EASA Regulations & Airworthiness Directives

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

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350222Airbus A330220Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941132Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787115Show all...

EASA AD CF-2023-37R1

May 23, 2024

Standard Practices / Structures — Verification of Aircraft Repairs and Damage Assessments

Airworthiness Directive CF-2023-37R1 is a Canadian regulatory update addressing Airbus Canada Limited Partnership (ACLP) model BD-500-1A10 and BD-500-1A11 aircraft. It focuses on verifying aircraft repairs and damage assessments in light of revised structural stress data and operational loads for the A220 aircraft. The directive ensures compliance with updated repair manuals and engineering orders to maintain structural integrity.

Airworthiness Directive
  • Airbus BD-500 (A220 Series)
  • Airbus Canada BD-500-1A10
  • Airbus Canada BD-500-1A11

EASA AD US-2024-10-04

May 23, 2024

Wings - Rear Wing Spar Attachment Fitting - Inspection

The Federal Aviation Administration's Airworthiness Directive 2024-10-04 addresses certain Piper Aircraft, Inc. models PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes. This directive mandates inspection of the rear wing spar attachment fitting due to a manufacturing defect involving a double-drilled bolt hole, which compromises structural integrity. The AD aims to prevent potential wing separation and loss of control by requiring inspections and corrective actions as necessary.

Airworthiness Directive
  • Piper Aircraft PA-28 (Archer)
  • Piper Aircraft PA-28R (Arrow)
  • Piper Aircraft PA-34 (Seneca)
  • Piper Aircraft PA-44 (Seminole)
  • Piper PA-28-181
  • Piper PA-28R-201
  • Piper PA-34-220T
  • Piper PA-44-180

EASA AD 2024-0103-CN

May 22, 2024

CANCELLED: Wings — Flaps Beams No 2 — Inspections

EASA Airworthiness Directive Cancellation Notice 2024-0103-CN cancels the previous DGAC France AD 2000-040-034(B) R1, which required inspections of flap beam No 2 on Airbus A300-600ST aeroplanes. The cancellation applies to all A300F4-608ST aircraft except those modified in production with Airbus mods 11133 or 19050. The original inspections addressed potential cracks in flap beam No 2 that could compromise structural integrity.

Airworthiness Directive
  • Airbus A300-600ST (Beluga)
  • Airbus A300-600ST

EASA AD 2024-0102

May 17, 2024

Engine – Low Pressure Compressor Blades – Inspection / Replacement

EASA Airworthiness Directive 2024-0102 is issued for Rolls-Royce Deutschland Ltd & Co KG RB211 Trent 700 engines, specifically models RB211 Trent 768-60, 772-60, 772B-60, and 772C-60, commonly installed on Airbus A330 aircraft. The directive mandates ultrasonic inspections and potential replacement of low pressure compressor blades with specific part numbers to address risks of partial blade release. This AD ensures continued airworthiness by requiring repetitive inspections and corrective actions to prevent engine damage and safety hazards.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700
  • Airbus A330

EASA AD BR-2023-05-03R2

May 17, 2024

Equipment / Furnishings - Monuments Structural Reinforcements / Replacement of Fasteners

Brazilian Airworthiness Directive AD No. 2023-05-03R02 is issued by the Agência Nacional de Aviação Civil (ANAC) and applies to Embraer S.A. EMB-505 aircraft as specified in Embraer Service Bulletin SB505-25-0046, revision 03. This directive mandates structural reinforcement installation on monuments and replacement of floor support fasteners to address safety concerns. The AD ensures compliance with Brazilian aviation regulations for all aircraft registered in Brazil.

Airworthiness Directive
  • Embraer EMB-505 (Phenom 300)
  • Embraer EMB-505

EASA AD 2020-0195R1

May 15, 2024

Engine — Low Pressure Turbine Discs — Inspection

EASA Airworthiness Directive 2020-0195R1 is an updated regulatory requirement addressing inspection and repair of low pressure turbine discs in Rolls-Royce Trent 1000 engines installed on Boeing 787 aircraft. The directive mandates repetitive inspections of specific turbine disc parts for cracks and introduces approved repair instructions as an alternative to part replacement. This directive ensures continued airworthiness and safety of affected engines by preventing potential turbine disc failures.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
  • Boeing 787

EASA SIB CASA-2024-04

May 15, 2024

Loose Bolts and Missing Sealant at the Fuel Boost Pump Canister to Wing Rib 6 Interface

Transport Canada Civil Aviation Safety Alert CASA 2024-04 is a safety alert addressing the discovery of loose bolts and missing sealant at the Fuel Boost Pump Canister to Wing Rib 6 interface on Airbus Canada Limited Partnership aeroplanes models BD-500-1A10 and BD-500-1A11. The alert highlights potential risks related to fuel leaks and corrosion due to these issues. It applies to all serial numbers of the affected aircraft models.

Safety Information Bulletin
  • Airbus BD-500 (A220 Series)

EASA AD US-2024-06-15

May 14, 2024

[Correction] Engine - Interstage High-Pressure Turbine Rotor Seal - Inspections

Correction to Airworthiness Directive 2024-06-15 issued by the Federal Aviation Administration (FAA) concerning General Electric Company Model GE90-110B1 and GE90-115B engines. The correction addresses typographical errors in the references to service information related to inspections of the interstage high-pressure turbine (HPT) rotor seal. The directive mandates ultrasonic inspections and eventual replacement of the affected rotor seals to prevent engine failure.

Airworthiness Directive
  • General Electric GE90

EASA AD 2024-0088

May 14, 2024

[Correction] Placards and Markings — Rear Facing Seat(s) — Placard Installation

EASA Airworthiness Directive 2024-0088 is a safety directive addressing placard installation for rear facing seats on Leonardo AB139 and AW139 helicopters modified under EASA Supplemental Type Certificates 10030095 and 10017198. The directive mandates new placards instructing occupants to lock the seat headrest in the highest position during take-off and landing. This applies specifically to certain serial-numbered helicopters modified by Mecaer Aviation Group VIP Interiors.

Airworthiness Directive
  • Leonardo S.P.A. Helicopters AB139
  • Leonardo S.P.A. Helicopters AW139
  • Leonardo AB139
  • Leonardo AW139

EASA AD GA8-3-Amdt4

May 14, 2024

Forward Cargo Door Slide - Inspection

The Commonwealth of Australia Civil Aviation Safety Authority Airworthiness Directive AD/GA8/3 Amdt 4 addresses the forward cargo door slide on Gippsland Aeronautics GA8 Series Aeroplanes. It mandates compliance with the manufacturer's mandatory service bulletin SB-GA8-2005-23 Issue 8 dated 11 October 2023 to ensure the safety and integrity of the cargo door mechanism. This directive aims to prevent potential in-flight door detachment caused by excessive wear.

Airworthiness Directive
  • Ga8 Airvan Pty Ltd (Gippsaero) GA8
  • Gippsland Aeronautics GA8

EASA SIB CASA-2024-03

May 13, 2024

Inboard Flap Spigot Tube and Mid and Outboard Flap Corrosion

Transport Canada Civil Aviation Safety Alert CASA 2024-03 addresses corrosion issues affecting the inboard flap spigot tubes and the internal structure of the mid and outboard flaps on Bombardier Inc. aeroplanes models BD-700-1A10 and BD-700-1A11. The alert highlights the need for inspections and corrective actions to mitigate corrosion risks in these specific aircraft components. It recommends incorporating related Maintenance Review Board Report and Aircraft Maintenance Manual tasks into the approved maintenance schedule.

Safety Information Bulletin
  • Bombardier BD-700

EASA SIB SAIB-2024-02

May 13, 2024

Wing Spar - Inspection

Special Airworthiness Information Bulletin SAIB: 2024-02 is an FAA informational bulletin addressing potential cracks and hole-quality issues in the wing rear attach beam assembly of Revo Incorporated Model Colonial C-1, Colonial C-2, Lake LA-4 series, Lake Model 250, and Lake 270 Turbo Renegade aircraft. The bulletin highlights inspection areas and provides guidance to owners, operators, and maintenance personnel to identify and address these concerns. This bulletin is not a mandatory directive but serves as a safety alert.

Safety Information Bulletin
  • Revo, C-1
  • Revo, C-2

EASA AD 2024-0100

May 10, 2024

Superseded by EASA AD 2024-0233

EASA Airworthiness Directive 2024-0100 is issued for Airbus Helicopters AS 332 C, C1, L, and L1 models equipped with dual hoist installation and de-icing systems. It addresses a vibration issue around 12 Hz frequency observed after retrofit of the de-icing system, which could lead to structural failure or loss of control. The directive mandates removal or operational limitations related to the dual hoist and de-icing systems to mitigate this unsafe condition.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 C
  • Airbus Helicopters AS 332 C1
  • Airbus Helicopters AS 332 L
  • Airbus Helicopters AS 332 L1

EASA AD BR-2023-08-03R2

May 8, 2024

Windows - Cockpit Side Windows - Inspection / Replacement

Brazilian Airworthiness Directive AD No. 2023-08-03R02 is an official regulatory document issued by the Agência Nacional de Aviação Civil (ANAC) that applies to Embraer S.A. airplanes model EMB-545 and EMB-550 equipped with cockpit side windows having Part Numbers NP-200402-7 or NP-200402-8. The directive mandates inspection and replacement procedures for these cockpit side windows to address safety concerns. It provides detailed inspection methods and replacement requirements to prevent potential in-flight depressurization due to window failure.

Airworthiness Directive
  • Embraer EMB-545
  • Embraer EMB-550

EASA AD 2024-0099

May 6, 2024

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

EASA Airworthiness Directive 2024-0099 is an airworthiness directive issued for Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses issues with fuselage and belly fairing mounted emergency evacuation escape slides, specifically those with certain part numbers and serial numbers that have shown seam failures during proof pressure testing after overhaul. The directive mandates replacement and inspection requirements to ensure the continued airworthiness of these emergency slides.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD US-2024-06-01

May 6, 2024

Fuselage - Skin and Bear Strap at the Forward Galley Door Cutout - Inspection

Federal Aviation Administration Airworthiness Directive 2024-06-01 is a final rule addressing certain Boeing 737-600, -700, -700C, -800, -900, and -900ER airplanes. It mandates inspections of the fuselage skin and bear strap at the forward galley door cutout forward upper corner due to reported cracks caused by high operating stresses. The directive aims to ensure structural integrity and prevent potential rapid decompression.

Airworthiness Directive
  • Boeing 737600700700C800900900ER

EASA AD US-2024-06-14

May 2, 2024

Engine - High-pressure Compressor 2nd and 4th Stage Rotors - Replacement

The Federal Register document titled "Engine - High-pressure Compressor 2nd and 4th Stage Rotors - Replacement" is a final rule airworthiness directive (AD 2024-06-14) issued by the FAA affecting International Aero Engines, LLC Model PW1124G1-JM, PW1127G-JM, PW1127GA-JM, PW1129G-JM, PW1130G-JM, PW1133G-JM, and PW1133GA-JM engines. It addresses potential degradation and fracture risks in the high-pressure compressor 2nd and 4th stage rotors due to improper cleaning procedures. The AD mandates replacement of certain affected rotors to ensure continued airworthiness and safety.

Airworthiness Directive
  • International Aero Engines PW1100
  • International Aero Engines PW1400

EASA AD 2024-0098

May 2, 2024

Fuselage – Forward Cargo Door Piano Hinges – Inspection

EASA Airworthiness Directive 2024-0098 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection of the forward cargo door piano hinges 2 and 3 due to potential cracking risks. This directive applies to specific manufacturer serial numbers and aims to ensure continued structural integrity of the affected aircraft.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041

EASA AD US-2024-07-05

May 2, 2024

Fuselage - Station 1640 Frame Web Between S-14 and S-15 - Inspection / Maintenance Records Check

The Federal Aviation Administration's Airworthiness Directive 2024-07-05 is a final rule addressing certain Boeing 757-200, 757-200CB, and 757-300 airplanes. It mandates inspections or maintenance records checks for liner holes in the fuselage at station 1640 frame web between stringers S-14 and S-15 due to detected cracks. The directive aims to ensure structural integrity by requiring corrective actions when necessary.

Airworthiness Directive
  • Boeing 757200200CB300