<(>,<)>Or later revisions of the above listed document(s) approved/acceptedunder the EASAsystem. None 03/04/2020 Active 10077570 MINOR CHANGE AERO CLUB (AE.C.) DI PADOVA F150J Installation of EASA STC 10040937 (validation of FAA STC SE7559SW) topermit use of a spin-on oil filter model TAF-Long Oil Filter on theReims Cessna F150J s/n F15000442. 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... Aero Club Padova Minor Change Certification Document No. ACPD- MC-02 RevA, dated 12/10/2021Stratus Tool Technologies, LLC Model TAF-L Oil Filter Adapter forContinental Engines C-75-12 Series, C-85-12 Series, C-90 Series, O-200Series Installation Instructions, document DN- ST007 Rev.-2, dated04.02.2020... Applicable only for aircraft Model Reims Cessna F150J, s/ n F150000442The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/ repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed cha... 28/10/2021 Active 10077591 MINOR CHANGE AERO CLUB (AE.C.) DI PADOVA F150L Installation of EASA STC 10040937 (validation of FAA STC SE7559SW) topermit use of a spin-on oil filter model TAF-Long Oil Filter on theReims Cessna F150L s/n F15001116 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... Aero Club Padova Minor Change Certification Document No. ACPD- MC-01 RevA, dated 12/10/2021Stratus Tool Technologies, LLC Model TAF-L Oil Filter Adapter forContinental Engines C-75-12 Series, C-85-12 Series, C-90 Series, O-200Series Installation Instructions, document DN- ST007 Rev.-2, dated04.02.2020... Applicable only for aircraft Model Reims Cessna F150L s/n F15001116The approval holder shall fulfill the obligations ofPart 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed chang... 03/11/2021 Active 10077727 MINOR CHANGE AERO CLUB (AE.C.) DI PADOVA F150J Installation of EASA STC 10040937 (validation of FAA STC SE7559SW) topermit use of a spin-on oil filter model TAF-Long Oil Filter on theReims Cessna F150J s/n F15000434. 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... Aero Club Padova Minor Change Certification Document No. ACPD- MC-03 RevA, dated 12/10/2021Stratus Tool Technologies, LLC Model TAF-L Oil Filter Adapter forContinental Engines C-75-12 Series,C-85-12 Series, C-90 Series, O-200 Series Installation Instructions,document DN- ST007 Rev.-2, dated 04.02.2020... Applicable only for aircraft Model Reims Cessna F150J, s/ n F150000434.The approval holder shall fulfill the obligationsof Part 21, Point21A. 109.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed ch... 19/11/2021 Active Page 3 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10078665 MINOR CHANGE AERO CLUB (AE.C.) DI PADOVA 182R REMOVAL OF VACUUM SYSTEM ON CESSNA 182R S/N 182-67749 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... Installed in accordance with ACPD-MC-04 Rev B dated 21/1/2022<(>,<)>or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. This design change is limited to the aircraft Cessna 182R s/n 182-67749Installation of EASA STC 10075856 is a precondition of this designchange<(>,<)>The equipment installed in accordance with EASA STC 10075856 must havebeen installed as the primary source for attitude and slip.The approval holder s... 22/02/2022 Active 10086899 MINOR CHANGE AEROCLUB COBURG F172N Maximum Take Off Weight increase to 2400 lbs. The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval.Thiscertificate/approval involves a change with an impact on the noisedatabase and/or emission levels. The environmental protectionrequirements are amended as follows:ICAO Annex 16 Vol... Absolute Pilots Supplement Airplane Flight Manual, documentAP- AFMS-172-1089-00 Revision 00,Revision date 2022-05-31Airplanes Installation Instructions document No.: 1722400-1, date June11, 1999.EASA Certification Noise Level is C13984.or later revisions of the above listed document (s) approved/accep... 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.The approval holder shall fulfil the obligations of Par... 11/04/2025 Active 10081592 MINOR CHANGE AERO CLUB COMO 172N Removal of Artificial Horizon and relevant Vacuum System 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: CS 23.601, 23.603,23.671, 23.771, 23.867, 23.1301, 23.1303, 23.1306, 23.1308, 23.1309,23.1311, 23.1321, 23.13... Doc. No. 01-AB-MC “MINOR CHANGE CERTIFICATION DOCUMENT FOR THE REMOVALOF VACUUM SYSTEM ON TEXTRON AVIATION INC. MODEL CESSNA 172N S/N 17269026REGISTRATION I-SAAB”, Issue A, Revision Bor later revisions of the above listed document(s) approved/acceptedunder the EASA system. This change is limited to S/N 17269026;This change requiresthe installation of uAvionixAV-30C components, inaccordancewith of EASA STC 10075856, latest approved revision;Aircraft operations are limited to VFR-Day only.The approval holdershall fulfill the obligations of Part 21, Point21A.109.Prior... 28/03/2023 Active 10081901 MINOR CHANGE AERO CLUB COMO 172N INSTRUMENT PANEL UPGRADE 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 later amendment: CS 23.301 (a), CS23.303, CS 23.305 (a)(b), CS 23.307 (a), CS 23.337 (a)(b), CS 23.561(a)(b,3)(e), CS 23.603... Doc. No. 02-AB-MC “Minor Change certification document for theInstrument Panel Upgrade on Textron Aviation Inc. Model Cessna 172N S/N17269026 Registration I-SAAB” Issue A, Revision 1, dated 27 April 2023<(>,<)>or later revisions of the above listed document(s) approved/ acceptedunder the EASA system.... This change is limited to S/N 17269026;This change requiresthe installation of:- uAvionixAV-30C components, in accordance with of EASA STC 10075856,latest approved revision;- Garmin G5 unit, in accordance with of EASA STC 10060846, latestapproved revision;- J.P. Instrument EDM 900, in accordance wi... 10/05/2023 Active 10075129 MINOR CHANGE AEROCLUB LOUIS BONTE DR 400/140 B Avionics upgrade on DR 400/140B aircraft S/N 2086Installation of Garmin GTN650 and related modifications for VFRoperations The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- The following paragraph(s) at a later amendment:23.1301(a),23.1301 (b), 23.1301(c), 23.1301(d), 23.1309(e), 23.1361(a), 23.1365,23.1367(d), 23.1431(b), 23.1519 from CS23... Definition of modification in accordance with section 3 of ACLB_MC_001Revision 1.1Installation in accordance with section 4 of ACLB_MC_001 Revision 1.1Instruction for continued airworthiness in accordance with section 5 ofACLB_MC_001 Revision 1.1Operation in accordance with section 6 and Appendix 1R... This modification only applies to aircraft S/N 2086.The approval holder shall fulfill the obligations of Part 21, Point21A.109. 10/12/2020 Active Page 4 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10084672 MINOR CHANGE AEROCLUB LOUIS BONTE DR 400/2+2 UAVIONIX AV-30-C Installation 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 Amendment 4,,23.301 - 23.305 - 23.307 - 23.1301 - 23.1309 - 23.1351 - 23.1357 -23.1365 - 23.1431 - 23.1581.The req... Change dossier ACLB_MC_002 Revision 1.1 dated 11 June 2024< (>,<)>Or later revisions of the above listed document (s) approved/ acceptedunder the EASA system. Limited to DR 400 MSN 1966.The approval holder shall fulfill the obligations of Part 21, Point21.A.109.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 adv... 11/06/2024 Active 10083445 MINOR REPAIR AERO-CLUB MARCEL DASSAULTLOUIS BREGUET DR 400/180 Fuel Selector Repair 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... Technical Repair Dossier FGGHT Le Bozec A7089_Revision 03 dated 06December 2023<(>,<) >Or later revisions of the above listed document(s) approved/acceptedunder the EASA system. DR 400/180 Manufacturer Serial Number (MSN) 1846.The approval holder shall fulfill the obligations of Part 21,21.A.451 (b).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 wil... 07/12/2023 Active 10074228 MINOR CHANGE AERO CLUB NATIONAL DU PERSONNELDES INDUSTRIES ELECTRIQUE ET GAZIER(ANEG) PA-28-181 (ARCHER III) Installation of four (4) Cylinder Head Temperature (CHT) and Exhaust GasTemperature (EGT) probes along with cabling anda circuit breaker tosupport installation of a graphic engine monitoring instrument. 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... Minor change description F-GYNN, compiled by Patrick Bezault, Revision0, dated 9 September 2020or later revisions of the above listed document(s) approved/acceptedunder the EASA system. This design change approval does not allow replacement of existingengine instruments.This design change approval excludes installation of any graphic enginemonitoring instrument.Graphic engine monitoring instrument may be installed if specificallyapproved by an EASA design approval or allowed by CS-... 10/09/2020 Active 10081484 MINOR CHANGE AEROCLUB PARIS SUD 172M Instrument Panel Refurbishment 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... Installed in accordance with Doc.-No. ACPS-005 – FBXQQ rev C dated11/03/2023 Cessna 172 S/N 17265685 to 17275759 and Reims-Cessna 172,S/N 1385 to 2194The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously insta... 14/03/2023 Active 10083833 MINOR CHANGE AEROCLUB PARIS SUD FRA150M FRA150L FA150M FA150L FA150K F150M F150L F150K Instrument panel refurbishment 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... Certification Program No. ACPS-007, rev. F, dated 01/02/2024;Aircraft Flight Manual Supplement ACPS-007, rev. A, dated 29/01/2024;or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Applicable to Cessna 150 aircraft from serial number 15071129 to15077005, Reims- Cessna F150 aircraft from serial F15000530 to F15001248and Cessna FA150 aircraft from serial numberFA1500001 up to serialFA1500281The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to insta... 02/02/2024 Active Page 5 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10079335 MINOR CHANGE AEROCLUBUL ROMANIEI IS-29D Change of Instrument PanelChange of Flight Instruments/ VHF/ Transponder 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... Upgrade of instruments and instrument panel in accordance withAeroclubul Romaniei (AR) change dossier document AR. 29D2.11.03.1007,dated May 2019;Aircraft Flight Manuel Supplement, AR doc. AR.29D2.11.03.1004, datedMay 2019;Maintenance Manual Supplement, AR doc. AR. 29D2.11.03.1004, dated May2019;... None 23/05/2022 Active 10073818 MINOR CHANGE AERODESIGN AND MANUFACTURIN GTECHNOLOGY S.L. ATR 72-212 A Installation of TELEX boomsets in ATR72 Cockpit for the observer seat 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 product are unchangedand remain applicable to this certificate/ approval without any impact... INSTALLATION INSTRUCTIONS MOBT-1828-INS01, Revision 3CMM SUPPLEMENT MOBT-1828-CMMS01 Revision 1Or 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... 16/07/2020 Active 10077177 MINOR CHANGE AERODESIGN AND MANUFACTURIN GTECHNOLOGY S.L. ATR 72-212 A ATR 72-212 ATR 72-211 ATR 72-202 ATR 72-201 Introduction of Alternative Boomsets for the Flight Crew 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 product are unchangedand remain applicable to this certificate/ approval without any impact... MASTER DATA LIST MOBT-2015-MDL Rev.01 (31/08/2021)Or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. This approval is only applicable to the following Aiprlanes:AIRPLANES ATR 72 Series; MSN 234, 171, 192, 204, 207, 330, 416, 147,150, 274, 446, 494, 498, 550, 568, 595, 763, 809, 824AIRPLANES ATR 42 Series; MSN 141, 218, 231, 242, 254, 321 (ATR-42) The approval holder shall fulfill the obligations of2... 02/09/2021 Active 10078026 MINOR CHANGE AERODESIGN AND MANUFACTURIN GTECHNOLOGY S.L. EMB-120RT External Emergency Lights SubstitutionThis modification removes the overwing external emergency lights onEMB-120 in freighter configuration, and install a metal cover plate. 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... - MDL MOBT-2119-MDL Rev. 00 “External emergency lights substitution bycover plate In EMB-120”or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Aircraft previously modified according to FAA STC ST00598WI, dated 14November 1997The approval holder shall fulfill theobligations of Part 21, Point21A.109.Prior to installation of this change/ repair it must be determined thatthe interrelationship between this change/repair and any otherpreviouslye... 20/12/2021 Active 10078028 MINOR CHANGE AERODESIGN AND MANUFACTURIN GTECHNOLOGY S.L. EMB-120RT EMB-120ER EMB-120 Introduction of Alternative Boomset P/ NsThe purpose of thismodification is to change boomsets installed onaircraft EMB120 to new alternative boomsets with Active Noise Reduction(ANR). 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 Data List MOBT-2110-MDL Rev. 00 “INTRODUCTION OF ALTERNATIVEBOOMSET (TELEX) P/NS FOR THE EMB 120 COCKPIT”or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109. 20/12/2021 Active Page 6 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10078238 MINOR CHANGE AERODESIGN AND MANUFACTURIN GTECHNOLOGY S.L. ATR 72-212 A Introduction of Alternative Jack Panel and Boomset P/Ns 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 DATA LIST MOBT-2124-MDL Rev. 00< (>,<)>or later revisions of the above listed document (s) approved/ acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 01/02/2022 Active 10079649 MINOR CHANGE AERODESIGN AND MANUFACTURIN GTECHNOLOGY S.L. ATR 72-212 A Installation of HEPA filterThis modification consists in installing an HEPA filter in therecirculation fan on aircraft The Type and OSD Certification Bases for the original product remainsapplicable 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 witho... MASTER DATA LIST MOBT-2009-MDL REV 01Or later revisions of the above listed document(s) approved/acceptedunder the EASAsystem. 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... 06/07/2022 Active 10081218 MINOR REPAIR AERODESIGN AND MANUFACTURIN GTECHNOLOGY S.L. ATR 72-212 A ATR 72-211, ATR 72-212 ATR 72-201, ATR 72-202 ATR 72-101, ATR 72-102 COUPLING RING REPLACEMENT IN AIR COOLING SYSTEM DUCTS 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 Data List REBT-1906-MDL Rev. 05 dated 23/01/2023. This approval supersedes the previous certificate 10069237 originalissues in its entirety. Earlier versions of repair REBT-1906 are notanymore authorized to be applied.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any other... 09/02/2023 Active 10082463 MINOR CHANGE AERODESIGN AND MANUFACTURIN GTECHNOLOGY S.L. ATR 72-212 A REPLACEMENT OF COUPLING RINGS INSTALLED IN THE DUCTS OF THEAIR-CONDITIONING AIR-COOLING SYSTEM. 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 Data List, Ref. MOBT-2218-MDL, Rev. 01, Date: 13.06.2023Service Bulletin, Ref. MOBT-2218- SB00, Rev. 00, Date: 17.02.2023Or 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... 26/07/2023 Active 10072386 MINOR CHANGE AERO ENGINEERING SERVICES ATR 72-212 A ATR 72-101/-102/-211/-212 ATR 42-200/-300/-320/-400/-50 0 Owner and Registration Plates Installation 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 Amdt 4 - CS25.29; CS 25.561(b); CS 25.603; CS 25.1529; CS 25.1541 and CS 25.1557(b)& (c)The requirements for environ... - Project Opening Sheet P00968-POS-001 Revision 00 dated 04February2020- Certification Report P00968-CR-001 Revision 00 dated 04 February 2020- Master Data List P00968-MDL-001 Revision 00 dated 04 February 2020- Service Bulletin P00968-SB-001 Revision 00 dated 04 February 2020or later revisions ofu... ATR 42 and ATR 72 all MSN.The approval holder shall fulfillthe obligations of Part 21, Point21A.109.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 advers... 05/02/2020 Active Page 7 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10073317 MINOR CHANGE AERO ENGINEERING SERVICES CL-600-2E25 (RJ SERIES 1000) CL-600-2C10 (RJ 700, 701, 702) Live Animals Cargo Stowage Installation 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 Amdt 4 - CS25.29; CS 25.301; CS 25.303; CS 25.305; CS 25.307; CS 25.321; CS 25.333;CS 25.337; CS 25.341; CS 25.365;2... - Project Opening Sheet P00592-POS-001 Revision 00 dated 19May 2020- Service Bulletin P00592- SB-001 Revision 00 dated 19 May 2020or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. CL-600-2C10 MSN 10032; 10036; 10037; 10089; 10093; 10096; 10198; 10245;10263 to 10265 included, and<(>,<) >CL-600-2E25 MSN 19004; 19006; 19007; 19009; 19010; 19012 to 19019;19023; 19024 and 19041.The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of thist... 29/05/2020 Active 10073598 MINOR CHANGE AERO ENGINEERING SERVICES 737-400 Galley Area Flight Crew Stowage Installation 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 Amdt 4 - CS25.29; CS 25.301; CS 25.303; CS 25.305;CS 25.307; CS 25.321; CS 25.337; CS 25.341; CS 25.365; CS 25.561(b... - Project Opening Sheet P00645-POS-001 Revision 00 dated 23June 2020- Service Bulletin P00645- SB-001 Revision 00 dated23 June 2020or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Limited to B737-400 MSN 24709; 25063; 25180 and 25595.The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or rep... 25/06/2020 Active 10083901 MINOR CHANGE AERO ENGINE ITALY SRL O-200-C O-200-B O-200-A Additional Crankcase Oil Sealing for Continental O-200-A, -B, -C models 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... O200P001-CMC-00 Compact Minor ChangeO200P001-Sbt-00 Issue 0Installation Service BulletinO200P001-ICA-00 Issue 0 Instruction for Continued Airworthinessor later revisions of the above listed document(s) approved/acceptedunder the EASA system. None 14/02/2024 Active 10079868 MINOR CHANGE AERO GROUP S.A. P2012 TRAVELLER Skynode S100 InstallationInstallation of a satellite tracking system Latitude SkyNode S-100 withcombined antenna GPS L1/Iridium model S5GIR1516RR- A2P-XTT-1. 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 product are unchangedand remain applicable to this certificate/ approval without any impact... - AG-DOC-23 Minor Certification Skynode S100_HB-LVS, Rev. 1- Instructions for continued airworthiness: Doc. No. 2022-094-ICA Rev. 0 S/N 050 (HB- LVS)The approval holder shall fulfill the obligations of Part 21, Point21.A.109.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... 03/08/2022 Active 10079948 MINOR CHANGE AERO GROUP S.A. M20R Ground clearance system installation 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... Minor Change Certification Document No. AG-DOC-23 Rev 1, dated07.07.2022Flight Manual Supplement, document No. 2021-93- AFMS Rev 0, dated14.01.2022Instruction for Continued Airworthiness, document No. 2021-93-ICA Rev 0,dated 14.01.2022or later revisions of the above listed document(s) approved/ accept... Only applicable to Mooney M20R aircraft S/N 29-0034.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 airworthiness of the product. 17/08/2022 Active Page 8 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10082347 MINOR CHANGE AERO GROUP S.A. 208B FLARM External antennas installation on CESSNA 208B S/N 208B-5183 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... Minor change certification document for: External antennas installation,Ref: 2023-016-MCA-1 Revision 1, dated 29 JUNE 2023.or later revisions of the above listed document(s) approved/acceptedunder the EASA system. S/N 208B-5183The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/ repair it must be determined thatthe interrelationshipbetween this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffect upon... 07/07/2023 Active 10087062 MINOR CHANGE AERO GROUP S.A. B200 Installation of an Iridium satellite telephone and trackingsystem,model Latitude S200-021 with remote cockpit dialer PTA12-100, replacingthe existing model Latitude S100-001 system. 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... Latitude Installation and Operation Manual for Skynode S200TrackingSystem P/N: S200-021,Document No. S200-402, Revision 2.10, September 10, 2019, or laterrevision.NAT Installation and Operation Manual for NAT PTA12-100 POTS TelephoneAdapter, REV. 4.00 or later revision.Aero Group Drawings:Skynode 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.The approval holder shall fulfil the obligations of Par... 12/05/2025 Active 10087279 MINOR CHANGE AEROKLUB GLIWICKI SZD-9 BIS 1 E "BOCIAN" SEE EASA APPROVED MODEL LIST Nicopress - SZD-JeżówThe minor change is for usage of Nicopress crimping sleeves for crimpingcontrol cables in SZD Gliders included in „Jeżów sailplanes” TypeCertificate. 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... - Minor Change Certification Document for SZD-Jezow Gliders<(>,<) >Doc. No. 1/AGL/MCC/ 2025, Issue 1, 06 May 2025.- Instrukcja obciskania linek i połączenia przy pomocy tulejekzaciskowych - NICOPRESS<(>,<) >Instructions for crimping cables and connecting them with crimpingsleeves - NICOPRESS<(>,<)>Dok.... The approval holder shall fulfill the obligations of Part 21, Point21.A.109.Prior to installation of this change/ repairit must be determined thatthe interrelationshipbetween thischange/repair and any other previously installed changeand/ or repair willintroduce no adverse effect upon the airworthi... 10/06/2025 Active 10087535 MINOR CHANGE AEROKLUB GLIWICKI 182H Cessna 182H MODIFICATION FOR AIRDROP (Fox vaccines)The modification is related to a luggage door, on left side of thefuselage, in which will be cut the hole for vaccinations drop.Inbaggage compartment, will be mounted the metal table and line tubeconnecting the table with the hole in luggage door.w... The Type and OSD Certification Bases for the original product remainsapplicable 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 witho... -Minor Change Certification Document for Cessna 182H “Fox Operation”,Doc No. 182H/KEM/2025MC, Issue 0, dated 03 JUN 2025.- Flight Manual Supplement to the FAA Approved 182H OWNER’SMANUAL “Foxvaccination operation equipment”, Doc No. AFM/ 182H/KEM/2025MC, Issue 0,dated 03 JUN 2025. The approval holder shall fulfill the obligations of Part 21, Point21.A.109.Cessna 182H, S/ N 18256425, Reg. OK-KEM 09/07/2025 Active 10088251 MINOR CHANGE AEROKLUB GLIWICKI SEE EASA APPROVED MODEL LIST Nicopress - PW-5, PW-6The minor change is for usage of Nicopress crimping sleeves for crimpingcontrol cables in the PW-5 and PW-6 sailplanes. See appendix to TVThe 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 impact onthe noise database. -Minor Change Certification Document for PW-5 and PW-6 gliders<(>,<)>Doc. No. 2/AGL/MCC/2025, Issue 0, 11 July 2025.- Instrukcja obciskania linek i polaczenia przy pomocy tulejekzaciskowych - NICOPRESS<(>,<) >Instructions for crimping cablesand connecting them with crimpingsleeves - NICOPRESS<(>,<)>1... 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... 07/10/2025 Active Page 9 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10083352 MINOR CHANGE AERO MAINTENANCE AUVERGNE P.68C Installation of an electronic ignition system (EIS) 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... Report No. P.68C-EIS “Dossier de Modification Mineure Application duSI1569 Ind. B sur un Vulcanair P.68C”, Issue C, dated 22/11/2023<(>,<)>or later revisions of the above listed document(s) approved/acceptedunder the EASA system. This Change is applicable only to Aircraft S/N 402.The approval holder shall fulfill the obligations of Part 21, Point21A.109.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... 27/11/2023 Active 10074073 MINOR CHANGE AEROMECANIC DHC-6 SERIES 300 Installation of two Garmin GSB 15 USB charging hubs on pilot andco-pilot sub panels. 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... Dossier Technique de Modification Aeromecanic/ 20/001/DHC-6/GSB-15, Rev0, date 07/2020.or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Only applicable to S/N 557 and S/N 696.The approval holder shall fulfill the obligations of Part 21, Point21A.109.Priorto installation of this change/repair it must be determinedthatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introd... 20/08/2020 Active 10081957 MINOR CHANGE AEROMECANIC F90 GNS530W - ILS/GPSDisconect the ILS Energize from the GNS 530W P5006 and connect toILS/GPS on GNS 530W P5001 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 later amendment: CS23.2005 Amd 5,CS23.2510 Amd 5.The requirements for environmental protection and the associatedcertified n... Sabena/23/001/f90/ GNS530W<(>,<)>or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Limited to MSN LA 113.The approval holder shall fulfill theobligations of Part 21, Point21A.109.Prior 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 adverseeff... 17/05/2023 Active 10072918 MINOR CHANGE AERO MECANIC'S CAP10B MINOR CHANGE CERTIFICATION DOCUMENT FOR THE EDM730/830 INTEGRATION INCAP 10 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... Doc N°2018-00461 Issue 05 dated 27/03/2020<(>,<) >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. 30/03/2020 Active 10075455 MINOR CHANGE AERO MECANIC'S CAP10B EDM730/830 INSTALLATION 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 product are unchangedand remain applicable to this certificate/ approval without any impact... Technical Dossier 2018-00461 Issue 6 dated 11 January 2021Or 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... 25/01/2021 Active 10078638 MINOR CHANGE AERO MECANIC'S CAP10B Installation of Garmin GI275 - CAP10B - F-HNLB 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... Installed, operated, and maintained in accordance with documents listedin:Minor Change Certification Document MOD_F-HNLB-01 Rev 4.3 dated14/02/2022 Limited to S/N 70The approval holder shall fulfill the obligations of Part 21, Point21A.109.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 u... 17/02/2022 Active Page 10 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10075208 MINOR CHANGE AERO MEDIA Kft. F172F This Minor Change Approval approves the use of FAA STC SA4428SW for theInstallation of 180 Horsepower Lycoming engine 0-360-A4M and propellerSensenich 76EM8S14-0-60 to Reims builtCessna F172F serial number 0140. The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection are unchanged but thiscertificate/ approval involves a change with an impact on the noisedatabase and/or emission levels. Installation, operation and maintenance in accordance with the datacontained in FAA STC SA4428SW and Aero Media Kft. Minor ChangeCertification Document for Cessna F172F HA-SLF, document 01-2020, IssueA, date 15/12/2020.Noise record C14434or later revisions of the above listed document (s) approved/ac... Applicable only to aircraft S/N 0140The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior toinstallation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce... 15/12/2020 Active 10084388 MINOR CHANGE AERONAVA CABIN INTERIORS S.R.L. A319-112, A320-214 Bose A30 Headset InstallationReplacement of existing Bose A20 Headsets with new Bose A30 Headsets. 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 later amendment: CS 25.1, CS 25.25, CS25.27, CS 25.601, CS 25.603, CS 25.611, CS 25.771, CS 25.773, CS25.1301, CS 25.1302, C... . The change is defined with Revision 2 of Aeronava Master Data ListMDL_AER021019.. The aircraft shall be maintained inaccordance with Revision 2 ofAeronava Instructions for Continued Airworthiness documentICA-AER021019.. The OSD-Flight Crew Data per the CS-FCD issue 2 is contained by thedocuments:... 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. 03/05/2024 Active 10087802 MINOR CHANGE AEROPHILE S.A.S. AEROPHILE 5500 Introduction of Photocatalytic Lacquer and update of theScientific-platform. The Type and OSD Certification Bases (CB) for the original productremains applicable to this certificate/ approval. Aerophile SAS Master Document List (MDL) Issue 1, Rev. 0, dated July29th 2025or 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.The approval holder shall fulfil the obligations of Par... 18/08/2025 Active 10073685 MINOR CHANGE AEROPUBBLICITA VICENZA S.R.L. F150K Installation of Pacific Aerial Tow Hook, Tow Bar and SafetyTow Link inaccordance with FAA STC SA220SO 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... Installation, maintenance and operation in accordance with AML SA220SO,Mater Drawing List FWI660-90 Rev B dated 20/12/2017 Component Manual andInstructions for Continuous Airworthiness FW-FWI660-13 Rev IR dated1/5/2017or later revisions ofthe above listed document(s) approved/ accepted onbehalf of E... Limited to Reims Cessna F150K Serial Number 0597The approval holder shall fulfill the obligations of Part 21, Point21A.109.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 wi... 02/07/2020 Active 10088288 MINOR CHANGE AERO R & Dd/b/a AEROPHOTONAV MBB-BK117 D-3M MBB-BK117 D-3 MBB-BK117 D-2 AéroPhotoNav System (Supplementary information display) 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... Minor Change Dossier AERO R<(>&<) >D_AeroPhotoNav_001 Supplementaryinformation display for Day VFR operation Edition 9 dated 10/09/2025;Maintenance Manual Supplement AeroPhotoNav Revision 0 dated 10/09/2025;Flight Manual Supplement AeroPhotoNav Revision 0 dated 10/09/2025;Service Bulletin Dossier AER... The AeroPhotoNav must not be used for navigation purposes or relied uponas a primary system for operating the rotorcraft.The AeroPhotoNav shall only be used for day VFR operations.No other items of equipment are permitted to be installed in the rearlower avionics compartment when the AeroPhotoNav sy... 08/10/2025 Active Page 11 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10080643 MINOR CHANGE AERO RESTAURATION SERVICE DR 253 GTN650Xi Installation 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... Certification Program GTN650Xi Installation Revision 0 dated 07 November2022<(>,<)>Or later revisions of the above listed document(s) approved/acceptedunder the EASA system. CEAPR DR 253 Manufacturer Serial Number (MSN) 110.The approval holder shall fulfill the obligations of Part 21, Point21.A.109.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... 17/11/2022 Active 10081076 MINOR CHANGE AERO RESTAURATION SERVICE F260, F260B Fuel selector replacement on F260 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: CS 23.305, CS 23.603,CS 23.605, CS 23.613, CS 23.777, CS 23.951, CS 23.993, CS 23.995, CS23.1301, CS 23.1309T... Doc. No. ARSMOD2022-004 “Minor Change Certification Programfor Fuelselector replacement on SIAI Marchetti F260 S/N 1-01 to 3-190”, revision5, dated 16/01/2023or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. This change is applicable to F260 aircraft MSN from 1-01 to3-190The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship betweenthis change/repair and any otherpreviously installed changee... 18/01/2023 Active 10078251 MINOR CHANGE AERO SERVICE ROMANS DR 400/180 Installation of AV-30C – F-GIKD - DR400/180 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... Installed, operated<(>,<)> and maintained in accordance with documentslisted in:Minor Change Certification Document: Doc. No. MC-001, Issue A Revision1, Dated 02/11/2021 Limited to S/N 1914, installation may not be performed as part of anintegrated autopilot system, including heading bug interface, attitudesource or flight director display.Installation may not be performed as a replacement of a HorizontalSituational Awareness Indicator (HSI).In installations where t... 03/02/2022 Active 10078252 MINOR CHANGE AERO SERVICE ROMANS DR 400/140 B Installation of AV-30C – F-GORG - DR400/140B 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... Installed, operated<(>,<)> and maintained in accordance with documentslisted in:Minor Change Certification Document: Doc. No. MC-002, Issue A Revision1, Dated 02/11/2021 Limited to S/N 1034, installation may not be performed as part of anintegrated autopilot system, including heading bug interface, attitudesource or flight director display.Installation may not be performed as a replacement of a HorizontalSituational Awareness Indicator (HSI).In installations where t... 03/02/2022 Active 10081325 MINOR CHANGE AERO SERVICE ROMANS DR 400/140 B Attitude and Directional Indicator ReplacementChange is removing vacuum driven attitude indicator and directional tofitin place two Uavionix devices AV-30C. (i.a.w ESASA STC 10075856). 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 amendment 423.301 No change, 23.305 No change, 23.307No change, 23.1301 Equipment STC 10075856 approved, 23.1309 N... AV-30-C Flight Manual Supplemental UAV-1004044-001 Rev CAV-30-C Installation Manual UAV-1003947-001 Rev EAV-30-C Instructions for Continuous Airworthiness UAV-1004045-001 Rev AAV-30-C Service Bulletin upgrade to 2.1.5 UAV-1005689-003 Rev AAV-30-C spec.Minor Change Certification Document ref : ASR-22... Limited to MSN 1191.Prior to installation of this change/repair it must be determined thatthe interrelationship betweenthis change/repair and any otherpreviously installed changeand/ or repair will introduce no adverseeffect upon the airworthiness of the product. 22/02/2023 Active Page 12 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10081402 MINOR CHANGE AERO SERVICE ROMANS DR 400/140 Attitude and Directional Indicator ReplacementChange is removing vacuum driven attitude indicator and directional tofitin place two Uavionix devices AV-30C. (i.a.w ESASA STC 10075856). 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 amendment 4-23.301 No change-23.305 No change-23.307 Nochange-23.1301 Equipment STC 10075856 approved-23.1309 No ch... AV-30-C Flight Manual Supplemental UAV-1004044-001 Rev CAV-30-C Installation Manual UAV-1003947-001 Rev EAV-30-C Instructions for Continuous Airworthiness UAV-1004045-001 Rev AAV-30-C Service Bulletin upgrade to 2.1.5 UAV-1005689-003 Rev AAV-30-C spec.Minor Change Certification Document ref: ASR-23-... Limited to MSN 1688The approval holder shall fulfill the obligations of Part 21, Point21.A.109.Prior to installation ofthis change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffec... 07/03/2023 Active 10082270 MINOR CHANGE AERO SERVICE ROMANS DR 220 A Installation of AV30-C 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... Minor Change Certification Document: Doc. ASR-22-12-3638 Rev. 3-1, dated27/06/2023or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Limited to aircraft s/n 91, For VFR-day only;Installation may not be performed as part of an integrated autopilotsystem, including heading bug interface, attitude source or flightdirector display.Installation may not be performed as a replacement of a HorizontalSituational Awareness Indicator (HSI).... 29/06/2023 Active 10084308 MINOR CHANGE AERO SERVICE ROMANS DR 400 RP, DR 400/100 DR 400/2+2, DR 400/200 I DR 400/200 R, DR 400/500 DR 400/180 R, DR 400/180 S DR 400/160 D, DR 400/180 DR 400/140 B, DR 400/160 DR 400/125I, DR 400/140 DR 400/125, DR 400/120 D DR 400/120, DR 400/120 A DR 360, DR 380, DR 400 NGL DR 300/180 R, DR 315, DR 340 DR 300/125, DR 300/140 DR 300/108, DR 300/120 DR 250, DR 250B, DR 250B-160 DR 250-160, DR 253, DR 253B DR 220B, DR221, DR 221B DR 200, DR 220, DR 220AB UAVIONIX AV-30-C ON DR253 SN 109Installation of 2 Uavionix AV-30-C in place of pneumatic attitude anddirectional 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 Amendment 423.301, 23.305, 23.307, 23.1301, 23.1309, 23.1351, 23.1357, 23.1365,23.1431 and 23.1581.The requirement... F-BPCC – AV30-C Minor change Certification for CEAPR DR253 MSN 109< (>,<)>Or later revisions of the above listed document (s) approved/ acceptedunder the EASA system. Limited to MSN 109.The approval holder shall fulfill the obligations of Part 21, Point21.A.109.Prior to installation ofthis change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffec... 17/04/2024 Active Page 13 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10088403 MINOR CHANGE AEROSPACE MANAGEMENT & SUPPORT G. P 60 55C 55B 55 36A 36 35A 35 31A 31 25F 25D 25C 25B 25 24F-A 24F 24D-A 24D 24B-A 24B 24A 24 Replacement of portable HALON fire extinguishers with HALON-free fireextinguishers 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 Ref F-MDL-04647 rev 01 dated 15/10/2025Instructions for continuous airworthiness Ref AMS-DO-F-ICA-04647 rev 01dated 23/9/2025Flight Manual supplement Ref AMS-DO- F-AFM-04647 rev 1 dated 15/10/2025or later revisions of the above listed document(s) approved/ acceptedunder the EASA s... The approval holder shall fulfil the obligations of Part 21, Point21A.109.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 airworthin... 23/10/2025 Active 10072698 MINOR CHANGE AEROSPOOL, SPOL. S R.O. CLUB Installation of equivalent model of ACL/ NAV/POS Lights and modificationof the Brake System filling/bleeding with hydraulic fluid. 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... AS-RTC-20-005, Certification Document of Minor Change No. DCH005,Exterior Lights – equivalent, Modification of Brake System, Revision 1,dated 03 March 2020.or later revisions of the above listed document(s) approved/acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 09/03/2020 Active 10072699 MINOR CHANGE AEROSPOOL, SPOL. S R.O. CLUB Installation of ELT model Kannad AF INTEGRA. 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... AS-RTC-20-006, Certification Document of Minor Change No. DCH006, ELTKannad AF INTEGRA, Revision 1, dated 03 March 2020.or later revisions of the above listed document(s) approved/acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 09/03/2020 Active 10073873 MINOR CHANGE AEROSPOOL, SPOL. S R.O. CLUB Replacement of fuel pressure sensor and oil hose 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... Modification in accordance with: Certification document of minor changeDCH007, AS-RTC-20-007, initial revision.or laterrevisions of the above listed document (s) approved/ acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 24/07/2020 Active 10073878 MINOR REPAIR AEROSPOOL, SPOL. S R.O. CLUB Repair of cut-out edge of vertical stabilizer skin 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... Repair in accordance with: Service Bulletin SBRTC-2020-4, initialrevision.or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21,21.A. 451(b).Prior to installation of this change/repair itmust be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffect upon the airworthine... 24/07/2020 Active Page 14 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10074200 MINOR CHANGE AEROSPOOL, SPOL. S R.O. CLUB Replacement of Traffic Information SystemTRX-1500 (GarrechtAvionik GmbH) is replaced by AT-1 (Air Avionics). 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... Installed in accordance with: Servise Bulletin SBRTC-2020-7Operated in accordance with: Supplement No.001, AS- POH-01-001, revision4or later revisions of the above listed document(s) approved/acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 07/09/2020 Active 10075525 MINOR CHANGE AEROSPOOL, SPOL. S R.O. CLUB DCH009: Unification of Structure Configuration. Modification of ThrottleControl. Change of adhesive and resin in secondary structure. 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... Installed in accordance with: . AS-TC-20-009, rev 0, dated 20/01/2021 . SBRTC-2020-8, initial revision.Operated in accordance with: . Pilot’s Operating Handbook: AS- POH-01-000, rev 5, dated24/11/2020 . Supplement 12: AS- POH-01-012, rev 0, dated 24/11/2020 . Supplement 3: AS-... The approval holder shall fulfill the obligations of Part 21,21.A. 451(b).Prior to installation of this change/repair itmust be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffect upon the airworthine... 01/02/2021 Active 10075666 MINOR CHANGE AEROSPOOL, SPOL. S R.O. CLUB DCH010: Approval of minor changes with differences between seriallyproduced aircraft and serial No. DY-444/2012 LSA 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... -Change definition document: AS-TC-20-010, Revision 0, Certificationdocument of minor change No. DCH010- SBLSA-930-2021,revision 1.or later revisions of the above listed document(s) approved/acceptedunder the EASA system. Limited to S/N DY-444/2012 LSAThe approval holder shall fulfill the obligations of Part 21, Point21A.109.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 ad... 18/02/2021 Active 10076975 MINOR CHANGE AEROSPOOL, SPOL. S R.O. CLUB DCH011: Approval of optional throttle controller and updateof Pilot’sOperating Handbook and Aircraft Maintenance Manual 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... - Type design definition: Annex 1 – Type Design Definition,AS- RTC-15-001.A1, revision 18, dated July 2021- Operated in accordance with: Pilot’s Operating Handbook,AS- POH-01-000, revision 6, dated April 2021- Instructions for continued airworthiness in accordance with:AS- AMM-01-000, revision 6, dated... The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 22/07/2021 Active 10080503 MINOR CHANGE AIR AMBULANCE TECHNOLOGY GmbH CL-600-2B16 (604 VARIANT) CL-600-2B16 (601-3R VARIANT) CL-600-2B16 (601-3A VARIANT) CL-600-2A12 (601 VARIANT) CL-600-1A11 (600) Air Ambulance Equipment CL-25-20-21.000 Airplane Flight ManualSupplementThis minor change provides an amendment of the Airplance Flight ManualSupplement for the new configuration introduced with AAT Minor ChangeApproval Number MCA-596 amending the possible configurations of EASA STCEASA.A.S.00733 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... The aircraft shall be operated in accordance with Revision 2 of AATAirplane Flight Manual Supplement document AFM-AAT19<(>,<)>or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Accomplishment of AAT Minor Change approval number MCA-596.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 airworthiness of the prod... 03/11/2022 Active Page 15 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10073302 MINOR CHANGE AIR ATLANTA ICELANDIC 747-400, 747-400F, 747-400 BCF EGPWS CALLOUT MENU 38 STANDARDISATIONStandardisation of theEGPWS Altitude Callouts Menu 38 and of the500SMART Callout to all the Air Atlanta B747-400. 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, Amendment 24 -25.1701, 1703, 1705, 1707, 1709, 1711, 1713, 1715, 1717, 1719, 1721,1723, 1725, 1727, 1729, 1731.Thec... Air Atlanta Icelandic Drawing 747-34-001, Revision 11 dated09 May 2020<(>,<)>or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 19/05/2020 Active 10077602 MINOR CHANGE AIR ATLANTA ICELANDIC 747-400F 747-400 EGPWS CALLOUT MENU 38 STANDARDISATIONStandardisation of theEGPWS Altitude Callouts Menu 38 and of the 500SMART Calloutto all the Air Atlanta B747-400 aircraft. 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: CS-25, Amendment 24 for25.1701, 1703, 1705, 1707, 1709, 1711, 1713, 1715, 1717, 1719, 1721,1723, 1725, 1727,T... Air Atlanta Icelandic Drawing,,747-34-001, Revision 12 dated 16 October2021or 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... 04/11/2021 Active 10078905 MINOR CHANGE AIR ATLANTA ICELANDIC 747-400F 747-400 EGPWS CALLOUT MENU 38 STANDARDISATIONStandardisation of theEGPWS Altitude Callouts Menu 38 and of the 500SMART Calloutto all the Air Atlanta B747-400 aircraft. 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: CS-25, Amendment 24 for25.1701, 1703, 1705, 1707, 1709, 1711, 1713, 1715, 1717, 1719, 1721,1723, 1725, 1727,T... Air Atlanta Icelandic Drawing,,747-34-001, Revision 13 dated 11 March2022or 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... 24/03/2022 Active 10079750 MINOR CHANGE AIR ATLANTA ICELANDIC 747-400F 747-400 EGPWS CALLOUT MENU 38 STANDARDISATIONStandardisation of theEGPWS Altitude Callouts Menu 38 and of the 500SMART Calloutto all the Air Atlanta B747-400 aircraft. 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: CS-25, Amendment 24 for25.1701, 1703, 1705, 1707, 1709, 1711, 1713, 1715, 1717, 1719, 1721,1723, 1725, 1727,T... Air Atlanta Icelandic Drawing - 747-34-001, Revision 15 dated 20 July2022or 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... 21/07/2022 Active 10084106 MINOR CHANGE AIR ATLANTA ICELANDIC 777-300ER EGPWS Callouts Menu 38 ConfigurationEGPWS Altitude CalloutsMenu 38 and 500 Smart Callout configuration onthe Air Atlanta Icelandic Boeing 777-300ER. 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 later amendment: JAR-25, Change 14:1301, 1309, 1529; CS-25, Amdt. 27: 1701, 1703, 1705, 1707, 1709, 1711,1713, 1719, 1729; C... Drawing Index, DWG-777-34-001, Rev. 2 (including Aircraft Maintenance Manual Supplement)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. 13/03/2024 Active 10086186 MINOR CHANGE AIR ATLANTA ICELANDIC 747-400, 747-400F EGPWS CALLOUT MENU 38 STANDARDISATIONStandardisation of theEGPWS Altitude Callouts Menu 38 and of the 500SMART Calloutto all the Air Atlanta B747-400 aircraft. 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 later amendment: CS-25, Amendment 24for 25.1701, 1703, 1705, 1707, 1709, 1711, 1713, 1715, 1717, 1719, 1721,1723, 1725, 1727... Air Atlanta Icelandic Drawing 747-34-001, Revision 17 dated11 Jan 2025<(>,<)>or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. The approval holder shall fulfil the obligations of Part 21, Point21.A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 13/01/2025 Active Page 16 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10086341 MINOR CHANGE AIR ATLANTA ICELANDIC 777-300ER 777-200 EGPWS Callouts Menu 38 ConfigurationEGPWS Altitude CalloutsMenu 38 and 500 Smart Callout configuration onthe Air Atlanta Icelandic Boeing 777. 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: CS-25 Paragraphs:25.1701, 25.1703 (a) (b)(e), 25.1705, 25.1707 (a)(b), 25.1709, 25.1711,25.1713(a)(c), 25.171... DRAWING INDEX, TYPE CERTIFICATE AND TYPE DESIGN INFORMATIONSDWG-777 -34-001 REV 3 dated 15.09.2024or later revisions of the above listed document(s) approved/ acceptedunder the EASAsystem. 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. 03/02/2025 Active 10083303 MINOR CHANGE AIRBORNE TECHNOLOGIES GmbH DA 62 Ferry Tank ProvisionWithin this minor change EO-AT-192 the Diamond DA62 aircraft is equippedwith a provision for installation of a ferry tank. The provisionconsists of the installation of fuel lines from the LH and RH auxiliaryto main tankconnection into the cabin where they are terminated with ana... 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... Installation in accordance with Installation Instructions II-EO-AT-192,rev. 0.Maintenance in accordance with MaintenanceManual SupplementAMM-EO- AT-192, rev.0.or later revisions ofthe above listed document(s) approved/ acceptedunder the EASA system. Only applicable on DA62 with Auxiliary Fuel Tank System (DAI OEM62.001).Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ orrepair will introduce no adverseeffect upon the airworthines... 17/11/2023 Active 10082485 MINOR CHANGE AIRCADS GmbH A320-232 Change in Galley G1 and G5 on A320-232SL MSN 5472Change of galley G1 and G5 - increasing the number of oven (G1: +1 oven,G5: +2 ovens) - replacement of coffee maker by water boiler (G1: 1xequipment change, G5: 2x equipment change) 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... ACS-CP-2204003 – Certification Program Issue 4 dated 27 January 2023.ACS-MDL-2204003 – Master Data List Issue 6 dated 30 June 2023.ACS- ICA-2204003 – Instructions for Continued Airworthiness dated 26April 2023or later revisions of the abovelisted document(s) approved/ acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 28/07/2023 Active 10072267 MINOR CHANGE AIR CALEDONIE INTERNATIONAL S.A.AIR CALIN A320-271N SAFETY PLATES INSTALLATION 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... Technical Dossier No. 01/ M-A322/19/A_Edition 1_Amdt 1 dated17 December2019<(>,<)>or later revisions of the above listed document(s) approved/acceptedunder the EASA system. Limited to AIRBUS A320-271N MSN 10049.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. 23/01/2020 Active 10072625 MINOR CHANGE AIR CALEDONIE INTERNATIONAL S.A.AIR CALIN A330-941 WATER HEATER REPLACEMENT 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... Technical Dossier No. 01/ M-A339/20/A_Edition 1_Amdt 1 dated25 February2020<(>,<)>or later revisions of the above listed document(s) approved/acceptedunder the EASA system. AIRBUS A330-941 MSN 1937 and MSN 1938.The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/ repair it must be determined thatthe interrelationship between this change/repair and anyotherpreviously installed change and/ or repair will introdu... 28/02/2020 Active Page 17 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10075213 MINOR CHANGE AIR CALEDONIE INTERNATIONAL S.A.AIR CALIN A320-271N Crew Rest Curtains Removal & Installation 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... Technical Dossier No. 02/ M-A322/20 Issue A dated 02 December 2020<(>,<) >Or later revisions of the above listed document(s) approved/acceptedunder the EASA system.,, Limited to AIRBUS A320-271N MSN 10049.The approval holder shall fulfill the obligations of Part 21, Point21.A. 109.Priorto installation of this change/repair it must be determinedthatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introd... 16/12/2020 Active 10081998 MINOR CHANGE AIR CALEDONIE INTERNATIONAL S.A.AIR CALIN A320-271N Safety Plate installation The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- The following paragraph(s) at a later amendment:CS25 amendment 27:25.899 and 25.609.The requirements for environmental protection and the associatedcertified noise and/... Modification N°01/M- A322/19 issue B<(>,<)>Or later revisions of the above listed document(s) approved/acceptedunder theEASA system. MSN 10049 and 11882.Prior to installation of this change/repair it must be determined thatthe interrelationship betweenthis change/repair and any otherpreviously installed changeand/ or repair will introduce no adverseeffect upon the airworthiness of the product. 25/05/2023 Active 10082015 MINOR CHANGE AIR CALEDONIE INTERNATIONAL S.A.AIR CALIN A320-271N CREW REST CURTAINS REMOVAL / INSTALLATION The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:- The following paragraph(s) at a later amendment:CS25 amendment 27:25-853 (a).The requirements for environmental protection and the associatedcertified noise and/ or emi... Modification N°02/M- A322/20 Issue B<(>,<)>Or later revisions of the above listed document(s) approved/acceptedunder theEASA system. MSN 10049 and MSN 11882.The approval holder shall fulfill the obligations of Part 21, Point21.A.109.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 adverse... 31/05/2023 Active 10083126 MINOR CHANGE AIR CALEDONIE INTERNATIONAL S.A.AIR CALIN A330-941 'NO STOWAGE' Stickers Installation on Lower Deck Mobile Crew Rest Bunks 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 product are unchangedand remain applicable to this certificate/ approval without any impact... Technical Dossier No. 01/ M-A339/23 issue A dated 25 July 2023Or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. AIRBUS A330-941 Manufacturer Serial Number (MSN) 01937 and MSN 01938The approval holder shall fulfill the obligations of Part 21, Point21.A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed cha... 25/10/2023 Active 10085163 MINOR CHANGE AIR CALEDONIE INTERNATIONAL S.A.AIR CALIN A320-271N WIFI PLACARD REMOVAL The Certification Basis for the original product remains applicable tothis certificate/ approval. Technical dossier MODIFICATION N° 01/M- A322/24 issue A dated 17/07/2024Or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. MSN 10049 and 11882The approval holder shall fulfill the obligations of Part 21, Point21.A.109.Prior to installation ofthis change/repair it must be determined thatthe interrelationship between this change/repair and any otherpreviously installed change and/ or repair will introduce no adverseeffec... 23/08/2024 Active 10086187 MINOR CHANGE AIR CALEDONIE INTERNATIONAL S.A.AIR CALIN A330-941 Aircalin project: Economical Seat Maximum Recline Reduction 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 N° 04/M- A339/19 Issue C signed on 10.Jan.2025<(>,<)>or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. The approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between thischange/repair and any otherpreviously installed change and/or repair will introduce no adverseeffect upon the airworthi... 13/01/2025 Active Page 18 of 182 This report lists certificates issued during the period 01/01/2020 until 11/11/2025. In case you need a certificate not included, please contact applicant.services@easa.europa.eu. An agency of the European Union easa.europa.eu Minor Change / Minor Repair EASA Certificate Number Application Nature Certificate Holder Rev. level Models Description Certification basis Associated Technical Documentation Limitations/Conditions Date of Issue Status 10072988 MINOR CHANGE AIRCRAFT COMPLETION ENGINEERING SEE EASA APPROVED MODEL LIST 1801-2 - Provision for installation of a medical Oxygen bottle The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:the following paragraph(s) at a later amendment: 25.1, 25.303, 25.305,25.333, 25.561(a)(b)(d)(c), 25.562, 25.571(b), 25.601, 25.603, 25.605,25.607, 25.609, 25.611, 25.613,... Master Document List MDL 1801-2-001 Issue 1 dated 03/04/2020or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Provisions only. Not certified for use with pressurized Oxygen.The Oxygen Bottle is not part of the modificationIntegration of EASA STC 10031757 is a pre- requisite for this MinorChange or for optional configuration without STC 10031757 theaffectedseat row is blocked and placarded "DO NOT OCCUPY"The... 08/04/2020 Active 10072989 MINOR CHANGE AIRCRAFT COMPLETION ENGINEERING SEE EASA APPROVED MODEL LIST ACE 1809-2 - Provision for the installation of an incubatoron theBucher stretcher The Certification Basis for the original product as amendedby thefollowing additional or alternative airworthiness requirements:the following paragraph(s) at a later amendment: 25.1, 25.303, 25.305,25.333, 25.561(a)(b)(d) (c), 25.562,25.571(b), 25.601, 25.603,25.605, 25.607, 25,609, 25.611, 25... Master Document List MDL ACE1809-2-001 Issue dated 03/04/2020or later revisions of the above listed document(s) approved/ acceptedunder the EASA system. Integration of EASA STC 10031757 is a pre-requisite for this MinorChangeThe incubator is not part of the modificationThe approval holder shall fulfill the obligations of Part 21, Point21A.109.Prior to installation of this change/repair it must be determined thatthe interrelationship between this cha... 08/04/2020 Active 10080368 MINOR CHANGE AIRCRAFT COMPLETION ENGINEERING REV. 2 SEE EASA APPROVED MODEL LIST 1801-3 - Provisions: Alternative rack for ACE medical oxygen kitACE1801-000- XXXReason for revision 1: Editorial corrections / clarifications of ServiceBulletinReason for revision 2: Addition of alternative parts for Medical oxygenkit ACE1801-000-xxx installed in the alternative rack (ref. Minor Chan... 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: 25.1(a), 25.301 (a),25.303, 25.305(a)(b),25.561(a) (b)(c)(d), 25.571(b), 25.601, 25.603(a),25.605(a), 25.607(a... Master Docum