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EASA Regulations & Airworthiness Directives

Browse 5,158 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350222 Airbus A330220 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941132 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787115 Show all...

EASA AD US-2022-21-06

Engine - Low Pressure Turbine Stage 5 Discs - Removal / Replacement

The Federal Aviation Administration's Airworthiness Directive 2022-21-06 addresses certain General Electric Company CF34-8C and CF34-8E model turbofan engines. It focuses on the removal and replacement of the low-pressure turbine (LPT) stage 5 disk, part number 4117T14P02, due to a reported crack in the forward arm area. This directive aims to ensure continued airworthiness and safety of affected engines.

Airworthiness Directive

General Electric CF34-8

EASA AD US-2022-22-12

NOT ADOPTED - EASA DECISION ATTACHED

The document titled NOT ADOPTED - EASA DECISION ATTACHED is an official position from EASA regarding FAA Airworthiness Directive 2022-22-12. This FAA AD applies to certain helicopters modified by FAA STC SR01298NY, including Bell Textron Inc. type designs and Leonardo AB412 helicopters. EASA has determined that FAA AD 2022-22-12 is not eligible for adoption within the European Union because the FAA STC SR01298NY is not validated by EASA for all affected helicopter types, specifically Leonardo AB412 helicopters.

Agency Decision

Bell Textron Inc. (Bti) 204B
Bell Textron Inc. (Bti) 205
Bell Textron Inc. (Bti) 210
Bell Textron Inc. (Bti) 212
Bell Textron Inc. (Bti) 412
Leonardo S.P.A. Helicopters AB212
Leonardo S.P.A. Helicopters AB412
Mcdermott 214 Holdings, 214
Bell Textron Inc. Helicopter
Leonardo AB412

EASA AD 2022-0219

Engine — Hot Strut Module — Inspection

The document titled Engine — Hot Strut Module — Inspection is an informational Airworthiness Directive record created by EASA regarding the Europrop International GmbH TP400-D6 engine. It clarifies that no Europrop TP400-D6 engines are currently in civil service, so no public AD exists. The document serves as a recommendation for military authorities responsible for aircraft equipped with TP400-D6 engines to issue their own applicable ADs.

Airworthiness Directive

Epi Europrop International Gmbh TP400-D6

EASA AD 2021-0089R1

Engine — Propeller Gearbox Shaft Flange — Inspection

EASA Airworthiness Directive 2024-0198 is an informational document concerning the inspection of the propeller gearbox shaft flange on Europrop International GmbH TP400-D6 engines. This directive applies specifically to military aircraft equipped with TP400-D6 engines, as there are currently no such engines in civil service. The document serves as a recommendation for military authorities to issue their own legally binding airworthiness directives.

Airworthiness Directive

Epi Europrop International Gmbh TP400-D6

EASA AD 2022-0213R1

Doors — Passenger Door / External Handle Mechanism — Cleaning / Lubrication

EASA Airworthiness Directive 2022-0213R1 is an updated regulatory requirement addressing the cleaning and lubrication of the passenger door external handle mechanism on Airbus A318, A319, A320, and A321 aircraft. The directive targets specific affected doors where corrosion protection compound caused sticky mechanisms, potentially impairing door operation and emergency evacuation. This AD applies to all manufacturer serial numbers of the listed Airbus models.

Airworthiness Directive

Airbus A318
Airbus A319
Airbus A320
Airbus A321

EASA AD 2022-0218

Equipment / Furnishings – Fuselage / Belly Fairing Mounted Emergency Evacuation Escape Slides – Replacement

EASA Airworthiness Directive 2022-0218 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses the replacement of fuselage and belly fairing mounted emergency evacuation escape slides manufactured by Collins with specific part numbers. The directive aims to ensure the continued airworthiness and safety of these aircraft by mitigating risks associated with slide seam degradation.

Airworthiness DirectiveSuperseded

Airbus A380841842861

EASA AD US-2022-20-15

Wings - Centre Wing Box Rear Spar, Lower Skin, Lower Chord - Inspection / Repair

Airworthiness Directive AD 2022-20-15 is a final rule issued by the Federal Aviation Administration (FAA) addressing all Boeing Company Model 757 airplanes. It mandates repetitive inspections and repairs of cracks found in the fastener holes of the center wing box rear spar, lower skin, and lower chord. The directive aims to ensure the structural integrity of these aircraft by detecting and correcting potential cracking issues.

Airworthiness Directive

Boeing 757

EASA SIB 2022-09

WITHDRAWN — RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin 2022-09 is an informational document regarding the uncontrolled re-entry of the large space debris from the Rocket Long March 5B (CZ-5B) launched on 31 October 2022. The debris, weighing between 17 and 23 tons, is expected to re-enter Earth's atmosphere on 4 November 2022, potentially affecting several southern European Flight Information Regions. This bulletin does not mandate any operational directives but provides situational awareness to aviation stakeholders.

Safety Information Bulletin

EASA AD G-2022-0019

Doors — Passenger Door Inner Skin, Edge Member and Seal Carrier adjacent to Roller Brackets — Inspection

The Civil Aviation Authority Proposed Airworthiness Directive 2002 addresses inspection requirements for the passenger door inner skin, edge member, and seal carrier adjacent to roller brackets on BAE Systems Jetstream 4100 series aeroplanes. This directive applies to all models and serial numbers of the Jetstream 4100 series and mandates inspections to detect potential cracking in critical door components.

Airworthiness Directive

Bae Systems (Operations) Jetstream 4100
BAE Systems Jetstream 4100

EASA AD US-2022-19-15

Superseded by FAA AD 2024-05-11

FAA Airworthiness Directive 2022-19-15 is a final rule correction applicable to certain International Aero Engines, LLC PW1000G series turbofan engines including models PW1122G-JM, PW1124G1-JM, PW1124G-JM, PW1127G1-JM, PW1127GA-JM, PW1127G-JM, PW1129G-JM, PW1130G-JM, PW1133GA-JM, and PW1133G-JM. The directive mandates ultrasonic inspections of the high-pressure turbine first-stage and second-stage disks to prevent uncontained disk failures. This correction updates incorrect table references in the original service bulletin instructions.

Airworthiness Directive

International Aero Engines PW1100
International Aero Engines PW1400

EASA AD US-2022-21-05

Auto Flight - Auto-Throttle Computer - Built-in Test Equipment Tests

Airworthiness Directive 2022-21-05 is a final rule issued by the Federal Aviation Administration affecting certain Boeing 737-300, -400, and -500 series airplanes. It addresses a safety issue where a spoiler sensor failure may go undetected by the autothrottle computer, potentially leading to asymmetric thrust and uncommanded roll. The directive mandates repetitive built-in test equipment (BITE) tests of the autothrottle computer to detect and correct spoiler sensor failures.

Airworthiness Directive

Boeing 737300400500

EASA AD BR-2022-04-01R1

Flight Controls - Electrical Harnesses W126 and W127 - Inspection

The Brazilian Airworthiness Directive AD No. 2022-04-01R1 is an official regulatory document issued by ANAC that mandates inspection and correction of the electrical harnesses W126 and W127 routing on Embraer ERJ 170 series aircraft, including models 170-100 LR, SE, STD, SU, and 170-200 LR, STD, SU, LL with serial numbers 17000002 through 17000914. This directive aims to ensure proper segregation of critical electrical harnesses to maintain aircraft safety and compliance with airworthiness standards.

Airworthiness Directive

Embraer ERJ 170

EASA AD CF-2022-59

Maintenance Requirements Manual, Part 2 Airworthiness Limitation Items — Introduction of New Section 7-00 — Candidate Certification Maintenance Requirements Limitations

Maintenance Requirements Manual, Part 2 Airworthiness Limitation Items — Introduction of New Section 7-00 — Candidate Certification Maintenance Requirements Limitations is a Canadian Airworthiness Directive CF-2022-59 issued by Transport Canada. It applies to De Havilland Aircraft of Canada Limited model DHC-8-401 and -402 aeroplanes of all serial numbers. The directive mandates the incorporation of a new section in the Maintenance Requirements Manual that introduces Candidate Certification Maintenance Requirements limitations for continued airworthiness.

Airworthiness Directive

De Havilland Canada DHC-8
De Havilland DHC-8-401
De Havilland DHC-8-402

EASA AD 2021-0092R1

Pneumatic — Cross-Bleed Ducts — Inspection / Replacement

EASA Airworthiness Directive 2021-0092R1 is an updated regulatory requirement addressing inspection and replacement of cross-bleed ducts on Airbus A380-841, A380-842, and A380-861 aeroplanes. It targets specific part numbers of cross-bleed ducts prone to cracking due to manufacturing misalignment, which can lead to bleed leaks and structural damage. The directive mandates inspections and corrective actions to ensure continued airworthiness of affected aircraft.

Airworthiness Directive

Airbus A380

EASA AD US-2022-18-11

Superseded by FAA AD 2023-17-14

FAA Airworthiness Directive 2022-18-11 is a final rule affecting all Boeing Company Model 777 airplanes, including the 777-200, -200LR, -300, -300ER, and 777F variants. It addresses the discovery of cracks in the front spar lower chord during underwing longeron replacements and mandates repetitive inspections and modifications to critical structural components at station 1035. The directive aims to prevent fuel leaks, fire hazards, and potential structural failures.

Airworthiness Directive

Boeing 777

EASA AD AD-F100-98

Aerospace NDI Pty Ltd - Main Landing Gear Pistons Overhaul - Inspection / Removal

The Aerospace NDI Pty Ltd - Main Landing Gear Pistons Overhaul - Inspection / Removal is an Australian Civil Aviation Safety Authority Airworthiness Directive (AD/F100/98) addressing Fokker Services F100 (F28 Mk 100) series aeroplanes equipped with Goodrich Main Landing Gear pistons overhauled by Aerospace NDI Pty Ltd. It mandates inspection and removal of specific pistons treated with AeroNikl or Atotech plating processes due to potential safety risks. The directive applies to pistons identified by certain serial numbers and overhaul dates between October 2019 and November 2021.

Airworthiness Directive

Fokker F28
Fokker F100

EASA AD AD-F28-93

Aerospace NDI Pty Ltd - Main Landing Gear Pistons Overhaul - Inspection / Removal

The Aerospace NDI Pty Ltd - Main Landing Gear Pistons Overhaul - Inspection / Removal is an Airworthiness Directive issued by the Civil Aviation Safety Authority of Australia concerning Fokker Services F28 Mark 0070 aircraft equipped with specific Goodrich Main Landing Gear part numbers and pistons overhauled by Aerospace NDI Pty Ltd. It mandates inspection and removal from service of pistons treated with AeroNikl or Atotech plating processes within specified serial numbers. The directive addresses safety concerns related to hydrogen embrittlement and potential piston failure.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070

EASA AD 2022-0215

Engine — Bearing Spring Finger Housing — Inspection

EASA Airworthiness Directive 2022-0215 is an airworthiness directive addressing CFM International LEAP-1B engine models installed on Boeing 737-8, 737-8200, and 737-9 aircraft. It mandates inspection and monitoring of the bearing No. 3 spring finger housing to detect wear that could cause non-synchronous vibrations and potential engine failure. The directive applies to all serial numbers of affected LEAP-1B engines and prohibits installation of certain affected parts.

Airworthiness Directive

CFM International LEAP-1B
Boeing 737-8
Boeing 737-8200
Boeing 737-9

EASA AD CF-2022-47R1

Flight Controls — Multi-Function Spoiler (MFS) — Replacement of MFS 1, MFS 2, and MFS 3 Anti-Rotation Plates

Canadian Airworthiness Directive CF-2022-47R1 addresses the replacement of Multi-Function Spoiler (MFS) anti-rotation plates on Bombardier Inc. model BD-700-2A12 aircraft, serial numbers 70006 through 70129. This directive mandates inspection and replacement of MFS 1, MFS 2, and MFS 3 anti-rotation plates to prevent failure due to thin wall design. The directive updates previous requirements to include credit for prior incorporation of Bombardier Service Bulletin 700-27-7504 Basic Issue.

Airworthiness Directive

Bombardier BD-7002A12

EASA AD US-2022-18-06

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment; Engine - Interstage High Pressure Turbine Rotor Seals - Removal / Replacement

The Federal Aviation Administration's Airworthiness Directive 2022-18-06 addresses safety concerns for General Electric Company GE90-110B1, GE90-115B, GE90-76B, GE90-85B, GE90-90B, and GE90-94B model turbofan engines. It focuses on reducing life limits and requiring removal and replacement of certain interstage high-pressure turbine rotor seals due to detected manufacturing anomalies. This directive aims to prevent premature failure of critical engine parts and potential uncontained debris release.

Airworthiness Directive

General Electric GE90