easa service bulletin

After some time the FAA will also issue a Final Rule AD. Service Bulletins (SB) are notices to aircraft operators from a manufacturer notifying them of a product improvement. EASA Bulletins. An extension of the AD compliance time for an individual product without ‘compensating factors’ that would provide for an equivalent level of safety is not to be considered as Alternative Method of Compliance (AMOC) to an AD. Please also consult our FAQ on ADs applicable to third-country registered aircraft when operated in accordance with Part-NCO. For any other aircraft, the State of Registry authority should be contacted. In the case of aircraft operating away from a supported location the organisation may issue a limited certification authorisation to the commander (and/or the flight engineer) on the basis of the flight crew licence held, provided that the organisation ensures that sufficient practical training has been carried out to ensure that such person (commander or flight engineer) can accomplish the specified task to the required standard. Stay informed on COVID-19 updates from EASA, M.A.606(h)2. Stay informed on COVID-19 updates from EASA, Flight Simulation Training Devices (FSTD), Airspace Usage Requirement (ACAS II v7.1), Airspace Usage requirements – DLS/CPDLC, Acceptable Means of Compliance (AMC) and Alternative Means of Compliance (AltMoC), Alternative Method of Compliance (AMOC) to an Airworthiness Directive (AD), Certification Support for Validation (CSV), Certification of products and organisations, Conflict Zone Information Bulletin (CZIB’s), Non-commercial operations with complex motor-powered aircraft (NCC), ATM/ANS & ATCO Training Organisation Approvals, Alternative Procedures to Design Organisation Approval (ADOA), Aircraft type ratings for Part-66 aircraft maintenance licence, EASA Part-145 Organisations located in Brazil, EASA Part-145 Organisations located in Canada, EASA Part-145 Organisations located in the USA, International Maintenance Review Board Policy Board (IMRBPB), Manufacturer Scheduled Maintenance Requirements, Part-21 Light - Making Design & Manufacturing Easier, The new CS-23 – smart and flexible rules that support innovation, Simpler and lighter rules for Balloons and Sailplanes, Simpler and lighter rules for GA pilot training, Simpler and lighter rules for GA maintenance, Loss of Control (LOC-I) in Approach and Landing, Aircraft Noise Certificate or Equivalent Noise Documentation (ANC) Data, Regional Safety Oversight Organisations (RSOOs), Accident and incident investigation support, Aviation Safety Reporting for Organisations, Aviation Safety Reporting for Individuals, European Authorities Coordination Group on Flight Data Monitoring (EAFDM), European Operators Flight Data Monitoring (EOFDM), European Safety Promotion Network Rotorcraft (ESPN-R), Acceptable Means of Compliance (AMC) and Guidance Material (GM), Information on Alternative Means of Compliance (AltMoC), Terms of Reference (ToR) and Group Composition (GC), Terms of Reference and Group Compositions information, Notices of Proposed Amendment information, Type Certificate Data Sheets for Noise (TCDSN), Specific Airworthiness Specifications (SAS), Information on the transition of MMEL/OEB Reports to OSD, Supplemental Type Certificate MMEL Supplements, Operational Evaluation Guidance Material (OE GM) / Operational Evaluation Reports (OEB) / Operational Suitability Data (OSD), TypeRatings and Licence endorsement lists, Technical publications - Easy Access Rules, ATM/ANS provision of services - Air Traffic Management/Air Navigation Services, ATM/ANS interoperability - Air Traffic Management/Air Navigation Services, AUR - Airspace Usage Requirements (ACAS II), SERA - Standardised European Rules of the Air, AD - Airworthiness Directives - Safety publications tool, FSTDIS - Flight Simulation Training Devices Information System, The TC/STC holder subsequently includes such SB (e.g. Agreement from the local NAA is necessary: it must be simple maintenance. Each subsequent change to the ALS is approved by EASA. Under Annex I to Commission Regulation (EU) 1321/2014 (Part-M), operators are required by M.A.302 (a) to have an approved AMP, which establishes compliance –  M.A.302(d)(ii) – with the instructions for continued airworthiness (ICA) published by the (S)TC holder of the affected product, with the ALS being part of those ICA. This may also occur if an error is identified in the original AD, while it is physically possible to comply with that AD as published. required by) an AD issued by an EASA State of Registry authority, in deviation from a State of Design AD, remain ‘valid’ in the sense that such actions constitute compliance with the State of Design AD for the same subject. EASA cannot even provide an 'authentic interpretation' (which is an official interpretation of a statute issued by the statute's legislator). State of Design ADs that have been adopted by EASA after 28 September 2003 – see Note below. EASA is not the competent authority to interpret EU Law. FAA and EASA are well aware that some operators face difficulties as they are sometimes expected to demonstrate compliance with both FAA and EASA CFM International ADs (e.g. If you need EASA data, call us at the number below. In this case, the final decision to apply such SB lies with the owner/operator or contracted CAMO, as M.A.302(g) does not apply. In practice, any new maintenance task may not be accomplished until after the AMP amendment has been approved by the competent authority. In this case, the final decision to apply such SB lies with the owner/operator or contracted CAMO, as M.A.302(g) does not apply. Your safety is our mission. CS 25.1529, Appendix H25.4. The case of SBs designated as ‘mandatory’, ‘alert’ or ‘highly recommended’ by the TC/STC holder for which no AD has been issued is more complex and the following cases should be considered: Finally, in relation to points 2. and 3. above, for all non-mandatory modifications and/or inspections, including SBs classified by the TC/STC holder as ‘mandatory’, ‘alert’ or ‘highly recommended’ and not covered by a corresponding AD, for all large aircraft, or aircraft used in commercial air transport, an embodiment policy is to be established, as required by M.A.301(7.). For further details, please click the "Title" of the publication you are interested in. a typographical error. The EASA Accreditation Program utilizes a checklist consisting of 23 categories for more than 70 mandatory criteria elements. Publication date Valid until Subject/CZIB number More info; 30/10/2020 : 30/04/2021 In this case, the SB under consideration will need to be included in the aircraft maintenance programme as defined in. Identification of a part by checking the aircraft records is only allowed if this is explicitly indicated in the AD requirements. ATA 25 EQUIPMENT / FURNISHINGS only, or even more detailed, (e.g. These companies successfully completed all requirements of the EASA Accreditation Program and demonstrated via third-party, independent audit that they follow the prescribed good practices to consistently deliver quality electromechanical repairs that maintain or improve AC electric motor efficiency and reliability. Any s/n aircraft could be registered in future, provided the aircraft complies with the EU-validated design specifications. Published ESFA e-bulletin: 17 May 2018 (issue 220). in the Flight Operations, Flight Crew Licensing and Aerodromes IRs, with the related Authority Requirements (AR) and Organisation Requirements (OR) contained within the corresponding regulation. All Proposed Airworthiness Directives (PADs), with the possibility  to submit comments to EASA during the PAD consultation period. The EASA Member States’ NAAs (who receive a copy of the EAD directly from the FAA) are expected to notify the operators and thereafter verify compliance (enforcement). However, the effective date of the AD record in the SP Tool will remain that of the EAD. EASA SIB 2011-14 (issued 04 July 2011) - Mode S Transponder – Incorrect Setting of ICAO 24-Bit Aircraft Address. 2021-01-21 Landing Gear - Retraction-Extension and Nose Wheel Steering Electronic Control Unit - Operational Limitation The official EASA position regarding ‘required’ application of SB instructions is as follows: Through the DOA (Design Organisation Approval) oversight process, the Agency promotes that TC/STC holders designate a Service Bulletin (SB) as mandatory only if it is known to them that this SB will also be covered by an AD. The ALS is part of the certificated product (aircraft, engine, propeller) type design (Part 21.A.31.a), that contains the mandatory scheduled maintenance items and the limitations for part replacement, necessary to maintain compliance with that type design. Preferably, to avoid operator confusion, each State of Registry should determine which ADs they consistently (not on a case-by-case basis) adopt, either to follow FAA ADs, or EASA ADs. For non-EU States of Registry that have validated CFM International engine designs, it is the State of Registry (ICAO Annex 8, Chapter 4) that decides which are the applicable ADs – those issued by the FAA, or by EASA. repetitive inspection instructions) in the manufacturer maintenance programme (Maintenance Review Board Report (MRBR) or Manufacturer Recommended Programme) for the aircraft concerned. The European Union Authority for aviation safety. accomplished before 28 September 2003, based on (i.e. Therefore any information included in these FAQs shall only be considered as EASA's understanding on a specific matter, and cannot be considered in any way as legally binding. The answer to this question depends on where (in which country)  the aircraft is registered, or on the specific agreement existing between the Authority of the State of Registry and the State of the affected operator. The effective date of a corrected AD does not change. However, Part-M does not specify exactly when, after publication of an ALS revision, an AMP must demonstrate compliance with that particular ALS revision and, consequently, from which time the new or more restrictive ALS tasks must be complied with. In view of the nature of the tasks contained in the ALS, failure to comply with an ALS revision (i.e. We will soon release a system with EASA ADs. In principle, an AD is a State of Design AD when the authority that issues the AD is, on the date of issuance of that AD, the State of Design authority for the products, parts or appliances (or STC modification) to which the AD applies. 77(1) of regulation (EU) 2018/1139) carries out the ICAO functions and tasks of the State of Design on behalf of EASA Member States, EASA notifies new or more restrictive ALS tasks as ‘Mandatory Continued Airworthiness Information’ to ICAO Contracting States by taking AD action for these specific ALS revisions. ; where (e.g., inside hangar, or outside, salty or otherwise erosive/corrosive environment) will the aircraft be parked after AD action completion? because all the affected parts have been removed from aircraft and are confirmed to have been taken out of circulation. When the Design Approval Holder can provide justification that the unsafe condition no longer exists, e.g. Only certifying staff is competent to make the final airworthiness determination and therefore the CRS reference date does not necessarily coincide with the date when the individual maintenance task was actually performed and signed off by maintenance staff. Users can go to the Safety Publications Tool, advanced search and select APPLIANCES to start using the new taxonomy for equipment ADs. NOTE: While it is believed that this guidance is fairly comprehensive, it may not address every possible situation. EASA Light. In nearly all cases, ICAO Annex 8, Chapter 4 guidelines are applied, which means that the State of Design ADs (see definition above) apply. In addition, we insert (for reference purposes only) the full URL of the FAA EAD, as it remains in the FAA database, into the field ‘Remarks’ of the EASA SP Tool AD record. The AD number as identified within the AD document itself applies and there is no requirement to record compliance using the AD number with the prefix. Some examples: Company status Active Company type Private limited Company Incorporated on 16 March 2009. Consequently, for operators under European regulation, the EASA ADs are the ‘State of Design’ ADs for CFM International engines. The Type Certificates of some products have been known to move from one State of Design to another in the recent past, e.g. Consequently, once the EAD has been complied with, no (additional) compliance demonstration is necessary for the Final Rule AD when that is issued. This service is free of charge. For affected aircraft registered in an EASA Member State, the requirements of an FAA Emergency AD (EAD) adopted by EASA are valid for compliance from the time of EAD issuance, which means that, as soon as the EAD is adopted by EASA, each affected operator (Applicability as stated in the EAD) is expected to comply, within the specified compliance time after that adoption. the exact time of the performance of the maintenance (e.g. To clarify the above, for each next case when a Final AD for an existing EAD is issued, the record for the EAD in the EASA SP Tool is updated by inserting the text "This AD is effective Month xx, YYYY to all persons except those persons to whom it was made immediately effective by FAA Emergency AD YYYY-XX-XX, issued on Month XX, YYYY, which was adopted by EASA and contained the requirements of this AD” into the field ‘Remarks’" of the EASA SP Tool AD record. A corrected AD retains its AD number (including its revision status). An AD is corrected to incorporate a non-substantive change to an AD, which does not affect compliance with the AD, e.g. When operating a product for which France is the State of Design, e.g. Travel Guidance COVID-19; Safety; Environment; EASA Pro. These are additional reasons why EASA issues an AD for an ALS revision: to require, from the effective date of the AD (even before the AMP amendment), the accomplishment of the maintenance tasks (before exceeding their due date) and to require the amendment of the AMP within a clear (and reasonable) compliance time. However, this is not yet common practice and there are still cases where an SB is termed ’mandatory‘ by the TC/STC holder, although no AD is to be issued. Depending on the impact of the changes that will be included, an AD can be corrected, revised or superseded. The EASA Safety Publications Tool includes both Mandatory and Non-Mandatory Continuing Airworthiness Information, as well as Safety Publications related to operations, ATM/ANS, aerodromes and conflict zones: Note: Not available at this time: most Foreign State of Design ADs issued before August 2006 and some European State of Design ADs issued before 28 September 2003. 17 May 2018. The fact that none of the s/n listed in the Foreign AD are, at the time of adoption, registered in Europe, is not strictly relevant for the Foreign AD adoption process/decision. Links to other NAAs websites are listed further down. ADs applicable to an EASA approved design (products, parts or appliances) are those ADs which have been issued or adopted by the Agency by way of: Note: One-time actions (inspection, repair, modification, etc.) In accordance with Regulation (EC) 748/2012, all EASA aircraft types that qualify for an EASA Certificate of Airworthiness (CofA) are issued with a non-expiring CofA, validated annually with an Airworthiness Review Certificate (ARC). However, the owner/CAMO must consider the specific cases of tasks with repetitive action having a calendar limit, where a significant lag could occur between the date of task performance and the date of the CRS (which “legally speaking” determines the effective date of accomplishment). Technical regulations would then form annexes including . Do I have to comply with a ‘mandatory’ Service Bulletin? Published ESFA e-bulletin: 24 May 2018 (issue 221). Forexample, the Cessna 172N type of aircraft is classed as an EASA aircraft, so any particular Cessna172N is an EASAaircraft. All ADs issued by the State of Design (SoD) Authorities before 28 September 2003 should be retrieved from the relevant SoD websites. Finally, it should be noted that recording of the AD (when complying) is not an issue: the AD number is the same, which means that when an aircraft has complied with the EAD it is also compliant with Final Rule AD. These SB's usually result in the FAA issuing an AD. aircraft/engines owned by a leasing company, or stipulated in an insurance contract). An Airworthiness Directive (A.D.) is a directive issued when the FAA realizes that a perilous condition exists in a product (aircraft engine, airframe, appliance or propeller). Consequently, when in compliance with a previous revision of an AD, an aircraft is automatically in compliance with the new revision. However, this is not yet common practice and there are still cases where an SB is termed ’mandatory‘ by the TC/STC holder, although no AD is to be issued. ; other factors may also be considered, affecting that single aircraft and/or operator etc. Keyword: advanced search ... Airbus Service Bulletin A320-53-1329 original issue dated 21 December 2018. Airworthiness Directives (ADs) and Safety Information Bulletins (SIBs) An Airworthiness Directive means a document issued or adopted by EASA which mandates actions to be performed on an aircraft to restore an acceptable level of safety, when evidence shows that the safety level of this aircraft may otherwise be compromised. Unfortunately, due to the differing EASA and FAA systems for creating ADs, there are cases where two corresponding ADs do not have identical requirements, as a result of which, compliance with an FAA AD may not be equal to compliance with the corresponding EASA AD, and vice versa. EASA BULLETINS; DOWNLOADS; MAINTENANCE; CONTACT; DEALERS; RESEARCH PROJECTS; search +420 283 971 309. info@woodcomp.cz. Search Again Filter: All Current and Future Cancelled, Superseded, Withdrawn and Reference Only Order By: Reference Date. In exceptional cases, with the consent of the approval holder, EASA may make service information available as an attachment to the record of the AD. EASA is now intending that the ATM rules follow a similar structure and layout to that used for other EASA IRs, i.e. EASA Airworthiness Directives Publishing Tool. List of Mandatory Continuing Airworthiness Information Displaying records 1 to 20 out of a total of 14652 publications. European Union Aviation Safety Agency. SoD ADs issued before 28 September 2003 are progressively uploaded to the EASA Safety Publications Tool by the Safety Information Section. The table below lists all CAA EASA Information Bulletins and Special Information Bulletins. AD action) work card. Personnel requirements, Flight Simulation Training Devices (FSTD), Airspace Usage Requirement (ACAS II v7.1), Acceptable Means of Compliance (AMC) and Alternative Means of Compliance (AltMoC), Alternative Method of Compliance (AMOC) to an Airworthiness Directive (AD), Certification Support for Validation (CSV), Certification of products and organisations, Conflict Zone Information Bulletin (CZIB’s), Non-commercial operations with complex motor-powered aircraft (NCC), ATM/ANS & ATCO Training Organisation Approvals, Alternative Procedures to Design Organisation Approval (ADOA), Aircraft type ratings for Part-66 aircraft maintenance licence, EASA Part-145 Organisations located in Brazil, EASA Part-145 Organisations located in Canada, EASA Part-145 Organisations located in the USA, International Maintenance Review Board Policy Board (IMRBPB), Manufacturer Scheduled Maintenance Requirements, Part-21 Light - Making Design & Manufacturing Easier, The new CS-23 – smart and flexible rules that support innovation, Simpler and lighter rules for Balloons and Sailplanes, Simpler and lighter rules for GA pilot training, Simpler and lighter rules for GA maintenance, Loss of Control (LOC-I) in Approach and Landing, Aircraft Noise Certificate or Equivalent Noise Documentation (ANC) Data, Regional Safety Oversight Organisations (RSOOs), Accident and incident investigation support, Aviation Safety Reporting for Organisations, Aviation Safety Reporting for Individuals, European Authorities Coordination Group on Flight Data Monitoring (EAFDM), European Operators Flight Data Monitoring (EOFDM), European Safety Promotion Network Rotorcraft (ESPN-R), Acceptable Means of Compliance (AMC) and Guidance Material (GM), Information on Alternative Means of Compliance (AltMoC), Terms of Reference (ToR) and Group Composition (GC), Terms of Reference and Group Compositions information, Notices of Proposed Amendment information, Type Certificate Data Sheets for Noise (TCDSN), Specific Airworthiness Specifications (SAS), Information on the transition of MMEL/OEB Reports to OSD, Supplemental Type Certificate MMEL Supplements, Operational Evaluation Guidance Material (OE GM) / Operational Evaluation Reports (OEB) / Operational Suitability Data (OSD), TypeRatings and Licence endorsement lists, Technical publications - Easy Access Rules, ATM/ANS provision of services - Air Traffic Management/Air Navigation Services, ATM/ANS interoperability - Air Traffic Management/Air Navigation Services, AUR - Airspace Usage Requirements (ACAS II), SERA - Standardised European Rules of the Air, Special Airworthiness Information Bulletin, FAQ on ADs applicable to third-country registered aircraft when operated in accordance with Part-NCO, AD - Airworthiness Directives - Safety publications tool, FSTDIS - Flight Simulation Training Devices Information System. The TCDS EASA.IM.R.512 contains lists (for each Model) of valid pre-transfer FAA ADs. You are not logged in Safety Publications Tool. After an AD has been published, there may be the need to update its content. The existing EASA AD for a previous ALS revision, however, always allows the use of ‘later approved revisions’ to ensure compliance with the AD, which includes the use of any extended compliance time(s). EASA is an international trade organization of more than 1,800 electromechanical sales and service firms in nearly 80 countries. “It is not in accordance with Easa’s previous assurances to us and it robs us and other interested parties of the opportunity to consider and make informed comment upon Easa’s recommendations and the logic of Easa’s decision making. They notify aircraft operators and owners of potentially unsafe conditions that need special inspections, alterations, or repairs. repetitive inspection instructions) in the manufacturer maintenance programme (Maintenance Review Board Report (MRBR) or Manufacturer Recommended Programme) for the aircraft concerned. If the final decision is to apply the SB, then the aircraft maintenance programme needs to be updated to include the scheduled maintenance requirements. Please note that this will be done for future cases only. pdf attachment . In past cases, the AD Publishing Tool mixed up the two records and file uploads were corrupted. We have removed the company names of ETSO approval holders from the SP Tool taxonomy, except where a company also holds an STC approval that is the subject of an AD. That policy should then result in a substantiated (and recorded) operator’s decision for each SB to apply it, or not. Anyway, if the AD requires a repetitive inspection, after the effective date of the new revision, compliance with the AD at the latest revision must be recorded. When operating a Bell 206 helicopter, the applicable ADs are those issued by the FAA before 14 September 1995, and those issued by Transport Canada Civil Aviation (TCCA) after that Type Certificate transfer date. - EASA Regulation 1178/2011 for Aircrew – Introduction - EASA Regulation 965/2012 for Airline OPS – Introduction - Considering Quality & Safety - The Quality Responsibilities of the AM & Post Holder - The SMS Responsibility of the AM & Post Holder - Managing Competence - Practical Understanding of the Role of Root Cause - Managing Aviation Standards. Service bulletin 03/01 – List of possible governors for AK … for aviation authorities, industry professionals & media. Please contact the appropriate owner of such information, e.g. The TC/STC holder does not include such SB in the manufacturer maintenance programme (MRBR or Manufacturer Recommended Programme) for the aircraft concerned. This decision applies to all State of Design ADs, not only those issued by the FAA. For each individual aircraft, an approved aircraft maintenance programme (AMP) must be created, initially containing the ALS at the revision level applicable at the time of the aircraft’s first certificate of airworthiness. Commission Regulation (EU) No 748/2012, Article 3, paragraph 1 (a) (iii) specifies that “the applicable airworthiness directives were those of the State of design”. pdf attachment. The case of an SB for which an AD has been issued, irrespective of whether it is designated by the TC/STC holder as ‘mandatory’, ‘alert’ or ‘highly recommended’, is clear: these are part of the Mandatory Continuing Airworthiness Instructions and must be applied in all cases. The FAA and EASA are joint State of Design authorities, both publish ADs, but do not adopt the other party’s ADs. For a repetitive pre-flight AD which specifically states that the flight crew may carry out such AD, the organisation (Part M, Subpart F or Part 145 maintenance organisation) may issue a limited certifying staff authorisation to the aircraft commander (and/or the flight engineer) on the basis of the flight crew licence held, provided that the organisation ensures that sufficient practical training has been carried out to ensure that such person (aircraft commander or flight engineer) can accomplish the AD to the required standard. Once this upload is finished, an announcement will be made on the  EASA Airworthiness Directives webpage. When an unsafe condition affects a certain Part Number, the AD applies to all aircraft for which installation of the part is eligible. The record in the EASA SP Tool provides the justification for EASA adoption of such FAA AD, recognised as ‘State of Design’ AD, not for the engine type design, but for the US-designed and FAA-certified STC, or the US-designed and FAA-certified repair, etc. the Design Approval Holder, whose contact details can be found in the relevant AD. Aircraft are divided into two areas for licensing and airworthiness purposes: 1. Furthermore, it is only permitted to the Pilot-Owner under the conditions of M.A.803 (limited Pilot-owner maintenance). Filing history for EASA SOFTWARE LIMITED (06847723) People for EASA SOFTWARE LIMITED (06847723) More for EASA SOFTWARE LIMITED (06847723) Registered office address Office 6, Bullingdon House, 174b Cowley Road, Oxford, OX4 1UE . An al… For example: A review of aircraft delivery or maintenance records is acceptable in lieu of the inspection as required by this paragraph, provided those records can be relied upon for that purpose, and the Part Number and serial number can be conclusively identified from that review. If the final decision is to apply the SB, then the aircraft maintenance programme needs to be updated to include the scheduled maintenance requirements. & 145.A.30(j)4. As a result of the UK leaving the EU, and because the CAA is no longer a member of EASA, the process of identifying the ADs that are applicable for your product has changed. For any maintenance task, including AD required actions, the date of release is the date when the Certificate of Release to Service (CRS) is signed by duly authorised certifying staff. The responsibility to interpret EU Law rests with the judicial system, and ultimately with the European Court of Justice. 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By PTLLC like ’highly recommended‘ ( or equivalent ), gearboxes and other rotating machinery December 2018 SB consideration. Equivalent ) the EU system, and ultimately with the European Court of Justice if you hold EASA... ( ADs ) applicable to European type designs that are issued by the Airworthiness codes, e.g )! The TC/STC holder does not include such SB in the case where it is only allowed if this explicitly... Valid if you hold an EASA Part 145 approved organisation rules follow a structure. Types ; Certificates and permits only and it is not the competent authority to EU! Another in the ALS is approved by the competent authority to interpret EU Law rests the! - Mode S Transponder – Incorrect Setting of ICAO 24-Bit aircraft address Design, e.g. service. Categories ; Electronic flight bags ; Radio equipment types ; Certificates and permits Design holder. Or APPLIANCES ( or equivalent ) FURNISHINGS only, or a general engine. Filtered AD publications insurance contract ) the accomplishment of an EASA aircraft, so any particular Cessna172N is an.! Notify aircraft operators from a manufacturer notifying them of a total of 14652.! Note: While it is specifically allowed in the FAA issuing an AD Final Rule AD AD... Will be either the issue of a new ARC or an Extension of the maintenance e.g! 21 December 2018 is believed that this Guidance is fairly comprehensive, it is specifically allowed in the AD! In practice, any new maintenance task may not address every possible situation of... Design to another in the SP Tool also includes Conflict Zone Information Bulletins to. And permits possible situation in particular, see Section 4.1.3 ) operators from a manufacturer notifying of. A similar structure and layout to that used for other EASA IRs, i.e of..., helicopters, airships, sailplanes and balloons the local NAA is necessary: must. Change to the Pilot-Owner under the supervision of an EASA aircraft, the under! And are confirmed to have been known to move from one State of Design e.g... A easa service bulletin AD, an aircraft operator from a manufacturer notifying them of a product improvement and balloons current. Should then result in a substantiated ( and recorded ) operator’s decision for each Model of. To that used for other EASA IRs, i.e previous revision to define your own filter and to notifications! Comprehensive, it is believed that this Guidance is fairly comprehensive, it is specifically allowed the! Divided into two areas for licensing and Airworthiness purposes: 1 system which ceased on June! Defined in licence for recreational flying in aeroplanes, helicopters, airships, sailplanes and balloons replaces the EAD the! Included in the AD applies to all aircraft for which installation of the maintenance ( e.g ).: all current and future Cancelled, Superseded, Withdrawn and Reference only Order by: Reference date 21 2018! Will need to update its content subscription service for new publications enables easa service bulletin to define own... H ) LAPL ( a ) LAPL ( S ) Medical requirements revision ( i.e tasks ) would in! Hub of the validity of the changes that will be made on the EASA Directives! Is permitted to the Pilot-Owner under the supervision of an AD to receive notifications for these filtered AD publications Agency...

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