Easa minor change approval list. 00044 - Minor change/repair action item list TE.

Easa minor change approval list The Agency applies its best efforts to ensure completeness of this list. Categorization of Instructions for Continued Airworthiness: A - Permanent Solution with no additional requirements The MCA documents and the Aircraft Flight Manual Supplement (AFMS) are issued for an individual aircraft. AR6201-AML -). Repairs When there is no type certificate holder approved data for a repair, the documents listed in CS-STAN can be used as the approved repair reference. The extension of delivery includes the full documentation acc. Per 21. Installation of a Trakka TC 300 gimbal camera on Cessna / Textron 172-,182-,206-series listed in EASA approved model list equipped This Work Instruction describes the certification process for type certificates (TCs), restricted type certificates (RTCs), supplemental type certificates (STCs), Changes, Repairs, and ETSO Authorisations. 00032 Minor Repair corresponds to FO. Additional guidance can be found in 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. Minor Change Bestellung. With the latest issue 4 EASA did add many new options and the ADL devices japan easa. Minimum Equipment List (MEL) amended: e. 33kHz COM/NAV. 0105 moog controls corporation philippine branch philippines easa. ). EASA does not have this regulation currently in their CS 23-4 and they have addressed this item inside their EASA Novel & Unusual CRI B-05 "Stick-Pusher". L. In most cases the actual replacement including ground checks can be done in 1-2 hours. : 10039302 Installation of Avidyne TAS605 EASA Approved Model List (AML) 10048734. 603(b), an open bracket system should be proposed to accommodate a series of minor changes to an ETSO article. It appears to me as business, only business! You apply for the minor change, pay the fee, get a piece of paper and In order to be able to process and approve minor changes to the type design, the design organization must have at least the privileges 21. The external AV-75 FLARM antennas should be installed in most aircraft. The means of approval depends on the classification of the change or repair and whether Design Organisation Approval (DOA) privileges can be used. 101 Type-certification basis, operational suitability data certification basis This instruction explains the use, writing and management of Certification Review Items and Certification Action Items. Document Changes EASA Minor Change Approval SUP/TT2x/002 Issue 1. 435 for Repair. The following numbers are listed on the certificate EASA current Project Number: 0010007777-001 EASA old Project Number: P-EASA. 691 regulation have some differences, applicants complying with EASA CRI B -05 could have non compliance to the FAA regulation. The roll-out from paper to digital approval is done in increments, the current scope is reflected in the graphic 3. The modification is registered with EASA. 108 has been known SSD between EASA and the FAA. The EASA Portal. The change approval certificate is issued by EASA. GEN. First – we suggest that you look at the Aircraft Approved Type List within the Minor Change Approval Summary Sheets (below). 1 17. List of all (current & historic) ETSOs as per CS-ETSO amendment 17 Click here to show only current ETSOsClick here to show all Trig is delighted to announce that the TN72 GPS Position Source now has EASA minor change approval and it can now be installed in EASA-certified aircraft covered by the approval. Amendment to supplemental type certificates: Please use the EASA Portal for Major Change to STC and Minor Change to STC. Weight and C of G Schedule Change: b. Scope: Major Change/Repair to TC issued under Part 21 or Part 21 Light, including requests to add new model(s) to the TC (activity formerly known as Derivative); Major Change to STC. A. When satisfied that compliance has been demonstrated, CAA will compile a Technical Visa and submit it to EASA. 5 Airbus 3. On most installations I charge the amount of the EASA minor change fee. Changes and Repairs are classified as major or minor. A list of EASA MCAs and STCs for installation of Aspen equipment and the respective DOA holders may be viewed or To comply with EASA Part-21, Subpart D, 21. On EASA STC certificates, the following statement “or later revisions of the above listed documents approved by EASA. Trig is delighted to announce that the TN72 GPS Position Source now has EASA minor change approval. As a general criterion, a change could be classified as “minor” if it does not require a complete re-investigation for assessing the Important note: As of January 2025, applications for Major Change / Repair, Minor Change / Repair, Supplemental Type Certificate (STC), Alternative Method of Compliance (AMOC), European Technical Standard Order EASA US Part-145 Approvals. 2014 11 ; Revision of SkyView system, supplementation of SkyView system adjustment, extension of nose landing gear leg check for Managing the impact of climate change on aviation 139778; Volcanic Ash; News; Events; Event Proceedings; List of EASA Part 21 Production Organisations approved by National Competent Authorities List of EASA Part 21 Production Organisations approved by National Competent Authorities. o. 3 To allow sufficient processing time by CAAS and EASA, applicant intending to apply for a CAAS Part 21 Design International is an EASA approved Part 21J DOA specializing in approvals of minor cabin modifications, repairs and livery designs. The installer shall report all discrepancies (if any) to the MC EASA | European Union Aviation Safety Agency: The European Union Authority for aviation safety Typically, EASA will issue a revision of the STC. (2) For an aircraft that, at any time after the effective date of this AD, is not in operation for a EASA approval number: Contributor: EASA General Aviation Section: Minor Change EASA. This means a fixed 290 Euro by Part 21. gov. 2014 10 ; Supplementation of balance ballast description and installation. Substantiation by test does not automatically mean that the change is major. Showing all 2 results. change from VFR to IFR. Under the above assumptions the worst case failure condition (failure here includes malfunctions of the FLARM system) at the aircraft level can be classified as Minor provided that the guidance of section 3 is followed, therefore leading to a Minor change classification. Official Publication; AD His engineer applies for a minor change, and it gets approved as minor changes as additional indicator. The process for minor and major changes to these equipment approvals is the same as the process for equipment with UKTSO authorisations. For minor changes to ETSO articles, the root part of the part number is unchanged and the minor change is identified via “open brackets”. Home – Approvals Approvals. POA. 91. Note 1: Reporting of inspection results to the manufacturer or to the aircraft design (change) approval holder is not required by this AD. TCCH. 10040937 or n. TRX-1500/TRX-1500A) collision warning systems. 97 Requirements for approval of a major change. Some less experienced Applicants for Type / Post-Type Certification in General Aviation, sometimes miss the practical experience with certification processes. Use this to verify that your specific aircraft model is The mechanism that is used is the minor change, even if the modification would normally be classified as STC (ie, a major change). Major – All other changes are major. This allows easier installation, Trig’s minor change approvals are free and the TN72 can now be installed into The MCA documents and the Aircraft Flight Manual Supplement (AFMS) are issued for an individual aircraft. e. ADS-B data from other aircraft are decoded by the built-in EASA | European Union Aviation Safety Agency: Alternative Procedures to Design Organisation Approval (ADOA) Continuing Airworthiness Organisations. The list is updated on a weekly basis. Shall inform EASA about minor changes. Aircraft Model List Rev. 1 Page 2 of 28 GAV-MC003-AML Record of Revisions Revision Date Description 1. As this is a living document, changes can be made without expressive notice. Note: Major changes lead to a new ETSO authorization. PBY-5A: AVC-0004-11: Upgrade of Dual Trimble HT-9100 GNSS to Dual Universal UNS-1LW FMS. The certification process is based on design activities (drawings, modeling, please consult our website. 2 An application for an EASA Minor Change approval will be made through instructions issued by the aircraft design (change) approval holder (see Note 1 of this AD). Those approvals have been grandfathered and are considered equivalent to ETSOAs/UKTSOAs and remain valid. Major changes lead to a new ETSO authorization. (d) An EASA minor design change, which is either approved directly by EASA or approved by a suitably approved EASA Part 21J DOA, to be embodied on an aircraft where the Type Acceptance Certificate basis is the applicable EASA Type Certificate. JUN 2014 Changes: Transfer of TC from Aircraft Industries to Blanik Limited. If compliance of a Design Change with the applicable EASA requirements cannot be shown at the EASA Portal. Classification or notification of changes; Acceptance of approvals issued by third countries; Categorisation of systems or equipment; Categorisation of software; installation of parts without an EASA Form 1; Ageing aircraft structures. Further details on the delineation between minor and major changes will be clarified in the forthcoming set of AMC/GM associated to Regulation (EU) 2023/1769 and apply regardless of when the system was deployed/implemented. 09. When you purchase the package, the following documents which are formally part of the Minor Change Approval are included: EASA Minor Change Approval 10074703; FTD-085-AFMS Aircraft Flight Manual Supplement (AFMS) FTD-085-10 Wiring Diagram At Trig we have developed a set of EASA approved upgrade instructions that document the process of installing the TN72 GPS Position Source in a range of. n. Instructions on their own are not classified. 066 Note: All approvals performed under DOA ref. 586 F260B, F260C, F260D, F260E, F260F, SF260 TP S. The DPO is required to communicate to the ANSP any update to the technical manuals This Minor Change Approval is issued by EASA, acting in accordance with Regulation (EC) No. 00044 - Minor change/repair action item list TE. 0108 oman air (s. w. Ref 21. The Trade and Cooperation Agreement between UK and EU states that non-significant supplemental type certificates, approvals of non-significant major changes, repairs and technical standard order authorisations issued by EASA or an EASA approved design organisation are accepted by the UK CAA without a need for issuance of an additional certificate. When you purchase the package, the following documents which are formally part of the Minor Change Approval are included: EASA Minor Change Approval 10074703; FTD-085-AFMS Aircraft Flight Manual Supplement (AFMS) FTD-085-10 Wiring Diagram The ETSOA holder can perform minor changes. 2. 25(a) for As a general criterion, a change could be classified as “minor” if it does not require a complete re-investigation for assessing compliance to the applicable requirements. (e) For EASA, Standard Changes or Standard Repairs accomplished in Any change has to be substantiated regardless if the change is classified minor or major; the responsibility is on the ETSOA Holder. 29 21. EASA Minor Change Approval (MCA) MCA for PowerFLARM Fusion. 1 Applicant’s Reference (if applicable) Internal Reference 1. MAR 2014 Initial release 1. Aircraft type ratings for Part-66 aircraft maintenance licence; How do I know This instruction explains the use, writing and management of Certification Review Items and Certification Action Items. 205 -20F, S. 451(a) and (b), it is the obligation of the respective Holders of a Minor Change Approval, a STC, or a Major Repair Design Approval, to specify the required markings, including EPA letters as applicable, in their Design (read, ‘Approved Data The Trig TN72 GPS Position Source is a highly affordable and certified TSO-C199 device that allows a Trig transponder to become 1090 ADS-B Out. , ltd. When you purchase the package, the following documents which are formally part of the Minor Change Approval are included: EASA Minor Change Approval 10055051; FTD-9-AFMS Aircraft Flight Manual Supplement (AFMS) FTD-9-10 Wiring diagram approved Minimum Equipment List (or similar document), remove that affected fire extinguisher from service and replace it with a serviceable part in accordance with instructions provided by the applicable aircraft design (change) approval holder. Aircraft Maintenance Programme EASA Portal. Information on the application process can be major design changes to ETSOAs, and repairs to critical parts that were developed by someone other than the TC/STC holder. Electrical Load Analysis (ELA): d. 1 This Section sets out procedures for the approval by EASA of Minor Changes to Type Certificates and STCs, and Minor Repair Designs that are approved by HKCAD or made under the privileges of a HKCAD DOA holder. to the Technical Note/ Minor Change Approval with detailed installation instructions, parts list, drawing and EASA FORM 1. This notification should be sent to etsoa [at] easa. Further EASA has recently simplified the administrative application process for Stand-alone FM revisions and has stopped issuing approvals under the title of “AFM Approval”. g. Terms : The rights of use are limited to the aircraft listed below, where this is specified in the AML (Approved Model List - MC1001. Applicant 1. The installer shall report all discrepancies (if any) to the MC Trig installers can use these instructions to achieve airworthiness compliance without needing to seek further approval from EASA. Services; MINOR CHANGE / REPAIR APPROVALS. 5. 101 Type-certification basis, operational suitability data certification basis holders to EASA. For major changes and major repair designs certified by a recognised National/Military Airworthiness Authority (N/MAA), the applicant must consider and assess any differences in the Defence configuration, role and operating environment when EASA Minor Change approval available; The TM250 is aimed at supporting air space surveillance for General Aviation, integrating Mode S, Mode A/C, ADS B, and FLARM®-Detection in one single cockpit device. 0 Schempp Hirth additional models Additional applicable aircraft 10030508 SUP/TT2x/002 Issue 4. Now these people at the FAA don’t even accept this changes, it needs to be reviewed again (similair as Final approval is pending the approval of EASA minor change Project Nr. EASA grants privileges for the DOA to design new products, product modifications or repairs and may include approval for these designs. The notification can be performed by either providing a This EASA Minor Change Approval approves the modification of the aircraft for the installation of AIR Traffic (AT-1) and TRX (e. 00035 - Compliance statement FO. 2 Name Name 1. A Certification Review Item (CRI) is a formal administrative means within the certification process Aspen announced today the issuance of EASA Minor Change Approval (MCA) for installation of the EFD1000H PFD System in Eurocopter models AS355E, AS355F, AS355F2, AS355N and AS355NP type certificated under EASA. Classification is the Certifying Authority (CA) responsibility and must be accepted by the Validating Authority (VA) . eu (etsoa[at]easa[dot]europa[dot]eu). When you purchase the package, the following documents which are formally part of the Minor Change Approval are included: EASA Minor Change Approval 10055051; FTD-9-AFMS Aircraft Flight Manual Supplement (AFMS) FTD-9-10 Wiring diagram Final approval is pending the approval of EASA minor change Project Nr. All EASA STCs are published except: - 'Grandfathered' STCs issued by the EU Member States prior to 29/09/2003. Each of the following links will open the official EASA STC approval. Examples for minor changes are: Part numbers to be added to the list of approved ones (for example to add open brackets) The FAA will issue approval letters for major level 1 design changes to TCs and STCs, major design changes to ETSOAs, and repairs to critical parts that were developed by someone other than the TC/STC holder. 00161 The ETSOA holder can perform minor changes. The FAA will accept EASA approved major level 2 design changes, minor design changes, and most repairs, which are considered approval application. Part - Ref - Sheet 1 (25) Saab AB DOA Approval No Approved Data Description Product Type Approval Date Saab AB, site Nyköping DOA EASA. EASA-approved retrofit kits, where the existing shoe brake wheel is replaced by a new disk brake wheel or a brake disk is fitted onto the existing shoe brake wheel. 611(a), the root part of the part number is unchanged and the minor change is identified via “open brackets”. 263 (c) 1 (classification) and 21. First – reference The Design Change meets OTAR 21. However, he has to inform EASA about minor changes. 451(a) and (b), it is the obligation of the respective Holders of a Minor Change Approval, a STC, or a Major Repair Design Approval, to specify the required markings, including EPA letters as applicable, in their Design (read, ‘Approved Data’), according EASA Part-21, Subpart Q. Aircraft Model List (AML) EASA Minor Change Approval 10048704 . Credit: e. It is required to regularly inform EASA about minor changes (at least once per year). In the past, applications for Stand-alone FM revisions could be made The MCA documents and the Aircraft Flight Manual Supplement (AFMS) are issued for an individual aircraft. EASA Minor Change Approval (MCA) for PowerFLARM Core € 109. CS-STAN is intended to provide an alternative to the established minor change process. The EASA document that explains CS-STAN in full can be found at the following link. Conversely, if the holder modification or a Minor Change Approval is required. For Minor Change Approvals we have developed a set of upgrade instructions that detail the process of changing an existing transponder or VHF radio to a Trig product, in a wide range of aircraft types. 00032 Production Organisation Approval - Initial corresponds to FO. 27. 205 -18F, S. The MCA documents and the Aircraft Flight Manual Supplement (AFMS) are issued for an individual aircraft. P. Major Repair Minor Repair Minor Temporary Change N/A: Instruction 16. The Portal is available for use The definition of major/minor changes are provided at the AMC/GM level. The applicant should apply on an EASA Form 32 referring to the FAA STC and its EASA grandfathered The classification of the RDAF complies with EASA Part 21A. Design Change Description(s): As defined in Table 1 of this AD Effective Date: 11 June 2021 EASA STC Number(s): Supplemental Type Certificate (STC) 10068537, 10070605, 10064987 or 10072189 Minor Change No: CAS-A330-17-006 up to Revision 3 (inclusive) Foreign AD: Not applicable Please note the CAA issued thousands of Equipment Approvals prior to the formation of EASA. Eligibility. 205 -18R, S. If compliance of a Design Change with the applicable EASA requirements cannot be shown at the date of airplane delivery, the type-certificate holder should notify the customer accordingly. Typically, EASA will issue a revision of the STC. Minor change A change that has no appreciable effect on the weight, balance, structural strength, reliability, operational characteristics, or other characteristics List of EASA Approved Changes Date: 18/06/2015 Page 1 of 3 AIRCRAFT (MFR/MODEL) APPROVAL NUMBER DESCRIPTION OF DESIGN CHANGE Piper PA-32 EASA approved Minor Change 10032400 Installation of Kelly ES4003 Piper PA-32-301FT / -301XTC EASA approved FMS No. We have obtained EASA approval so Trig installers can use these instructions to achieve airworthiness compliance without needing to seek further How do I know whether my proposed change is minor? Answer The ETSOA holder can perform minor changes. With the European Union EASA mandates all Mods for Commercial Air Transport ( CAT) & Large Aircraft – Minor or Major (STC) are managed through an EASA Part 21 Design Organisation The following table provides typical examples where an applicant or DOA holder gets help in the decision process to classify a design change as Minor or Major. You can check the relevant approved model •Classify changes to design or repairs as major or minor •Approve minor changes and repairs, •Approve major repairs to products for which it holds the TC or STC •Issue approved technical documentation •Approve minor revisions (previously documentary changes) to flight manuals •Approve permit to fly conditions (with listed exceptions). 451(a) and (b), it is the obligation of the respective Holders of a Minor Change Approval, a STC, or a Major Repair Design Approval, to specify the required markings, including EPA letters as applicable, in their Design (read, ‘Approved Data SAAB AB EASA DOA 21J. 10073411 MINOR CHANGE ADANAIR S. 0 Schempp Hirth Original Document N/A SUP/TT2x/002 Issue 2. co. These Minor Change Approvals are free. 8. 205 - In Europe the installation of a TN72 in an EASA aircraft uses our free EASA Minor Change, an AML (approved model list). 68 "OBSERVER" Installation of ASIVE CONSOLE in the interior The Certification Basis (CB) for the MASTER DATA LIST MDL001- Prior to installation of this change/ 05/06/2020 Active of Vulcanair P. Application effectiveness: The effectiveness of your application is limited to five (5) years for large aeroplanes and large rotorcraft and to three (3) years for any other product. minor change) for a product, part or non-installed equipment, that is to be installed on an aircraft operated by a comes from a Supplemental Type Certificate holder, minor change approval holder or repair approval holder, the parts will have to be marked as prescribed in the applicable data which should include an EPA marking since 28/3/2004 (*). Cabin Interiors (Carpets; Curtains; NTF; Decorative Laminates; Galley Modification / Managing the impact of climate change on aviation 139778; Volcanic Ash; News; Events; Event Proceedings; Research & Innovation Regulations in the area of aviation safety not stemming from the EASA Basic hazard assessment to a minor level. to the Technical Make: Airbus, Model: H125 B3e, Year built: 2020, TTAF: 3045 h, Location: Switzerland PK !ÞÒ•ƒî M [Content_Types]. Anyone may apply for the CAA approval of a minor modification or minor repair. Final approval is pending the approval of EASA minor change Project Nr. 68 ObserverThe modification original product remains applicableto Revision 1<(>,<)>Or later repair it EASA recommends holders of a type design approval (type certificate) or design change approval (supplemental type certificate, or minor change approval) to consider the presence of fire in addition to hot gases in assessing the effect at aircraft level of battery failures for the articles listed in the Applicability section of this SIB. 066 MINOR CHANGE APPROVALS BY TYPE – SITE NYKÖPING Effective date 2024-05-17. You can find the JAA approvals listed on our website. The same applies to the Major or Minor Change applications. 91 for Change and with 21A. There are several FAA STCs approved by EASA (i. ONLINE SERVICES. (*) – As from 18. 118A (b) and Subpart M, 21A. 1 For the European Union Aviation Safety Agency Cologne, Germany, 25 June 2020 Dominique RENAUD Section Manager Jet Aeroplanes This Certificate/Approval is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of Applications for approval of minor modifications and minor repairs to non-Part21 aircraft, such as amateur-built, microlights, gyroplanes, historic aircraft or replicas, can be submitted by email to apply@caa. 0 None Internal changes 10029518 SUP/TT2x/002 Issue 3. . ” is below the list of “Associated Technical Documentation”. Minor – A minor change has ‘no appreciable effect’ on airworthiness or environmental characteristics. sg. 00100 - Letter EASA-approved retrofit kits, where the existing shoe brake wheel is replaced by a new disk brake wheel or a brake disk is fitted onto the existing shoe brake wheel. This means that a DOA (EU) shall classify changes according to EU 748/2012 Annex 1 (Part 21). The Portal is available for use Applications for approval of minor modifications and minor repairs to non-Part21 aircraft, such as amateur-built, microlights, gyroplanes, historic aircraft or replicas, can be submitted by email to apply@caa. Instructions for Continued Airworthiness / Maintenance Manual supplements: c. 10047546- AVIONIK SERVICE LUFTFAHRTELEKTRONIK GmbH 2t10. The applicant shall classify the change (minor/major) according to the applicable regulatory framework for its design organization. The Trig TN72 GPS Position Source The Trade and Cooperation Agreement between UK and EU states that non-significant supplemental type certificates, approvals of non-significant major changes, repairs and technical standard order authorisations issued by EASA or an EASA approved design organisation are accepted by the UK CAA without a need for issuance of an additional certificate. In particular, a list of all Minor Design Changes approved by IAC since previous delivery must be provided to EASA for approval. Aircraft type ratings for Part-66 aircraft maintenance licence; How do I know Approval of minor changes, minor repairs and some major repairs can be conducted by approved organisations under privilege. 10047546 AS Avionic-Service Luftfahrtelektronik GmbH * Richthofenweg 13 * 49088 Osnabrück Germany TC Holder Type Models * No limitations applied TCDS Alenia Aermacchi F260 F260 EASA. MCA for PowerFLARM Core. Further EASA-approved retrofit kits, where the existing shoe brake wheel is replaced by a new disk brake wheel or a brake disk is fitted onto the existing shoe brake wheel. 263 (c) 2 (approval of minors) in its TOA. 0112 pan asia pacific aviation services ltd hong kong easa. 10048734 (retrofit AR6201 8,33/25 kHz VHF-COM to replace AR3201 or AR4201). Minor Changes to an STC may also be applied for by an applicant other than the STC holder. PROCEDURE: OTHER LABEL TO BECKER. Minor Change to STC corresponds to FO. The AV-75 antenna installation is covered in the EASA Minor Change Approval. 00001 “Airworthiness of Even minor modifications for example seat covers, replacement of stickers, or the installation of a magazine holder requires appropriate approved maintenance data. 19 Mar 2021. JUN 2014 Changes: Transfer of TC from Aircraft Industries to Blanik Limited EASA Form 32 Application for Approval of Minor Change / Minor Repair Design Page 1/5 Issue 5, dated 01. china easa. Are documents approved afterwards using a DOA privilege (e. 1. Supporting Documentation: a. First – reference the Applicable Aircraft Model List (bottom of page) to access the relevant Minor Change Approval Certificate for your aircraft. Can a US manufacturing The following table contains a list of our CAA Approved Minor Changes. These have been replaced by the issuance of a standard change approval (e. Minor Change Approval & EASA Approved EASA | European Union Aviation Safety Agency: The European Union Authority for aviation safety. - STCs issued by EASA Form NR 93 - Change approval template EASA Form NR 96 - Technical visa for post TC design approval FO. In the case of an STC, there is no reference to type design; instead, approve minor changes, or for approval of identical replacement parts (unless the installation of such parts constitutes a major change to the type design); I / we apply for a free of charge Minor Change Document set related to EASA approval No. 12129 CEAPR DR 400 HR 100 HR 100/250 TR Revision: Not applicable Correction: Not applicable Supersedure: This AD supersedes EASA AD 2011-0076 dated 29 April 2011. Also allows applicants to view and monitor the status of their applications, and to Trig installers can use these instructions to achieve airworthiness compliance without needing to seek further approval from EASA. The company owns the modification and you need to pay them if you use somebody’s else’s mod. 93 before recommending approval to EASA. The installer shall report all discrepancies (if any) to the MC approvals i. Since the EASA CRI and FAA 23. XXXXX Minor Repair Approval – 10098880 – Company Name Comment [r1]: EASA Approval number: This is the EASA approval Agency’s ERP system only once the technical visa has been issued and the project is For minor changes to ETSO articles, per Regulation Commission Regulation (EU) No 748/2012 article 21. EASA system. The extend of delivery includes the full documentation acc. There is a large number of old national approvals which were issued before 28 th September 2003 but due to the lack of full national Annexed to Commission Regulation (EU) No 748/2012 is Annex I (Part 21). i to iv, 0-3, 0-5, 3-1, 3-5, 3-10, 3-11 . 2014-08-22 ; EASA Minor Change Approval 10050318 . 0106 mtu maintenance zhuhai co. TC. Most paper work is already available and the remaining updates of the aircraft EASA. B727: AVC-0005-12: Installation of TT21 Transponder. A Certification Review Item (CRI) is a formal administrative means within the certification process and provides a structured means of recording subjects as listed in 2. Generally, if changes are classified minor and do not require a change to the certificate, any method to inform EASA is accepted. xml ¢ ( Ì—]oÓ0 †ï‘ø ‘oQânÀ„PÓ]ðq “ ·®}Ò â Ù§[ûï9NÚ léHƒzS©9~ß÷ñq »óë­©³; Q;[²‹bÆ2°Ò)mW%û~û9 DzˆÂ*Q; %ÛAd׋—/æ·; 1#µ %[#ú÷œG¹ #bá R9‡Öá «ÑY B€U 1 œ Ö „ñçÄ_ ­ñQë0I~k|D>å‰e S ì­ ! nŒÐ~ŽïDcóT$ l^Ät ÿ0íý*©s Ô ¸K$ëÑóƒteS ž›Ýž ':|zÂyóg`ñ ÿÿ PK !™U - EASA Minor Change Approval and approval according to FAA regulations - EASA Form One - Engineering Order - Approved Model List - CMM Already certified, installed and in service on: A318, A319, A320, A321, A330, A340, B717, B737, B747, B757, B767, MD11 Flying on EASA | European Union Aviation Safety Agency: The European Union Authority for aviation safety Priorto installation of this change/repair it must be determined that the interrelationship between this change/repair and any other previously installed change and/ or repair wi I introduce no adverse effect upon the airworthiness of the product. The FAA will accept EASA approved major level 2 design changes, minor design changes, and most repairs, which are considered approved by the FAA following approval under EASA’s system. Similarly, the fees are applied based on the type of application (STC/Major Change/Minor Change) – the only specific process is that, in case of an AML application, the heaviest aircraft is used to compute the applicable fees. ) t/a oman air oman easa. 0 26. Non-EASA aircraft Applications for the approval of minor modifications to Non-EASA aircraft should be EASA Minor Change Approval (MCA) MCA for PowerFLARM Fusion. EASA | European Union Aviation Safety Agency: The European Union Authority for aviation safety This EASA Minor Change Approval approves the modification of the aircraft for the installation of AIR Traffic (AT-1) and TRX (e. 2007 European Aviation Safety Agency Application for Approval of Minor Change / Minor Repair Design 1. CERT. page 2 of2 End - 60064851 MINOR CHANGE APPROVAL -10073318 - AVIATION - 302451 Document Changes EASA Minor Change Approval SUP/TT2x/003 Issue 1. EASA Part 21 Subpart J details the elements required of a design organisation in order to hold an EASA Design Organisation Approval (DOA). The OTARs accept the Minor/Major classifications used by the applicable NAA specified in OTAR Part 21. See the TIP for details. EASA. 7 Changes to AML Change EASA European Aviation Safety Authority FAA Federal Aviation Administration Design change A change in the approved design of an aircraft, aircraft engine or propeller. To comply with EASA Part-21, Subpart D, 21. 10042099) for which it is necessary to apply for a Minor change, too. As a general criterion, a change could be classified as “minor” if it does not require a complete re-investigation for assessing the compliance to the applicable requirements. It complements the EASA Procedure PR. Aircraft Type Change Description Change Number; AVC-0003-11: Introduction of Garmin GTX330 Transponder. Operational aspects are not subject of this table, e. EASA | European Union Aviation Safety Agency: Alternative Procedures to Design Organisation Approval (ADOA) Continuing Airworthiness Organisations. The rules for the classification are identified in paragraph 21. 205 S. a. If an EASA approved change is required, an EASA form 32 applies and can be viewed here. Can a holder of a design organisation approval (DOA) apply to EASA for a supplemental type certificate (STC) or other design approval (e. Fred now wants to change his registration to N-Reg. For antenna diversity (360° coverage), one antenna is installed on top of the aircraft and one below. MINOR CHANGE /MINOR REPAIR DESIGN APPROVALS 5. List of EASA Supplemental Type Certificates The list of EASA Supplemental Type Certificates is available in the download section below. 6 Abbreviation and Acronyms The following abbreviations and acronyms are used in this document: AFM Aircraft Flight Manual DC Direct Current DDP Declaration of Design Performance EASA European Aviation Safety Agency CS-STAN was introduced by the European Aviation Safety Agency (EASA) in 2015 and provides a cost effective and faster route to installing avionics in non-complex EASA aircraft. A convenient gateway allowing Applicants to prepare and submit applications online. Information on the embodiment of all Minor and Major Design Changes, should be made available by type-certificate holders to EASA. c. 145. 146. The aircraft shall not be released to flight before evidence of final approval is provided”; Aircraft modification: the installer modifies the aircraft using the design data provided by the MC applicant. The certification process is based on design activities (drawings, modeling, specifications), but consist mostly of engineering tasks (analysis, testing, assessment) where the applicant have to show, through certification Any article approved or validated by any member state before the establishment of EASA is deemed to be 'Grandfathered' under Commission Regulation (EU) No 748/2012 Article 6 . HDH140 Dove 8: EASA has recently simplified the administrative application process for Stand-alone FM revisions and has stopped issuing approvals under the title of “AFM Approval”. Minor Change; Minor Change to ETSOA; Minor Change to STC; Minor Repair; Production Organisation Approval; STC; Surrender of Product or Organisation; Validation of an EASA Certificate by the TCA; How to Register. 91 and the guidance in the GM 21. 73(a) requirements and is compatible with the aircraft design to the OTAA Type Acceptance Certificate in force for installation on the aircraft concerned: List of EASA Approved Changes Date: 18/06/2015 Page 1 of 3 AIRCRAFT (MFR/MODEL) APPROVAL NUMBER DESCRIPTION OF DESIGN CHANGE Piper PA-32 EASA approved The DPO is eligible to design and implement minor changes to its CERT/DECL equipment, but has to notify these changes to EASA in any case. 0113 pratt & whitney holdings sas (pratt & - EASA Minor Change Approval and approval according to FAA regulations - EASA Form One - Engineering Order - Approved Model List - CMM Already certified, installed and in service on: A318, A319, A320, A321, A330, A340, B717, B737, B747, B757, B767, MD11 Flying on more than 2300 aircraft world wide General Overview 21. Aircraft type ratings for Part-66 aircraft maintenance licence; Minor Changes/Minor Repairs (PDF Version) EASA publishes selected approval data under the links provided below to allow third parties to verify the data if necessary. 2022, parts covered by 21. In this case EASA will not issue a revision to the STC but a Minor Change approval in accordance with Subpart D of Commission Regulation (EC) No 748/2012. 00038 - Record of the certification team composition FO. R. 97. European Aviation Safety Agency Avionic Service Luftfahrtelektronik GmbH - EASA Approved Model List (AML) EASA has recently simplified the administrative application process for Stand-alone FM revisions and has stopped issuing approvals under the title of “AFM Approval”. STC Provision. 00032 - Type Certification Review Item FO. Minor Change Approval 10048734. Minor mods can be in-house approved by an EASA 21 company, within certain boundaries. europa. 95 Requirements for approval of a minor change . 1 regarding the certification basis and its interpretation throughout a certification EASA approval number: Contributor: EASA General Aviation Section: Minor Change EASA. EASA Form 16: view [docx] EASA Form 16 - EASA US Part-145 Approvals. 21. 25/06/2024 : FAA Recommendation. the alternative is to use the EASA CS-STAN approved changes for ELA2 aircraft below 2000kg. I / we apply for a free of charge Minor Change Document set related to EASA approval No. TCCA DAR* / DOA* / CAR 571 Appendix A: 12 . 00 Select options; EASA Minor Change Approval (MCA) for PowerFLARM Fusion EASA Form NR 121 - Expert statement of technical satisfaction EASA Form NR 94 - Repair approval template EASA Form NR 96 - Technical visa for post TC design approval FO. Minor Change Approval/Major Change Approval, etc. 3 Address (registered business/postal address) We would like to remind our customers that we have an EASA minor change approval for plug/play replacement of an existing King KX155/165/155A for a King KX165A 28V 8. CM-CS-005 Part 21J DOA for simple _ and ^complex _ types ^simple _ always by a minor change ^complex _ by major change / ST only if rotorcraft limitations and procedures are directly affected Partially accepted Introduced airworthiness approved [ as minor change, this included EASA and DOAs. 00100 - Letter Design Change Approval Holder’s Name: SOCIETE AIR FRANCE S. Article 2 of the Basic Regulation requires the Agency to take the responsibility for the design approval of products, parts and appliances designed, manufactured or used by persons/organisations under the regulatory oversight of the EU Member States, Norway, Iceland, Liechtenstein or Switzerland, except for those excluded by its Annex I. Applicant eligibility: More details on the eligibility criteria for STC applicants can be found in our EASA Minor Change Approval 10048185 18. XXX. EASA Approved Aircraft Model List (AML) Minor Change No. 0 Piper PA-28 Original Document N/A 1. Minor Change Order. minor change approval) covered by that statement? Some less experienced Applicants for Type / Post-Type Certification in General Aviation, sometimes miss the practical experience with certification processes. Official Publication. Use this to verify that your specific aircraft MINOR CHANGE APPROVAL 10061508 REV. 109, Subpart E, 21A. 603(b) The replacement of avionics is a change to the type design that has to be approved in accordance with Part-21, and, for that, it has to be classified as major or minor, depending on the effect that the change has on the airworthiness of the A/C. First – we suggest The following table contains a list of our CAA Approved Minor Changes. 0 Dimona HK36 series Additional applicable Please note this minor change was fully funded by Golze Engineering and we provide it free of charge to all customers having purchased an ADL150(B), ADL190 or ADL200 device. Acceptable Means of Compliance (AMC) and Guidance Material (GM) AMC To comply with EASA Part-21, Subpart D, 21. 00 – € 279. uk through the SRG1726NR form. of EASA minor change or minor repair design approval, the holder of a Part-21 DOA issued by EASA may contact CAAS directly via CAAS_AFO_infocenter@caas. 0109 pratt & whitney canada (sea) pte ltd singapore easa. 21J. Home – Obstacle Databases – Obstacle Database UK & Ireland 2025. MINOR CHANGE APPROVAL - . EASA CS-STAN* / DOA EASA Part 21 Subpart J*: f. If the TC holder is making the change, data is a change to type design as identified in Part 21. . 307(b) does need to be accompanied by an - EASA Minor Change Approval and approval according to FAA regulations - EASA Form One - Engineering Order - Approved Model List - CMM Already certified, installed and in service on: A318, A319, A320, A321, A330, A340, B717, B737, B747, B757, B767, MD11 Flying on more than 2300 aircraft world wide General Overview EASA | European Union Aviation Safety Agency: Alternative Procedures to Design Organisation Approval (ADOA) Continuing Airworthiness Organisations. C. Aircraft Model List Aircraft Model List (AML) EASA Minor Change Approval 10048704 . It's not related to safety or additional important requirements (as the STC itself gives all the necessary information). This allows the permanent installation of AIR Traffic, TRX and accessories such as traffic displays and antennas in many aircraft. Trig installers can use these instructions to achieve airworthiness compliance without needing to seek further approval from EASA. 1 Generally there are two classifications of design change: Minor and Major. qtcgti wicif dwire jvfp qlqgvxk xvvxeh ofbar mpcuip dlt yhad