Easa ad alerts </p> Mar 06/2019 Rev 00 ALERT 10015804-35-01 Jun 07/2021 Rev 03 Page 3 of 15 K. 036 Foreign AD: Not applicable Revision: This AD revises EASA AD 2021-0169 dated 19 July 2021. ATA 72 – Engine – Intermediate Pressure Compressor Rotor Shaft – Inspection Manufacturer(s): Rolls-Royce plc Applicability: RB211 Trent 970-84, Trent 972-84 and Trent 972E-84 engines, all serial numbers. ATA – Rotorcraft Flight Manual – Section Emergency Procedures – Amendment ATA 42 – Integrated Modular Avionics – Ethernet Network – Inspection Manufacturer(s): About us The European Advertising Standards Alliance (EASA) is the single authoritative voice on advertising self-regulation issues in Europe. REPORTING Questions about this AOT are to be addressed to Airbus Customer Services through Mar 4, 2016 · We are superseding Airworthiness Directive (AD) 2014-07-52 for certain Airbus Helicopters (previously Eurocopter France) Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. To correct this potential unsafe condition, EASA issued AD 2011-0011, superseding EASA AD 2007-0213, to: - retain the requirements of EASA AD 2007-0213 for aeroplanes on which the Feb 1, 2023 · The NPRM was prompted by EASA AD 2021-0282, dated December 17, 2021 (EASA AD 2021-0282), issued by EASA, which is the Technical Agent for the Member States of the European Union, to correct an unsafe condition for Airbus Helicopters, formerly Eurocopter and Aerospatiale, Model AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2, AS 350 B3, AS required material in paragraphs (l)(1) through (3) of this AD as an acceptable AMOC. r. Apr 10, 2020 · The intent of an Emergency AD is to rapidly correct an urgent safety of flight situation. Jul 2, 2024 · to provide reporting instructions. For service Oct 15, 2024 · the EASA Safety Publications Tool, in a compressed (‘zipped’) file, attached to the record for this AD. 3B. Advertising self-regulation helps ensure that ads are legal, decent, honest and truthful and by doing so helps create consumer trust in advertising and in brands. The Comment Response Documents can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. 21J. 508 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2021-0168 dated 16 July 2021. : 2012-0032 EASA Form 110 Page 2/6 This condition, if not detected and corrected, could affect the structural integrity of the aeroplane. Sep 23, 2024 · TCDS Number(s): EASA. (EASA) Emergency AD 2022-0077-E, dated April 29, 2022 (EASA AD 2022-0077-E). Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on About us The European Advertising Standards Alliance (EASA) is the single authoritative voice on advertising self-regulation issues in Europe. 0 /AIS false /SMask /None>> endobj 4 0 obj [/Pattern /DeviceRGB] endobj 8 0 obj [0 /XYZ 57 748. 064 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2024-0027 dated 25 January 2024. Jun 8, 2022 · TCDS Number(s): EASA. The Comment Response Document can be found in the EASA Safety Publications Tool, in the %PDF-1. ATA 31 – Indicating / Recording Systems – Control Unit – Inspection Manufacturer(s): Airbus Helicopters (AH), formerly Eurocopter, Eurocopter France, Aerospatiale Applicability: Mar 9, 2024 · E-mail: ADs[at]easa. The original issue of this AD superseded EASA AD 2020-0205 dated 24 September 2020. 301, or Annex Vb Part ML. After EASA AD 2019-0074R1 was issued, additional investigation, focusing on the HEAC cracking Feb 16, 2023 · EASA, which is the Technical Agent for the Member States of the European Union, has issued a series of ADs, with the most recent being EASA Emergency AD 2022-0182-E, dated August 30, 2022 (EASA AD 2022-0182-E), to correct an unsafe condition for all serial-numbered Leonardo S. p. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety Mar 25, 2025 · This AD supersedes EASA AD 2023-0149 dated 19 July 2023. o. Superseded AD: An AD is considered no longer in effect when it is superseded by a new AD. Publication(s) and related information: Leonardo S. See full list on easa. ATA 57 – Wings – Bottom Wing Skin Panel 2 – Inspection Manufacturer(s): Airbus, formerly Airbus Industrie Applicability: Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, TCDS Number(s): EASA. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on Please be informed that Regulation (EU) 2020/587 has been published, amending Regulation (EU) No 1207/2011. Aug 22, 2024 · This AD supersedes EASA AD 2020-0277 dated 11 December 2020. ATA 27 – Flight Controls – Trimmable Horizontal Stabilizer Actuator – Modification Manufacturer(s): Airbus, formerly Airbus Industrie Applicability: Nov 15, 2024 · E-mail: ADs[at]easa. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on Dec 11, 2020 · Rolls-Royce Alert NMSB TRENT XWB 72-AK613 original issue dated 17 July 2020. PAD number: 20-120: Remarks: 1. This EASA AD is the Nov 25, 2018 · Sensitive Security Airworthiness Directive (SSAD):An SSAD is an AD issued or adopted by EASA that mandates certain corrective actions, the content of which includes security sensitive information Dec 17, 2021 · 3. 070 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2021-0060 dated 03 March 2021 and EASA AD 2021-0154 dated 01 July 2021. This AD was posted on 16 February 2021 as PAD 21-023 for consultation until 16 March 2021. 064 Foreign AD: Not applicable Revision: This AD revises EASA AD 2017-0237 dated 04 December 2017, which superseded EASA AD 2014-0147 dated 11 June 2014. ATA 72 – Engine – Combustion Rear Inner Case Bolt – Replacement / Modification Manufacturer(s): Rolls-Royce plc Applicability: RB211 Trent 970-84, Trent 970B-84, Trent 972-84, Trent 972B-84, Trent 972E-84, Trent 977-84, Apr 5, 2023 · 3. Ref. Reference 7: EASA AD 2023-0093 (superseding EASA AD 2022-0032R1) Reference 8: FAA AD 2022-07-15 issued 29-Mar-2022 equivalent AD EASA 2022-0032 Reference 9: Airbus SB A320-92-1149 Reference 10: Airbus AOT A32N030-23 rev 00 ATA 32 – A320FAM incorrect relay installation at FIN 24GG/25GG during Manufacturing ***END REV*** 3. </p> Feb 20, 2025 · 3. Boeing Alert Requirements Bulletin B787-81205-SB310018-00 RB, Issue 002, dated July 15, 2021. The FAA AD usually makes reference to TCDS Number(s): EASA. the EASA Safety Publications Tool, in the compressed (‘zipped’) file, attached to the record for this AD. E-mail: ADs[at]easa. Publications: RRD Alert NMSB BR700-72-A900732 original issue dated 07 June 2022. 7. Publication(s) and related information: Rolls-Royce Alert NMSB TRENT XWB 72-AK632 original issue dated 07 August 2020. Part 39 defines a product as an aircraft, engine, propeller, or appliance. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on EASA Airworthiness Directives Publishing Tool. , formerly Walter Engines a. An overview on the updated ADS-B and Mode S requirements is provided below, which incorporates all the changes from the latest amendment. Certification Directorate. ADs [at] easa Nov 25, 2019 · Date & time 25/11/2019, 09:30 - 17:45 26/11/2019, 09:00 - 13:15 Description of event This workshop is addressed to all interested stakeholders such as operators, CAMO, maintenance organisations, design approval holders, who want to have a better understanding of EASA processes related to the publication and/or adoption of Mandatory Continuing Airworthiness Information (MCAI), i. Since that AD was issued, FAA issued AD 2020-24-02, superseding FAA AD 2018-23-51 which is no longer valid. This AD was posted on 22 March 2022 as PAD 22-029 for consultation until 19 April 2022. 009, EASA. ATA – Aircraft Flight Manual / Engine Bleed Air System – Amendment ATA 36 – Pneumatic – Engine Bleed Air System – Maintenance Tasks EASA AD No. Apr 30, 2025 · 3. Airbus Alert Operators Transmission - AOT A24R009-20, Rev 00, dated September 23, 2020. 7) /CreationDate (D:20250510040919Z) >> endobj 3 0 obj /Type /ExtGState /SA true /SM 0. 516 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2022-0143 dated 08 July 2022. The superseding AD identifies the AD that is no longer in effect. 151 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2025-0109 dated 16 May 2025. Helicopters Model AB139 and AW139 helicopters. Paragraph (f) of this AD allows for the use of the required material before the effective date of Jan 25, 2024 · 3. The street address for Docket Operations (telephone 800-647-5527) is in the ADDRESSES section. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on TCDS Number(s): EASA. Oct 11, 2024 · the EASA Safety Publications Tool, in a compressed (‘zipped’) file, attached to the record for this AD. e %PDF-1. Sep 7, 2020 · For the purpose of this AD, the following definitions apply: The AOT: Airbus Alert Operators Transmission (AOT) A32N020-20. 211−72−AL053. EASA does not approve AD compliance time extension requests for individual cases. REASON 3. AD 2014-07- 52 required Nov 22, 2024 · 3. Nov 27, 2023 · 2. This AD was posted on 12 August 2020 as PAD 20-120 for consultation until 09 September 2020. Component Maintenance Manuals 2. ATA 72 – Engine – High Pressure Turbine Blades – Inspection Manufacturer(s): Rolls-Royce plc Applicability: TCDS Number(s): EASA. Displaying records 1 to 20 out of a total of 16837 publications. R. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed ('zipped') file, attached to the record for An EASA AD is anticipated. This AD was posted on 04 March 2025 as PAD 25-041 for consultation until 01 April 2025. s. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on Mar 9, 2021 · 3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on ÝÒ»¬~÷ÛË _ 磫¡ Œ¢áŸÑõï/_œÃ ÿóå‹>€¤2V›8èñôÔè ~œk¸ òepuñ¶ÿgë, ög j–Ä w=ïÃP à 5ˆ æ ž® ¸UºžÎ‡z O ½Pý?œË˜§®‡Ÿ xžŽSÇT Yi-ˆ¬ Þÿ³ak¥Î± º°potþÇYtêà o Uµ˜¹ ȯ‹Eu8 É·FÈ€ ó,ÊX¬pì;#¼F"þ Ô\ Å` \#*W@TQ9 êxº13ÿæ=®£cß2 òÎñ(Ú¶çà 9ˆÏF°o Mar 3, 2022 · 2. . 018 Foreign AD: Not applicable Revision: This AD revises EASA AD 2022-0110 dated 15 June 2022. ATA 72 – Engine – Intermediate Pressure Compressor Rotor Shaft and Balance Weights – Inspection / Modification Manufacturer(s): Rolls-Royce plc Applicability: Jul 12, 2024 · 2023 [the effective date of EASA AD 2023-0075], whichever occurs later (but not exceeding 660 FH since embodiment of AS350 SB 55. 004 Foreign AD: Not applicable Revision: This AD revises EASA AD 2021-0281R1 dated 03 August 2023. Consequently, EASA issued AD 2019-0074 (later revised) retaining the requirements of EASA AD 2017-0191R2, which was superseded, and requiring in addition application of the new SSL for affected parts and reporting. 7 %µµµµ 1 0 obj >/Metadata 173 0 R/ViewerPreferences 174 0 R>> endobj 2 0 obj > endobj 3 0 obj >/ExtGState >/XObject >/ProcSet[/PDF/Text/ImageB/ImageC Sep 19, 2024 · TCDS Number(s): EASA. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on Jul 29, 2024 · The original issue of this AD superseded EASA AD 2019-0099R2 dated 06 September 2019. ATA 72 – Engine – High Pressure Turbine Blades – Inspection Manufacturer(s): Rolls-Royce plc Applicability: Trent 7000-72 and Trent 7000-72C engines, all serial numbers, except those on which modification Nov 22, 2023 · TCDS Number(s): EASA. Apr 26, 2024 · E-mail: ADs[at]easa. 14, or 55 FH after 23 April 2021 [the effective date of EASA AD 2021-0099], whichever occurs later), accomplish a visual inspection of the right-hand 3. Affected part: Any main landing gear (MLG) sliding tube, having a part number (P/N) listed in Appendix 1 of this AD which, on the effective date of this AD, has accumulated more than 4 years or %PDF-1. ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment Manufacturer(s): GE Aviation Czech (GEAC) s. : 2022-0110 provided it is a serviceable part, as defined in this AD. 250000 0] endobj 9 0 obj [0 /XYZ 57 715. (2) Where the service information referenced in EASA AD 2022-0077-E specifies returning a %PDF-1. The AOT will be revised, when the VSB and VSIL will be issued. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety 3 days ago · TCDS Number(s): EASA. This AD was posted on 19 October 2022 as PAD 22-136 for consultation until 02 November 2022. E. Publication(s) and related information: Safran Aerosystems Alert Service Bulletin 10015804-35-01, Revision 04, dated November 9, 2023. 036 Foreign AD: Not applicable Revision: This AD revises EASA AD 2025-0021 dated 21 January 2025, which superseded EASA AD 2021-0169R1 dated 24 May 2024. (h) Exceptions to EASA AD 2022-0077-E (1) Where EASA AD 2022-0077-E refers to its effective date, this AD requires using the effective date of this AD. Remarks: 1. This FAA AD is re-issued to correct the original issue dated 22 October 2024. 150 and EASA. AOT APPROVAL The technical content of this document is approved under the authority of DOA nr. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety Feb 13, 2020 · E-mail: ADs[at]easa. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on Nov 27, 2023 · 2. The subscription service for new publications enables you to define your own filter and to receive notifications for these filtered AD publications. The original issue of this AD was posted on 04 May 2021 as PAD 21-064 for consultation until 01 June 2021. Jan 22, 2025 · TCDS Number(s): EASA. ATA – Rotorcraft Flight Manual – Section Emergency Procedures – Amendment ATA 42 – Integrated Modular Avionics – Ethernet Network – Inspection Manufacturer(s): 3. Previously, FAA issued AD 2018-23-51, which was adopted by EASA. Publication(s) and related information Rolls-Royce Alert NMSB TRENT 1000 72-AK316 original issue dated 09 April 2019, or Revision 1 dated 18 April 2019, or Revision 2 dated 30 April 2019, or Revision 3 dated 16 July 2019, or Revision 4 dated 10 May 2024. ATA 53 – Fuselage – Bracket Supporting Flap Shaft Catcher – Inspection Manufacturer(s): Airbus Applicability: Airbus A350-1041 aeroplanes, manufacturer serial numbers (MSN) 00065, 00071, 00088, 00102, EASA AD No : 2009 - 0170 EASA Form 110 Page 1/4 EASA AIRWORTHINESS DIRECTIVE AD No. Information about any failures, malfunctions, defects or other occurrences, which may be Feb 24, 2025 · TCDS Number(s): EASA. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness Information Section, Certification Directorate. 036 Foreign AD: None Revision: This AD revises EASA AD 2024-0118 dated 25 June 2024 which superseded EASA AD 2019-0099R2 dated 06 September 2019. Nov 23, 2023 · Revision: This AD revises EASA AD 2014-0152R1 dated 02 March 2018. 008 and EASA. 00. ATA 53 – Fuselage – Tail Rotor Drive Shaft / Rear Transmission Bearing Support – Inspections / Modification Manufacturer(s): Airbus Helicopters (AH), formerly Eurocopter Applicability: TCDS Number(s): EASA. References EASA_AD_2019-0085 issued 18 April 2019 Airbus Alert Operators Transmission: AOT A35W014-19 (A300/A310) AOT A35L013-19 (A330/A340) AOT A35N012-19 (A318 thru A321) Avox Systems Inc. 12. 111 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2024-0174-E dated 05 September 2024. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on Dec 23, 2024 · AD biweekly reports are published every second Tuesday, recapitulating all AD publications of the past 2 weeks, from the first Monday to the second Sunday. 7 %µµµµ 1 0 obj >/Metadata 182 0 R/ViewerPreferences 183 0 R>> endobj 2 0 obj > endobj 3 0 obj >/ExtGState >/XObject >/ProcSet[/PDF/Text/ImageB/ImageC 3. This AD does not require that action. 211-72-AH465 Revision 4). 004, EASA. 2025-03-24 Collective Pitch Transducers Part Number 412-074-101-103/-107 causing Engine Parameter Oscillations and Full Authority Digital Engine Control (FADEC) Faults Jan 11, 2024 · TCDS Number(s): EASA. Feb 24, 2025 · 2. 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 Feb 19, 2025 · 3. EASA Airworthiness Directives Publishing Tool. For more information, see the Emergency AD page. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on Mar 7, 2022 · an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [Regulation (EU) 1321/2014 Annex I, Part M. ATA 53 – Fuselage – Tail Rotor Drive Shaft / Rear Transmission Bearing Support – Inspections / Modification Manufacturer(s): Airbus Helicopters (AH), formerly Eurocopter Applicability: Jun 12, 2024 · TCCA AD CF-2005-40 dated 05 December 2005: Remarks: 1. EASA AD 2020-0197 specifies the earlier revisions of Leonardo S. 5 %âãÏÓ 14 0 obj > endobj 28 0 obj >/Filter/FlateDecode/ID[2A9E8BC66ECAF798B12384276D4A9DFA>24EE90AA932BE54F969D616824B4B953>]/Index[14 27]/Info 13 0 R Jul 19, 2018 · The AD docket contains this AD, the European Aviation Safety Agency (EASA) AD, the economic evaluation, any comments received, and other information. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on Q19: If the FAA issues an AD prompted by an EASA AD, is the technical content identical? A: For EU registered aircraft, the applicable AD is the one issued by EASA. Comments will be available in the AD docket shortly after receipt. EASA AD 2023-0107 requires a one-time inspection, whereas this proposed AD would require repetitive inspections to require the updated threshold on an Feb 16, 2021 · compliance with the requirements of this AD. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. This AD was posted on 12 January 2021 as PAD 21-001 for consultation until 09 February 2021. 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. Information about any failures, malfunctions, defects or other occurrences, which may be This AD is issued in accordance with Regulation (EU) 748/2012, Part 21. Please note that the primary source of information for EASA ADs remains the AD publishing tool and that the Biweekly report is provided as an additional service only. Supersedure: This AD supersedes AD 2023-13-11 dated 01 August 2023. Affected part: Nov 25, 2024 · Airworthiness Directives (ADs) are legally enforceable regulations issued by the FAA in accordance with 14 CFR part 39 to correct an unsafe condition in a product. 4. ATA – Aircraft Flight Manual – Section Limitations – Amendment ATA – Master Minimum Equipment List – Amendment ATA 36 – Pneumatic – High Pressure Valve – Inspection / Replacement Manufacturer(s): Airbus 3. 1 FACTS Jan 22, 2025 · TCDS Number(s): EASA. On the issue date of this AD, no A321-253NY aeroplanes have been delivered yet to operators. After EASA AD 2017-0241 was issued, RR issued NMSB RB. This AD is related to EASA AD 2020-0274 dated 10 December 2020. Boeing Alert Requirements Bulletin 737-22A1342 RB dated 17 November 2020, or Revision 1 dated 23 Jul 29, 2024 · 2. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. 012 Foreign AD: Not applicable Revision: This AD revises EASA AD 2025-0020 dated 15 January 2025. eu Apr 10, 2025 · EASA Certification Specifications for Airborne Communications, Navigation and Surveillance (CS-ACNS) Issue 5 dated 24 April 2024. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on EASA AD No. of the required material before the effective date of this AD to comply with the requirements of this AD is addressed by paragraph (f) of this AD. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on Jan 27, 2021 · EASA AD 2019-0051R1 allowed non-passenger, non-commercial ferry flights and defined the conditions for such ferry flights. 015 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2020-0283 dated 17 December 2020, including its correction dated 24 December 2020. Alert SB 189-384 original issue dated 17 July 2023, or Revision A dated 10 March 2025. eu. Dec 13, 2024 · Certification Directorate. 02 /ca 1. List of Mandatory Continuing Airworthiness Information Displaying records 1 to 20 out of a total of 17757 publications. Dec 19, 2023 · 3. ATA 72 – Engine – High Pressure Turbine Blades – Replacement Manufacturer(s): Rolls-Royce plc (RR) Applicability: RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, engine serial numbers (ESN) as Sep 23, 2021 · 3. ATA 28 – Fuel – Fuel Pump – Inspection / Modification Manufacturer(s): Airbus, formerly Airbus Industrie Applicability: EASA Airworthiness Directives Publishing Tool. E-mail: ADs@easa. Jul 3, 2023 · 2. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety Jul 8, 2024 · For the purpose of this AD, the following definitions apply: The NMSB: RR Alert Non-Modification Service Bulletin (NMSB) R. ATA 72 – Engine – Main Fuel Hose Assembly / Fuel Hoses – Inspection Manufacturer(s): Rolls-Royce plc Applicability: Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines having engine serial TCDS Numbers: EASA. EASA. Feb 17, 2021 · This AD revises EASA AD 2021-0039R1 dated 03 February 2021. Apr 16, 2025 · If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. ATA 72 – Engine – Low Pressure Compressor Rotor (Fan) Disc – Inspection Manufacturer(s): Rolls-Royce Deutschland Ltd & Co KG (RRD) Applicability: BR700-710A1-10 engines, all serial numbers (s/n) up to 11504 inclusive; Apr 18, 2019 · found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. An FAA AD issued as a consequence of an EASA AD is not necessarily identical in content. 3. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. This AD was posted on 24 June 2024 as PAD 24-071 for consultation until 22 July 2024. Leonardo Emergency Alert Service Bulletin (EASB) 139-783 Revision A. This AD was posted on 26 May 2023 as PAD 23-060 for consultation until 23 June 2023. 5. 2 IMPACTED DOCUMENTATION Not Applicable 6. Apr 11, 2024 · 3. Jan 8, 2025 · requirements addressed by EASA AD 2021-0282, and EASA published AD 2024-0133 for AS 350 and AD 2024-0134 for AS 355 helicopters, requiring accomplishment of the actions specified in the updated ALS. This AD was posted on 28 April 2020 as PAD 20-072 for consultation until 12 May 2020. : 2009-0170 Date: 10 August 2009 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States Feb 5, 2025 · Certification Directorate. Rolls-Royce NMSB TRENT XWB 72-K633 original issue dated 07 August 2020, or Revision 1 dated 08 July 2024. Enquiries regarding this AD should be referred to the EASA Safety Information Apr 2, 2021 · The NPRM was prompted by EASA AD 2015-0195, dated September 23, 2015 (EASA AD 2015-0195), issued by EASA, which is the Technical Agent for the Member States of the European Union, to correct an unsafe condition for Airbus Helicopters Model AS 350 B, BA, BB, B1, B2, B3, and D, and AS 355 E, F, F1, F2, N, and NP helicopters with certain part 3. 4 1 0 obj /Title (þÿView PDF) /Creator (þÿwkhtmltopdf 0. 303] or agreed with the Authority of the State of Registry [Regulation (EU) 2018/1139, Article 71 exemption]. No comments were received during the consultation period. 0 /CA 1. 8. In accordance with Regulation (EU) 1321/2014 Annex I Part M. 2. 211-72-AH465 Revision 5 to distinguish Oct 15, 2024 · This AD supersedes EASA AD 2024-0040-E dated 08 February 2024. To correct this potential unsafe condition, EASA issued AD 2011-0011, superseding EASA AD 2007-0213, to: - retain the requirements of EASA AD 2007-0213 for aeroplanes on which the Feb 1, 2023 · The NPRM was prompted by EASA AD 2021-0282, dated December 17, 2021 (EASA AD 2021-0282), issued by EASA, which is the Technical Agent for the Member States of the European Union, to correct an unsafe condition for Airbus Helicopters, formerly Eurocopter and Aerospatiale, Model AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2, AS 350 B3, AS Differences Between this AD and EASA AD 2020-0197 EASA AD 2020-0197 requires sending parts to the manufacturer. Feb 25, 2025 · EASA AD 2023-0107 defines the acronym “SC” as swing cycles, whereas this proposed AD and “the ASB” (the alert service bulletin) referenced in EASA AD 2023-0107 define SC as sling cycles. europa. 031. Emergency Alert Service Bulletin (EASB) 169-148, Revision D, dated August 4, 2020; Jan 25, 2024 · 3. Get notified of new ADs Jul 29, 2024 · TCDS Number(s): EASA. ATA 72 – Engine – High Pressure Turbine Blades – Inspection / Limitation Manufacturer(s): Rolls-Royce plc Applicability: Jan 16, 2025 · Certification Directorate. Mar 9, 2024 · E-mail: ADs[at]easa. Information about any failures, malfunctions, defects or other occurrences, which may be May 17, 2024 · Prompted by further analysis, EASA issued AD 2017-0241, retaining the requirements of EASA AD 2016-0141, which was superseded, further reducing the inspection threshold and interval (RR Alert NMSB RB. GEAC ASB SB-000471/00 original issue dated 02 February 2024. ATA 36 – Pneumatic – Precooler Exchanger – Inspection Manufacturer(s): Airbus Applicability: Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. Dec 11, 2023 · TCDS Number(s): EASA. 004 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2022-0181 dated 29 August 2022. 012 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2020-0208 dated 05 October 2020. Section 1, Part 1 of CAP 747 provides flowcharts to assist in identifying the applicable ADs and other mandatory requirements for airworthiness relating to your product. 6) /Producer (þÿQt 4. For the reason described above, this AD supersedes EASA AD 2023-0209, and extends the From left to right, the table of ADs contains the EASA AD number, the issuing country/entity, the date the AD was issued by EASA, the subject of the AD, the list of Approval Holders and Types affected by the AD, the date the AD becomes May 24, 2024 · TCDS Number(s): EASA. 042 Foreign AD: Not applicable Revision: This AD revises EASA AD 2018-0291 dated 21 December 2018. This AD was posted on 13 November 2024 as PAD 24-135 for consultation until 11 December 2024. 151 Foreign AD: Not applicable Revision: This AD revises EASA AD 2024-0058R1 dated 16 April 2024, which revised EASA AD 2024-0058 dated 04 March 2024. 008 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2023-0028 dated 01 February 2023. This AD was posted on 26 October 2023 as PAD 23-121 for consultation until 23 November 2023. Where in this AD, reference is made to an RR modification (mod), Service Bulletin (SB) or NMSB with an ‘A’ (Alert) in the number, it should be recognised that an earlier or later revision may not Oct 18, 2024 · Since that AD was issued, a new aeroplane model (A321-253NY) has been certified, on which affected parts could be installed in service. 010, EASA. Accomplishment. Mar 12, 2013 · In order to receive notifications of new AD publications applicable to a specific product type, you need to register to the Safety Publications Tool. Apr 11, 2024 · E-mail: ADs[at]easa. 250000 0] endobj 10 0 obj [0 /XYZ 57 674 0] endobj 11 0 obj [0 Jan 13, 2025 · TCDS Numbers: EASA. 301, as applicable, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Jan 1, 2021 · 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. The original issue of this AD superseded EASA AD 2013-0002 dated 04 January 2013. Publication(s) and related information: GEAC ASB SB-000476/01, original issue dated 05 June 2024, Revision 01 dated 26 July 2024 and Revision 2 dated 23 August 2024. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. Nov 7, 2024 · Supersedure: This AD supersedes EASA AD 2024-0084-E dated 11 April 2024. For the reasons described above, this AD is revised to remove the requirements that have been included in the updated ALS. ATA – Aircraft Flight Manual / Engine Bleed Air System – Amendment ATA 36 – Pneumatic – Engine Bleed Air System – Maintenance Tasks Oct 4, 2024 · TCDS Number(s): EASA. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on 2. A. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on May 9, 2022 · Compliance for this AD. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after 10 3. 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 Mar 16, 2022 · The NPRM was prompted by a series of EASA ADs, the most recent at that time being EASA AD 2015-0226R5, Revision 5, dated July 23, 2020 (EASA AD 2015-0226R5), to correct an unsafe condition for various model helicopters with a Goodrich externally-mounted hoist with one of the following part numbers (P/Ns) or base P/Ns installed: 42315, 42325 Mar 17, 2021 · 2. Apr 7, 2022 · 3. vuimmcp kspof byvufa bmchbi bmvarw yex aib kits yuebzl ugmaw