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 2022-0111R1

Jul 26, 2023

Wings — Overwing Panel / Lug Attachment — Inspection

The document titled Wings — Overwing Panel / Lug Attachment — Inspection is an Airworthiness Directive issued for AIRBUS S.A.S. aircraft models A319, A320, and A321. It addresses inspection requirements for the overwing panel and lug attachment areas on these aircraft types to ensure structural integrity and safety. The directive provides guidance on inspection procedures specific to these Airbus models.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD CF-2023-53

Jul 25, 2023

Electrical Power — Transformer Rectifier Unit (TRU) Fan Inoperative

Canadian Airworthiness Directive CF-2023-53 addresses an electrical power issue related to the Transformer Rectifier Unit (TRU) fan on Bombardier Inc. model BD-700-2A12 aircraft, serial numbers 70006 through 70166. The directive mandates corrective action to prevent overheating and potential cascading failures of TRUs. This AD ensures improved safety by requiring replacement of a specific TRU unit with an updated version that includes a corrected fan and monitoring circuit.

Airworthiness Directive
  • Bombardier BD-7002A12

EASA AD 2023-0152

Jul 25, 2023

Engine — Low Pressure Compressor Booster Rotor — Inspection

EASA Airworthiness Directive 2023-0152 is an airworthiness directive addressing inspection requirements for the low pressure compressor booster rotors on Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 engines, commonly installed on Boeing 717 aircraft. The directive mandates fluorescent-penetrant inspections of specific affected parts to detect malformed scallop edge geometry and surface conditions that could lead to engine failure. It provides updated inspection intervals and corrective actions to ensure continued airworthiness.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg BR700-715
  • Boeing 717

EASA AD CF-2023-56

Jul 25, 2023

Equipment/Furnishings – Overhead Storage Compartments – Improvement of the Overhead Bin Harnesses Over the Class Divider

Canadian Airworthiness Directive CF-2023-56 mandates inspections and improvements to the overhead bin electrical harnesses above the class divider on MHI RJ Aviation ULC (formerly Bombardier Inc.) CRJ900 series aircraft, specifically models CL-600-2C10, CL-600-2D15, and CL-600-2D24 with specified serial numbers. The directive addresses potential damage risks to electrical harnesses that could affect critical aircraft systems such as emergency lighting, passenger oxygen, and air conditioning. This directive is issued under Canadian Aviation Regulation 521.427.

Airworthiness DirectiveSuperseded
  • MHI RJ Aviation CL-600 (Regional Jet)
  • MHI RJ Aviation ULC CRJ900

EASA AD CF-2023-55

Jul 25, 2023

Fuel — Fouling Condition between Fuel Scupper Attachment Bolt and Wire Harness

Canadian Airworthiness Directive CF-2023-55 addresses a fuel system safety issue on Bombardier Inc. CL-600-2B16 aircraft, specifically serial numbers 5775 through 5990 and 6050 through 6178. The directive requires inspection and potential repair of electrical wires near the fuel scupper attachment bolts to prevent sparking during refueling. This AD aims to eliminate fire hazards caused by electrical sparks generated from wire insulation damage due to contact with fuel scupper bolts.

Airworthiness Directive
  • Bombardier CL-600 (Challenger)
  • Bombardier CL-600-2B16

EASA AD 2023-0151

Jul 25, 2023

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – Amendment

EASA Airworthiness Directive 2023-0151 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with updated damage tolerant airworthiness limitations as specified in Airbus A318/A319/A320/A321 Airworthiness Limitations Section Part 2 Damage Tolerant Airworthiness Limitations Items Revision 09 Variation 9.3. This directive ensures continued airworthiness by introducing new or more restrictive maintenance tasks and limitations.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2023-0150

Jul 20, 2023

Fuselage — Crossbeam Splicing at Frames 16 and 20 — Inspection

EASA Airworthiness Directive 2023-0150 is an airworthiness directive addressing inspection requirements for the fuselage crossbeam splicing at frames 16 and 20 on Airbus A318, A319, A320, and A321 aeroplanes. It applies to specific serial numbers except those with certain Airbus modifications embodied in production or service. The directive mandates repetitive special detailed inspections to detect early cracks that could compromise structural integrity.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2023-0149

Jul 19, 2023

Engine Exhaust – Ejector Duct – Inspection

EASA Airworthiness Directive 2023-0149 is an airworthiness directive issued for Leonardo S.p.A. AW189 helicopters. It addresses potential cracking damage in the ejector duct parts on both left-hand and right-hand sides of the engine exhaust system. The directive mandates inspections and possible replacement of affected ejector ducts to ensure continued safe operation.

Airworthiness DirectiveSuperseded
  • Leonardo S.P.A. Helicopters AW189
  • Leonardo AW189

EASA AD 2023-0148

Jul 19, 2023

Main Rotor Drive — Main Gearbox — Replacement; Placards and Markings — ENG1 Training Idle Switch — Installation / Operational Restriction

EASA Airworthiness Directive 2023-0148 is issued for Airbus Helicopters EC 225 LP models addressing main rotor drive main gearbox (MGB) replacement and installation of placards related to the ENG1 Training Idle switch. It applies to all EC 225 LP helicopters with specific affected MGB part numbers and introduces operational restrictions for one engine inoperative (OEI) training flights. The directive mandates inspections, part replacements, and placard installations to ensure continued airworthiness.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters EC 225 LP

EASA AD CF-2023-54

Jul 19, 2023

Time Limits / Maintenance Checks – Airworthiness Limitations – Implementation

Airworthiness Directive CF-2023-54 is issued by Transport Canada and applies to Airbus Canada Limited Partnership aeroplanes, specifically models BD-500-1A10 and BD-500-1A11. This directive mandates updates to the aircraft maintenance schedules to incorporate the latest Airworthiness Limitations as defined in Issue No. 017.00 of the AWL publication. The directive ensures continued airworthiness by enforcing compliance with updated maintenance tasks and intervals.

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

EASA AD 2023-0106R1

Jul 18, 2023

Fuel — Fuel Pump — Inspection / Replacement

EASA Airworthiness Directive 2023-0106R1 is an updated regulatory requirement addressing inspection and replacement of specific fuel pumps on Airbus A318, A319, A320, and A321 aircraft. It targets fuel pumps with part numbers 568-1-27202-001, 002, 005 (Pump A) and 568-1-27202-02R (Pump B) installed in various fuel tank locations. This directive aims to prevent potential in-tank ignition risks caused by pump failures and cavitation erosion.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD CF-2023-51

Jul 17, 2023

Fuel Storage — Fuel Drain Quick Disconnect Valve Leakage Following Impact

The Airworthiness Directive CF-2023-51 is issued by Transport Canada and applies to Bell Textron Canada Limited model 505 helicopters with specific serial numbers. It addresses a fuel leakage issue from the fuel drain quick disconnect valve following an impact during crash testing. The directive mandates corrective measures to prevent fuel leakage and potential post-impact fire hazards.

Airworthiness Directive
  • Bell 505 (Jet Ranger X)
  • Bell Textron Canada Limited 505

EASA AD 2023-0146

Jul 14, 2023

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive 2023-0146 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus Helicopters SA 330 J models. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the SA 330 J Maintenance Program – PUMA 330 J Airworthiness Limitations 5.99, Edition 2, Revision 7. This directive ensures continued airworthiness by enforcing mandatory maintenance and replacement schedules for critical components.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters SA 330 J

EASA AD 2023-0140

Jul 14, 2023

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2023-0140 is an amendment concerning the time limits and maintenance checks detailed in the Airworthiness Limitations Section for Airbus Helicopters AS 332 L2 models. It mandates compliance with the updated Airworthiness Limitations Section issued by Airbus Helicopters, which includes all service life limits and maintenance tasks necessary for continued airworthiness. This directive applies to all AS 332 L2 helicopters regardless of serial number.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters AS 332 L2

EASA AD 2023-0142

Jul 14, 2023

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2023-0142 is an amendment concerning the time limits and maintenance checks detailed in the Airworthiness Limitations Section for Airbus Helicopters AS 332 L1 models. It mandates compliance with the updated Airworthiness Limitations Section issued by Airbus Helicopters, ensuring continued airworthiness of these helicopters. This directive applies to all manufacturer serial numbers of the AS 332 L1 helicopter.

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

EASA AD 2023-0144

Jul 14, 2023

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2023-0144 is an amendment addressing the time limits and maintenance checks for Airbus Helicopters AS 332 C1 models. It mandates compliance with the Airworthiness Limitations Section (ALS) Revision 009 dated 27 July 2022 to ensure continued airworthiness. This directive applies specifically to all manufacturer serial numbers of the AS 332 C1 helicopter.

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

EASA AD 2023-0141

Jul 14, 2023

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2023-0141 is an amendment concerning the time limits and maintenance checks detailed in the Airworthiness Limitations Section for Airbus Helicopters EC 225 LP models. It mandates compliance with the latest Airworthiness Limitations Section revision to ensure continued airworthiness of these helicopters. This directive applies to all manufacturer serial numbers of the EC 225 LP helicopter.

Airworthiness Directive
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters EC 225 LP

EASA AD 2023-0145

Jul 14, 2023

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2023-0145 is an amendment addressing the time limits and maintenance checks in the Airworthiness Limitations Section for Airbus Helicopters AS 332 C models. It mandates compliance with the updated Airworthiness Limitations Section issued by Airbus Helicopters, which contains mandatory maintenance tasks and service life limits to ensure continued airworthiness of these helicopters.

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

EASA AD 2023-0143

Jul 14, 2023

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2023-0143 is an amendment concerning the Airbus Helicopters AS 332 L model. It mandates compliance with the updated Airworthiness Limitations Section (ALS) for time limits and maintenance checks to ensure continued airworthiness. This directive replaces previous maintenance instructions with a more current and segregated ALS document.

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

EASA AD CF-2023-52

Jul 13, 2023

Oxygen — Portable Oxygen Bottles — Oxygen Masks Not Connected to Oxygen Bottles After Servicing

The Canadian Airworthiness Directive CF-2023-52 addresses an issue with portable oxygen bottles and oxygen masks on certain Airbus Canada Limited Partnership aircraft models BD-500-1A10 and BD-500-1A11. It mandates inspection and correction of oxygen masks that are not connected to their respective portable oxygen bottles after maintenance. This directive ensures proper oxygen supply to cabin crew and passengers during decompression or emergency situations.

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