on 15 December, interested parties would be able to comment on the relevant PAD at any time up until 23:59 on 15 December. In all other cases, the TC/STC holder should use a term like ’highly recommended‘ (or equivalent). All Proposed Airworthiness Directives (PADs), with the possibility  to submit comments to EASA during the PAD consultation period. We will do the same for all future equipment ADs. The provisions for a Pilot-Owner or Flight Crew to accomplish AD actions are to be found in Commission Regulation (EU) No 1321/2014 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks, Annex I (Part M) & Annex II (Part 145). Depending on the impact of the changes that will be included, an AD can be corrected, revised or superseded. This is a practical IT solution only and it is not meant to be read as a different or new AD number. Airbus Service Bulletin A320-53-1331 original issue dated 14 January 2019. EASA Airworthiness Directives Publishing Tool. 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. An AD is superseded if accomplishment of that AD can no longer assure an adequate level of safety, of a single aircraft and/or of the fleet: this may occur, for example, if a more stringent requirement is added (compliance time and / or required action), or if the applicability is expanded to aircraft models and/or serial numbers not included in the original applicability. Your safety is our mission. 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. 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.). In determining if a lag between the date of task performance and the date of the CRS is “significant”, engineering judgment and common sense must be used. Most popular. 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. The technical requirements and the compliance time are identical in both documents. Common requirements; LAPL (A) LAPL (H) LAPL (S) Medical requirements. The AD would contain a prohibition to install, or specify the conditions under which installation would be allowed, which are requirements that must also apply to aircraft that do not, on the effective date of the AD, have the part installed. The subscription service for new publications enables users to define their own filter and to receive notifications for these filtered documents. EASA supports companies involved in the service and sale of electric motors, pumps, drives, controls, gearboxes and other rotating machinery. 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. For all existing ‘equipment’ ADs, we have specified the name of each approval holder (as it was at the time of AD issuance) in the subject line of the AD record. Alert service bulletins are issued by the manufacturer when a condition exists that the manufacturer feels is a safety related item as opposed to just a product improvement. deviating AD, or statement of non-adoption). EASA has taken over the responsibilities of the former Joint Aviation Authorities (JAA) system which ceased on 30 June 2009. EASAaircraft; and 2. non-EASAaircraft Non-EASAaircraft are also known as ‘Annex II’ aircraft, as they are listed in Annex II to theBasic Regulation, the European legislation which is the source of requirements for pilotlicences. Stay informed on COVID-19 updates from EASA, M.A.606(h)2. This classification applies to types of aircraft, not individual aircraft. In case the SB will not be included in the manufacturer maintenance programme, the final decision to apply it or not lies with the owner/ operator or contracted CAMO. After an AD has been published, there may be the need to update its content. 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. The FAA and EASA are joint State of Design authorities, both publish ADs, but do not adopt the other party’s ADs. Therefore, EASA removes and replaces the EAD with the Final Rule AD in the EASA Safety Publications Tool. EASA does not plan to retrospectively update other existing records for FAA ADs that started life as Emergency AD. Published ESFA e-bulletin: 10 May 2018 (issue 219) The TC/STC holder subsequently includes such SB (e.g. Users can also define/amend their filter setting(s) accordingly, thereby ensuring to be notified when EASA publishes an AD or PAD that does not directly apply to aircraft, engine, or propeller type designs. These SB's usually result in the FAA issuing an AD. accomplished before 28 September 2003, based on (i.e. The accomplishment of an AD is permitted to the Pilot-Owner only in the case where it is specifically allowed in the AD. For example,  2 days are significant for a monthly interval task, and obviously insignificant for a 5-year interval task); what is the technical content (e.g., inspection for corrosion) of the AD task? 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. 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. aircraft/engines owned by a leasing company, or stipulated in an insurance contract). ; where (e.g., inside hangar, or outside, salty or otherwise erosive/corrosive environment) will the aircraft be parked after AD action completion? In all other cases, the TC/STC holder should use a term like ’highly recommended‘ (or equivalent). IF INDICATED IN THE AD, THE FOLLOWING APPLIES: IF NOT INDICATED IN THE AD,THE FOLLOWING APPLIES: This is only applicable in the case of privately (non-commercial) operated non-complex motor-powered aircraft of 2.730 kg MTOM and below, sailplanes, powered-sailplanes and balloons. 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). In the EASA system, the owner/CAMO is not required to keep the (so called) dirty finger prints, i.e. Keyword: advanced search ... Airbus Service Bulletin A320-53-1329 original issue dated 21 December 2018. FAA APPROVES 737-8 & -9 (Max) to … EASA Part-MED requirements; Ratings. EASA can only consider adoption of FAA CFM International ADs in cases where the responsible design (change) approval holder is not CFM International, or where the unsafe condition was due to maintenance errors, e.g. Service bulletin 03/01 – List of possible governors for AK … EASA is now intending that the ATM rules follow a similar structure and layout to that used for other EASA IRs, i.e. Please also consult our FAQ on ADs applicable to third-country registered aircraft when operated in accordance with Part-NCO. 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. Since EASA (under art. Furthermore, it is only permitted to the Pilot-Owner under the conditions of M.A.803 (limited Pilot-owner maintenance). 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. When operating a product for which France is the State of Design, e.g. 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. EASA Bulletins. 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. 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. an Airbus aeroplane, or a SAFRAN helicopter engine (formerly known as Turboméca), the applicable ADs are those issued (or approved) by EASA and, previously, ADs issued by DGAC France. An al… The table below lists all CAA EASA Information Bulletins and Special Information Bulletins. This may occur, for example, when the applicability is reduced; when the compliance time is extended; when an optional alternative method of compliance is added; when an optional terminating action is added; when clarification is provided  (including correction of errors in the previous AD that made the accomplishment of that AD impossible); when non-substantive changes are incorporated (such as the change in the address where a Service Bulletin is available or a change in the name of the contact person), A revised AD retains its AD number with the addition of the revision number, e.g., 2006-0067R1. ADs issued by the Agency through Agency decisions. Introduction. 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. FAA ADs can be found in the Regulatory and Guidance Library, while TCCA ADs can be found on the Transport Canada website, and (since 2003) on the EASA SP Tool. This means that all ADs issued by the State of Design before 28 September 2003 (start date of EASA), either applicable to European or non-European products (i.e. Links to other NAAs websites are listed further down. 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. Consequently, for operators under European regulation, the EASA ADs are the ‘State of Design’ ADs for CFM International engines. In addition, please consult the AMOC FAQ page. Repetitive actions, previously required by an AD issued by an EASA State of Registry authority, must be continued after 28 September 2003 as required by the State of Design AD for the same subject. EASA Part 21; EASA Part 145; EASA Part 147; Maintenance programme approvals; Third country approvals; Bilateral agreements; Lists of approved organisations; Design organisation approvals; Aircraft equipment. Identification of a part by checking the aircraft records is only allowed if this is explicitly indicated in the AD requirements. EASA Airworthiness Directives Publishing Tool. 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 effective date of a corrected AD does not change. EASA Light. Since CFM International engines (CFM56, and now also LEAP-1 engines) are jointly designed and manufactured by General Electric in the US and by SNECMA (now SAFRAN Aircraft Engines) in France, the situation is more complex than for other type designs. In case the SB will not be included in the manufacturer maintenance programme, the final decision to apply it or not lies with the owner/ operator or contracted CAMO. aircraft, engines, propellers), parts or appliances (or STC modifications),  have been adopted by EASA under that Regulation. harmonising regulations and certification 2. developing the single EU aviation market 3. drawing up technical aviation rules 4. type certification of aircraft & components 5. approving companies that design, manufacture & maintain aeronautical products 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. List of all Safety Information Bulletins CORONAVIRUS 2019-nCoV The European Union Aviation Safety Agency (EASA) has recently provided additional promotional material for airlines and their crews regarding the Coronavirus ‘2019-nCoV’ outbreak. The Agency has no legal tools to prohibit the use of the word ‘mandatory’ by TC/STC holders, but EASA Certification Memorandum CM-21.A-J-001 has been issued to provide advice and guidance on this subject. If the final decision is to apply the SB, then the aircraft maintenance programme needs to be updated to include the scheduled maintenance requirements. Guidelines for Following the Service Bulletin (SB) Flow Chart. 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. EASA Service Bulletin Review Process I.A.W Annex 4 to Appendix 3 to AMC 20-20: Service Bulletin Review Process - ED Decision 2007/019/R. For further details, please click the "Title" of the publication you are interested in. In order to receive notifications of new AD publications applicable to a specific product type, you need to register to the Safety Publications Tool. 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 an aircraft registered in an EASA Member State, the National Aviation Authority of the Member State can grant individual (temporary) exemptions on AD compliance time in the event of unforeseen urgent operational circumstances or operational needs of a limited duration, in accordance with Basic Regulation, Article 71. Technical regulations would then form annexes including . The auditor evaluates each criteria line item for evidence of conformity by review of applicable service center repair documents or by observation of service center practices. The new settings enable users to find all ADs applicable to a particular category of parts and appliances, or find all ‘equipment’ ADs with a single search action, rather than (as was previously the case) having to select each ETSO approval holder separately. Consequently, even in compliance with the original (superseded) AD, the owner and/or the operator of an affected aircraft must always comply with the superseding AD. 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. Any s/n aircraft could be registered in future, provided the aircraft complies with the EU-validated design specifications. FAA and EASA concluded a working arrangement, formalising the situation described above (in particular, see section 4.1.3). 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. The European Union Aviation Safety Agency (EASA) is an agency of the European Union established in 2002 by Regulation (EC) No 216/2008 of the European parliament and the Council in order to ensure a high and uniform level of safety in civil aviation, by the implementation of common safety rules and measures. In nearly all cases, ICAO Annex 8, Chapter 4 guidelines are applied, which means that the State of Design ADs (see definition above) apply. EASA Form 117 Page 2/2 . However, the effective date of the AD record in the SP Tool will remain that of the EAD. 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. An EASA pilot licence is only valid if you hold an EASA medical certificate. However, it is not a successor agency in legal terms since it functions … They notify aircraft operators and owners of potentially unsafe conditions that need special inspections, alterations, or repairs. Locate a member of EASA. It should be noted that the only real difference between EAD and Final Rule AD is the effective date: the EAD becomes effective ‘upon receipt’, whereas the Final Rule AD has a ‘fixed’ calendar date. A complete Regulatory Library: ADs, TCs, ACs & FARs; Meets all FAA requirements for IAs & DARs; AD System with graphics and Service Bulletins; Lycoming Service Bulletins SB632, SB632A and SB632B Connecting Rod Identification; DataBases are updated daily. Please contact the appropriate owner of such information, e.g. Forexample, the Cessna 172N type of aircraft is classed as an EASA aircraft, so any particular Cessna172N is an EASAaircraft. 17 May 2018. In such cases, the owner/CAMO must coordinate with the maintenance organisation the issuance of a release specifically and without undue delay to cover the particular task that is subject to a calendar limit when it has been applied, to avoid any distortion regarding limits associated with such repetitive actions or, as an alternative, record the date of AD accomplishment in the CRS. Forexample, the effective date of a total of 14652 publications future equipment ADs on. 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