EASA Regulations & Airworthiness Directives

Browse 5,161 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 787116Show all...

EASA AD 2021-0013

Jan 13, 2021

Navigation — Global Navigation Satellite System — Replacement / Aircraft Flight Manual — Amendment

EASA Airworthiness Directive 2021-0013 addresses the replacement of Thales Topstar 200 LPV GPS/SBAS receivers on ATR 42-500 and ATR 72-212A aeroplanes. This directive applies to aircraft equipped with specific affected part numbers and mandates amendments to the Aircraft Flight Manual. The directive ensures continued airworthiness by mitigating risks associated with erroneous GPS position outputs during certain satellite constellation conditions.

Airworthiness Directive
  • ATR ATR42
  • ATR ATR72
  • ATR 42-500
  • ATR 72-212A

EASA AD 2021-0014

Jan 13, 2021

Wings — Outer Wing Lower Skin — Inspection

Wings — Outer Wing Lower Skin — Inspection is a regulatory document issued by FOKKER SERVICES concerning the inspection requirements for the outer wing lower skin on Fokker F28 aircraft. The document outlines necessary inspection procedures to ensure the structural integrity and airworthiness of the affected wing components. It specifically targets operators and maintenance organizations responsible for the upkeep of Fokker F28 aircraft.

Airworthiness DirectiveSuperseded
  • Fokker F28

EASA AD 2021-0011

Jan 12, 2021

Equipment / Furnishings — Outboard Load System — Inspection / Modification

EASA Airworthiness Directive 2021-0011 is an airworthiness directive addressing the inspection and modification of the outboard load system on Airbus Helicopters Deutschland GmbH EC135 and EC635 helicopter models. It specifically targets Goodrich hoists with certain part numbers and their hook assemblies to prevent potential detachment of external loads or persons during hoist operations.

Airworthiness Directive
  • Airbus Helicopters EC135
  • Airbus Helicopters 635
  • Airbus Helicopters EC635

EASA AD CF-2020-06R1

Jan 12, 2021

Standard Practices/Structures — Introduction of Barrel Nut Inspections

The Standard Practices/Structures — Introduction of Barrel Nut Inspections is a Canadian Airworthiness Directive CF-2020-06R1 issued by Transport Canada affecting all serial numbers of De Havilland Aircraft of Canada Limited DHC-8-100, DHC-8-200, DHC-8-300, and DHC-8-400 series aeroplanes. This directive mandates inspections of barrel nuts installed at multiple structural locations on these aircraft to detect and address cracking caused by corrosion. The inspections aim to maintain structural integrity and prevent potential loss of control of the aeroplane.

Airworthiness Directive
  • De Havilland Canada DHC-8
  • De Havilland Aircraft of Canada Limited DHC-8-100
  • De Havilland Aircraft of Canada Limited DHC-8-200
  • De Havilland Aircraft of Canada Limited DHC-8-300
  • De Havilland Aircraft of Canada Limited DHC-8-400

EASA AD CF-2021-01

Jan 11, 2021

Fire Protection — Powerplant Fire Extinguishing (FIREX) Interconnection Hose Not Properly Installed

Canadian Airworthiness Directive CF-2021-01 addresses a fire protection issue related to the powerplant fire extinguishing (FIREX) interconnection hose installation on Airbus Canada Limited Partnership aircraft models BD-500-1A10 and BD-500-1A11. The directive applies to specific serial numbers of these models and mandates corrective action to ensure the FIREX hose is properly secured. This measure aims to prevent ineffective fire extinguishing in the event of a powerplant fire.

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

EASA AD 2021-0010

Jan 11, 2021

Fuel — Inward Vent Valve — Modification

EASA Airworthiness Directive 2021-0010 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus Aircraft Ltd PC-12/47E aeroplanes, specifically those with manufacturer serial numbers 1720 and 2001 or higher. The directive addresses an issue with inward vent valves that lack a chromate conversion coating, which could lead to corrosion and potential fire hazards. It mandates modification of affected inward vent valves to ensure continued airworthiness and safety.

Airworthiness DirectiveSuperseded
  • Pilatus Aircraft PC-12
  • Pilatus PC-12/47E

EASA AD 2021-0006

Jan 7, 2021

Engine Fuel and Control — Fuel Pump — Replacement [Life Limitation]

EASA Airworthiness Directive 2021-0006 is an airworthiness directive addressing fuel pump replacement life limitations for Rolls-Royce Trent 1000 series engines installed on Boeing 787 aircraft. It mandates the removal and replacement of specific fuel pumps with part numbers G5030FPU01 and TPS1000-05 before exceeding newly established reduced life limits to prevent fuel pump performance degradation. This directive applies to all serial numbers of affected Trent 1000 engine models.

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

EASA AD US-2021-01-03

Jan 7, 2021

Engine - High-Pressure Turbine 1st Stage and 2nd Stage Disks - Removal

The Federal Aviation Administration's Airworthiness Directive 2021-01-03 addresses certain International Aero Engines AG V2500 series turbofan engines installed on aircraft such as the Airbus A321-231. This directive mandates the removal from service of specific high-pressure turbine (HPT) 1st-stage and 2nd-stage disks due to an identified unsafe condition following an uncontained disk failure event. The AD aims to prevent potential engine failures that could lead to damage to the engine, aircraft, or loss of the airplane.

Airworthiness Directive
  • International Aero Engines Ag V2500-( )5
  • International Aero Engines Ag V2500-A1
  • Airbus A321-231

EASA AD 2021-0007

Jan 7, 2021

Nacelles / Pylons — Inboard Pylon Box Dog Head Fitting Holes — Inspection

EASA Airworthiness Directive 2021-0007 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes equipped with Rolls-Royce Trent 900 or Engine Alliance GP7200 engines. The directive mandates inspections of the inboard pylon box Dog Head fitting fastener holes to detect cracks that could compromise structural integrity. It applies to all manufacturer serial numbers of these aircraft models.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2021-0003

Jan 6, 2021

Placards and Markings – Emergency Exit Labels – Installation

EASA Airworthiness Directive 2021-0003 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, C1, L, L1, L2 and EC 225 LP models equipped with specific cabin plug doors (Part Numbers 332A221301.XX or 332AS251406.XX). The directive addresses the installation of additional emergency exit placards on cabin plug doors to improve passenger understanding of emergency door jettisoning procedures.

Airworthiness DirectiveSuperseded
  • 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
  • Airbus Helicopters AS 332 L2
  • Airbus Helicopters EC 225 LP

EASA SIB AIR-21-01

Jan 6, 2021

Textron Aviation (McCauley Propeller Systems) - Alternative Method of Compliance to FAA AD 2020-19-06

Textron Aviation (McCauley Propeller Systems) - Alternative Method of Compliance to FAA AD 2020-19-06 is an FAA-approved alternative method of compliance for Airworthiness Directive 2020-19-06. It specifically addresses the eligibility criteria for installation of McCauley governors with serial numbers after 180501, including new governors and those maintained according to specific McCauley Alert Service Bulletins. This document applies to McCauley propeller governors used on affected aircraft.

AMC/GM

EASA AD US-2020-25-10

Jan 5, 2021

Engine - High Pressure Turbine Rotor Stage 2 Disks - Inspection / Replacement

The Federal Aviation Administration's Airworthiness Directive 2020-25-10 is a final rule addressing certain General Electric Company GEnx-1B and GEnx-2B model turbofan engines equipped with specific high-pressure turbine (HPT) rotor stage 2 disks. This directive mandates inspection and potential replacement of these disks due to the risk of undetected subsurface anomalies that could lead to uncontained disk failure. The directive applies to multiple GEnx engine variants including GEnx-1B64/P2, GEnx-1B67/P2, GEnx-1B70/75/P2, and others.

Airworthiness Directive
  • General Electric GEnx

EASA AD 2021-0001

Jan 4, 2021

Powerplant – Front Engine Mount / Strut Mount and Thrust Link – Inspection

EASA Airworthiness Directive 2021-0001 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841 and A380-842 aeroplanes equipped with Rolls-Royce RB211 Trent 900 engines. The directive mandates inspections of the front engine mount, strut mount, and thrust link due to concerns about salvage welds on the compressor intermediate case lugs in certain engines. It aims to ensure continued airworthiness by requiring repetitive inspections and corrective actions to prevent potential engine detachment in flight.

Airworthiness DirectiveSuperseded
  • Airbus A380

EASA SIB SAFO20016

Jan 4, 2021

Saircorp / Flight Boss Ltd. (Saircorp) Consoles

SAFO 20016 is a Safety Alert for Operators issued by the U.S. Federal Aviation Administration concerning the use of Saircorp consoles in Textron Aviation Inc. Model 172-, 177-, 182-, 185-, 205-, 206-, 210-, 310-, 320-, 337-, and 340-series airplanes, as well as other aircraft. The alert highlights safety risks posed by these unsecured metal consoles, which can shift during flight and interfere with aircraft controls or emergency equipment access.

Safety Information Bulletin

EASA AD US-2020-26-09

Jan 4, 2021

Wings - Center Wing Box Fastener Holes - Inspection

FAA Airworthiness Directive 2020-26-09 is a final rule addressing all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates inspections of the center wing box fastener holes for cracks using high frequency eddy current, ultrasonic, or detailed internal inspection methods. The directive aims to maintain structural integrity by detecting and repairing cracks in critical wing components.

Airworthiness Directive
  • Boeing 737100200200C300400500

EASA AD US-2020-25-01

Jan 4, 2021

Wings - Lower Forward Wing Fittings - Inspection

Federal Register Volume 85, Number 235 (December 7, 2020) is a final rule airworthiness directive issued by the FAA addressing certain Textron Aviation Inc. airplanes (formerly Beechcraft Corporation) including Models F90, 65-90, B90, C90, H90 (T-44A), E90, 99 series, A99 series, B99, C99, 100 series, A100, and B100. The directive targets fatigue cracks in the lower forward wing fittings caused by the installation of a specific washer part number. It mandates inspection and corrective actions to ensure continued airworthiness and safety.

Airworthiness Directive
  • Textron Aviation 100 (King Air)
  • Textron Aviation 65 (Queen Air)
  • Textron Aviation 90 (King Air)
  • Textron Aviation 99 (Airliner)
  • Textron Aviation F90
  • Textron Aviation 65-90
  • Textron Aviation B90
  • Textron Aviation C90
  • Textron Aviation H90
  • Textron Aviation E90
  • Textron Aviation 99 series
  • Textron Aviation A99 series
  • Textron Aviation B99
  • Textron Aviation C99
  • Textron Aviation 100 series
  • Textron Aviation A100
  • Textron Aviation B100

EASA AD CF-2020-54R1

Dec 28, 2020

Landing Gear – Main Landing Gear (MLG) Shock Strut Lower Pin Cracking

Canadian Airworthiness Directive CF-2020-54R1 addresses cracking issues in the main landing gear (MLG) shock strut lower pin, part number 19146-3, on Bombardier Inc. model CL-600-2B16 aircraft with specified serial numbers. The directive mandates repetitive lubrication, detailed visual inspections, and non-destructive testing of the affected pins to detect and prevent structural failure. It applies to various CL-600-2B16 variants including CL-604, CL-605, and CL-650 models.

Airworthiness DirectiveSuperseded
  • Bombardier CL-600 (Challenger)
  • Bombardier CL-600-2B16
  • Bombardier CL-604
  • Bombardier CL-605
  • Bombardier CL-650

EASA AD 2020-0283

Dec 24, 2020

Fuel – Fuel Pump – Inspection

EASA Airworthiness Directive 2020-0283 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 and A340 aeroplanes. It addresses fuel pumps with specific part numbers installed at designated locations on these aircraft models. The directive mandates inspections and potential replacements of fuel pumps showing erosion to prevent fuel tank ignition risks.

Airworthiness DirectiveSuperseded
  • Airbus A330
  • Airbus A340

EASA AD 2020-0022R2

Dec 23, 2020

Time Limits / Maintenance Checks — Main Gear Box / Particle Detectors — Inspection; Main Rotor Drive — Planet Gear Assemblies — Replacement / Modification

EASA Airworthiness Directive 2020-0022R2 is an updated regulatory requirement affecting Airbus Helicopters AS 332 L, L1, C, and C1 models. It addresses inspection, replacement, and modification requirements related to the main gearbox (MGB) planet gear assemblies and particle detectors to mitigate risks associated with gear spalling and cracking. The directive mandates specific inspections and installation of a Full Flow Magnetic Plug (FFMP) device to enhance safety and continued airworthiness.

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

EASA AD US-2020-26-04

Dec 22, 2020

Fuselage - Skin Panels - Inspection / Repair / Installation

Airworthiness Directive 2020-26-04 is a final rule issued by the FAA addressing certain Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates inspections and repairs of fuselage skin panels, specifically targeting cracking along chem-milled lines. This directive updates and expands previous inspection requirements to ensure continued airworthiness.

Airworthiness Directive
  • Boeing 737100200200C300400500