FAA AD 2016-14-10 for P&W STC-modified engines; and AD 2009-11-02 for improper repair by PTLLC. Consequently, when in compliance with a previous revision of an AD, an aircraft is automatically in compliance with the new revision. repetitive inspection instructions) in the manufacturer maintenance programme (Maintenance Review Board Report (MRBR) or Manufacturer Recommended Programme) for the aircraft concerned. Next accounts made up to 31 March … Please also consult our FAQ on ADs applicable to third-country registered aircraft when operated in accordance with Part-NCO. Since October 2016, a new format to improve the taxonomy for ADs applicable to parts and appliances (equipment) has been fully implemented in the EASA Safety Publication Tool. Please note that this will be done for future cases only. 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. 24 May 2018. In practice, any new maintenance task may not be accomplished until after the AMP amendment has been approved by the competent authority. In all other cases, the TC/STC holder should use a term like ’highly recommended‘ (or equivalent). Guidelines for Following the Service Bulletin (SB) Flow Chart. - 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. for passengers, EU citizens & general public Most popular. Publication date Valid until Subject/CZIB number More info; 30/10/2020 : 30/04/2021 The LAPL is a simplified EASA licence for recreational flying in aeroplanes, helicopters, airships, sailplanes and balloons. A Service Bulletin (S.B.) on 15 December, interested parties would be able to comment on the relevant PAD at any time up until 23:59 on 15 December. The following questions should be considered: It is also to be noted that AD compliance verification (enforcement) is not an EASA responsibility, but that of the National Aviation Authority of the State of Registry of the aircraft, and it is always recommended, if in doubt, to seek their advice. That policy should then result in a substantiated (and recorded) operator’s decision for each SB to apply it, or not. deviating AD, or statement of non-adoption). EASA Airworthiness Directives Publishing Tool. The European Union Authority for aviation safety. 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.). 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 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. Stay informed on COVID-19 updates from EASA, M.A.606(h)2. Aircraft equipment; Approval categories; Electronic flight bags; Radio equipment types; Certificates and permits . 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. 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. Forexample, the Cessna 172N type of aircraft is classed as an EASA aircraft, so any particular Cessna172N is an EASAaircraft. Actions are not accomplished under the supervision of an EASA Part 145 approved organisation or EASA Part M, Subpart F approved organisation. 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. State of Design ADs that have been adopted by EASA after 28 September 2003 – see Note below. FAA and EASA concluded a working arrangement, formalising the situation described above (in particular, see section 4.1.3). Consequently, EASA has recently issued the following Safety Information Bulletins (SIBs): EASA SIB 2011-13 (issued 04 July 2011) - Mode S Transponder – Loss of Detection (Complete or Intermittent) of Aircraft by Mode S Interrogators. The TC/STC holder does not include such SB in the manufacturer maintenance programme (MRBR or Manufacturer Recommended Programme) for the aircraft concerned. aircraft/engines owned by a leasing company, or stipulated in an insurance contract). EASA is not the competent authority to interpret EU Law. 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. For further details, please click the "Title" of the publication you are interested in. The reason for this is that the unsafe part could be installed on any of those aircraft at a later stage after issuance of the AD. An AD is corrected to incorporate a non-substantive change to an AD, which does not affect compliance with the AD, e.g. 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. EASA enables you to create a web interface which contains the input data fields and fields for the calculated outputs, if appropriate (including charts, tables and graphics), while the native model, or process, becomes server based and only accessible by the web app interface (not the user). 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. In nearly all cases, ICAO Annex 8, Chapter 4 guidelines are applied, which means that the State of Design ADs (see definition above) apply. 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. 2021-01-21 Landing Gear - Retraction-Extension and Nose Wheel Steering Electronic Control Unit - Operational Limitation 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. 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. EASA Airworthiness Directives Publishing Tool. Each AD issued before 28 September 2003 by an EASA State of Registry authority, in the absence of a State of Design AD (also identified as ‘additional’ AD), is no longer valid from 28 September 2003 (i.e. Double-click on a TC holder/Type/Model in the Taxonomy panel or drag'n'drop them onto the current filter to narrow down your search. Since EASA (under art. 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. 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 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. As a result, all ADs issued by the State of Design authority for the affected product(s), part(s) or appliance(s) are valid in Europe, unless EASA has issued a different decision. CS 25.1529, Appendix H25.4. ADs issued by the Agency through Agency decisions. 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. This later decision implies that any AD issued by the State of Design authority for the products, parts or appliances (or STC modification) to which that AD applies, becomes valid in Europe upon the day that AD becomes effective, unless the Agency issues a different decision (e.g. The FAA and EASA are joint State of Design authorities, both publish ADs, but do not adopt the other party’s ADs. 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. Consequently, for operators under European regulation, the EASA ADs are the ‘State of Design’ ADs for CFM International engines. 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. In all other cases, the TC/STC holder should use a term like ’highly recommended‘ (or equivalent). 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. 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. The table below lists all CAA EASA Information Bulletins and Special Information Bulletins. 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. The prefix was therefore introduced to clearly distinguish those ADs. 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. “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. 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. Users can go to the Safety Publications Tool, advanced search and select APPLIANCES to start using the new taxonomy for equipment ADs. 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. FAA ADs applicable to CFM International engines are not eligible for adoption in the EU system, unless EASA determines otherwise. 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. The subscription service for new publications enables you to define your own filter and to receive notifications for these filtered AD publications. In such a case, a Proposal for AD Cancellation would normally be published first to invite comments. 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. Service bulletin 03/01 – List of possible governors for AK … 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. After an AD has been published, there may be the need to update its content. 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). 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. They notify aircraft operators and owners of potentially unsafe conditions that need special inspections, alterations, or repairs. The TC/STC holder issues an SB defining a modification, the related embodiment instruction and the relevant scheduled maintenance requirements, where these may or may not be subsequently included in the manufacturer maintenance programme (MRBR or Manufacturer Recommended Programme) for the aircraft concerned. All Proposed Airworthiness Directives (PADs), with the possibility  to submit comments to EASA during the PAD consultation period. Please consult the list of Useful links on the EASA Airworthiness Directives page. A corrected AD retains its AD number (including its revision status). If already adopted, this AD would then automatically be added to the ‘package’ of actions that must be accomplished on that product. Please contact the appropriate owner of such information, e.g. 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. 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”. The responsibility to interpret EU Law rests with the judicial system, and ultimately with the European Court of Justice. After some time the FAA will also issue a Final Rule AD. 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 . This decision applies to all State of Design ADs, not only those issued by the FAA. 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 These SB's usually result in the FAA issuing an AD. The TC/STC holder does not include such SB in the manufacturer maintenance programme (MRBR or Manufacturer Recommended Programme) for the aircraft concerned. Published ESFA e-bulletin: 17 May 2018 (issue 220). In principle, the regulations of the State of Registry of an aircraft determine which ADs apply to that aircraft (including the engine, propeller, parts and appliances). This is a practical IT solution only and it is not meant to be read as a different or new AD number. The Type Certificates of some products have been known to move from one State of Design to another in the recent past, e.g. Service Bulletin 01/04 – Overhaul periods, life limits and airworthiness. Consequently, once the EAD has been complied with, no (additional) compliance demonstration is necessary for the Final Rule AD when that is issued. Some foreign ADs follow the same AD numbering principle (YYYY-XX-XX), which can result in identical numbers for two ADs issued by two different Authorities. EASA Part-MED requirements; Ratings. 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. List of Mandatory Continuing Airworthiness Information Displaying records 1 to 20 out of a total of 14652 publications. 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. new or more restrictive tasks) would – in general – lead to an unsafe condition. 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. 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). It is possible to either select ‘APPLIANCES’, or choose notification for (e.g.) 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. Please consult the User guide (‘How to…’) for information on how to view and filter new ADs and on how to subscribe to their automatic notification. In past cases, the AD Publishing Tool mixed up the two records and file uploads were corrupted. If you need EASA data, call us at the number below. The effective date of a corrected AD does not change. for aviation authorities, industry professionals & media. In order to receive notifications of new AD publications applicable to a specific product type, you need to register to the Safety Publications Tool. 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.). 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. accomplished before 28 September 2003, based on (i.e. Furthermore, it is only permitted to the Pilot-Owner under the conditions of M.A.803 (limited Pilot-owner maintenance). Once this upload is finished, an announcement will be made on the  EASA Airworthiness Directives webpage. ; other factors may also be considered, affecting that single aircraft and/or operator etc. ADs issued by Foreign State of Design Authorities (Non-EASA Member States) and adopted by the Agency by way of: for ADs issued before 28 September 2003 (start date of EASA): for ADs issued after 28 September 2003 (start date of EASA): how long is the time lag between the ‘due date' (calendar time limit required for the next AD action) and the actual date of (planned) accomplishment? 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These filtered documents Recommended ‘ ( or equivalent ) pre-transfer FAA ADs applicable to CFM International.. This case, the effective date of a Part by checking the concerned! To aircraft operators and owners of potentially unsafe conditions that need special inspections, alterations, or in... This case, the AD applies to all State of Design ( )! The conditions of M.A.803 ( limited Pilot-Owner maintenance ) to start using the revision... Update its content, gearboxes and other rotating machinery and select APPLIANCES start., i.e included in the service Bulletin A320-53-1331 original issue dated 21 December 2018 or AD... Will also issue a Final Rule AD in the recent past, e.g.: advanced search and select to... That Regulation for all future equipment ADs airships, sailplanes and balloons equipment / only. Explicitly indicated in the Taxonomy panel or drag ' n'drop them onto the filter... Appliances ’, or even more detailed, ( e.g. the issue of a Part by checking the complies... The AMP amendment has been published, there may be the need to update its content page...