EASA Regulations & Airworthiness Directives

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

EASA AD G-2022-0021

Jan 4, 2023

Time Limits / Maintenance Checks — Corrosion Prevention and Control Programme — Amendment / Implementation

Civil Aviation Authority Airworthiness Directive G-2022-0021 addresses corrosion prevention and control for BAE Systems Jetstream 3100 and 3200 aeroplanes. It mandates compliance with the updated Corrosion Prevention and Control Programme (CPCP) document Revision 9 to ensure continued airworthiness. This directive applies to all models and serial numbers of the Jetstream 3100 and 3200 series.

Airworthiness Directive
  • Bae Systems (Operations) Jetstream 3100
  • Bae Systems (Operations) Jetstream 3200
  • BAE Systems Jetstream 3100
  • BAE Systems Jetstream 3200

EASA AD US-2022-27-04

Jan 3, 2023

Engine Controls - Electronic Engine Control Full Authority Digital Engine Control Software - Replacement

The document titled "Engine Controls - Electronic Engine Control Full Authority Digital Engine Control Software - Replacement" is a final rule airworthiness directive issued by the FAA affecting Pratt & Whitney PW1519G, PW1521G, PW1521G-3, PW1521GA, PW1524G, PW1524G-3, PW1525G, and PW1525G-3 turbofan engines. It addresses an unsafe condition caused by uncommanded dual engine shutdowns upon landing due to certain versions of the electronic engine control (EEC) full authority digital engine control (FADEC) software. The directive mandates updating the EEC FADEC software to a safer version to prevent compromised braking capability and potential runway excursions.

Airworthiness Directive
  • Pratt & Whitney PW1500G

EASA AD US-2022-25-20

Jan 3, 2023

Engine - High-Pressure Turbine Stage 2 Disks, Forward Seals and Stages 6-10 Compressor Rotor Spools - Replacement

The Federal Aviation Administration's Airworthiness Directive 2022-25-20 addresses certain General Electric Company GEnx-1B and GEnx-2B model turbofan engines. It targets high-pressure turbine stage 2 disks, forward seals, and stages 6-10 compressor rotor spools suspected to contain iron inclusions due to manufacturing defects. This directive aims to prevent potential engine failures and ensure continued airworthiness of affected engines.

Airworthiness Directive
  • General Electric GEnx

EASA AD US-2022-23-10

Jan 3, 2023

Water / Waste - Potable Water System - Deactivation / Modification

Airworthiness Directive 2022-23-10 is a final rule issued by the Federal Aviation Administration affecting all Boeing 777F series airplanes. It addresses unsafe conditions related to the potable water system, specifically water supply line detachment above an electronic equipment cooling filter that can cause water intrusion into the forward electronic equipment bay. This directive requires deactivating the potable water system, installing protective shrouds on water supply and return lines, and performing leak tests to prevent water damage to critical electrical systems.

Airworthiness Directive
  • Boeing 777
  • Boeing 777F

EASA AD 2022-0267-E

Dec 27, 2022

Wing Main Spar – Prohibition of Flights; Aircraft Flight Manual / Operational Limitation – Amendment

EASA Airworthiness Directive 2022-0267-E is an emergency directive addressing structural concerns on CEAPR DR 400 series aeroplanes, specifically those with certain main wing spars installed. The directive applies to multiple DR 400 models with serial numbers 2444 to 2777 and those equipped with wings delivered or overhauled after 1 February 2000 by Robin Aircraft. It mandates flight prohibitions or operational limitations depending on the presence of affected wing spars.

Airworthiness DirectiveSuperseded
  • Ceapr DR 400

EASA AD G-2022-0020

Dec 26, 2022

Time Limits / Maintenance Checks — Airworthiness Limitations — Amendment / Implementation

Civil Aviation Authority Airworthiness Directive G-2022-0020, issued on 2022-12-22, addresses mandatory airworthiness limitations and maintenance checks for all BAE Systems (Operations) Ltd ATP aeroplanes. It updates the Aircraft Maintenance Manual to Revision 96, introducing specific life limits for main landing gear shock absorber bolts and engine power control cables. This directive ensures continued airworthiness by enforcing compliance with revised maintenance tasks and life limitations.

Airworthiness Directive
  • Bae Systems (Operations) ATP
  • BAE Systems ATP

EASA AD 2022-0266

Dec 22, 2022

Electric and Electronic Common Installation — Cockpit Panel Bracket — Inspection

EASA Airworthiness Directive 2022-0266 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates detailed inspections of the 10VU rack side fittings on cockpit panel brackets to detect cracks that could affect primary flight and navigation displays. The directive applies to all manufacturer serial numbers except those with Airbus modification 157335 embodied in production.

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

EASA AD 2021-0166R1

Dec 22, 2022

Equipment / Furnishings — Passenger Seats — Inspection

EASA Airworthiness Directive 2021-0166R1 is a regulatory document addressing inspection requirements for Safran Seats France passenger seats Z85 Dragonfly installed on certain Airbus A320-214, A320-251N, and A320-271N aeroplanes. The directive mandates a detailed inspection of affected seat parts to detect damage caused by improper transportation or installation, which could lead to seat track detachment and potential personal injury.

Airworthiness Directive
  • Airbus A320

EASA AD CF-2022-70

Dec 22, 2022

Fuel Distribution – Motive Flow Fuel-feed Tubes Damaged at Bonding Clamp and Clamp Block Locations Inside the Fuel Tank

Canadian Airworthiness Directive CF-2022-70 addresses fuel distribution issues on Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft models. It mandates inspections and operational checks of motive flow fuel-feed tubes inside the fuel tank to prevent fuel imbalance caused by mechanical wear at bonding clamp and clamp block locations. This directive applies to specific serial numbers starting from 50001 for BD-500-1A10 and 55001 for BD-500-1A11 models.

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

EASA AD 2021-0101R2

Dec 21, 2022

Doors — Placards — Installation / Rotorcraft Flight Manual — Section Emergency Procedures — Amendment

EASA Airworthiness Directive 2021-0101R2 is an amendment addressing safety concerns on Airbus Helicopters SA 365, AS 365, and EC 155 models. It mandates installation of external jettisoning systems and placards on cockpit and cabin doors, along with amendments to the Rotorcraft Flight Manual emergency procedures section, to improve evacuation capability after ditching with inflated emergency flotation systems.

Airworthiness Directive
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Airbus Helicopters SA 365

EASA AD 2022-0264

Dec 21, 2022

Engine Fuel & Control — Fuel Pump — Replacement (Life Limitation)

EASA Airworthiness Directive 2022-0264 is an airworthiness directive addressing Rolls-Royce Deutschland Ltd & Co KG RB211 Trent 900 series engines, specifically the RB211 Trent 970-84, 970B-84, 972-84, 972B-84, 972E-84, 977-84, 977B-84, and 980-84 models. It focuses on the replacement of fuel pumps with part numbers 1703697C, 1703697E, or 1703697G due to life limitations. The directive mandates life limits for these fuel pumps to prevent engine thrust shortfall or insufficient fuel flow during in-flight windmill relight scenarios.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900

EASA AD 2022-0257

Dec 21, 2022

Fuel — Valves and Pumps — Inspection / Replacement

EASA Airworthiness Directive 2022-0257 is an airworthiness directive issued by EASA affecting Airbus A340-313 aeroplanes with specific manufacturer serial numbers. It mandates additional inspections and replacement of certain fuel valves and pumps to ensure continued safe operation beyond the Design Service Goal. The directive references Airbus Service Bulletin A340-28-4145 for detailed maintenance instructions.

Airworthiness Directive
  • Airbus A340313

EASA AD 2022-0263

Dec 21, 2022

Landing Gear — Main Landing Gear Bogie Pivot Pin — Greasing

EASA Airworthiness Directive 2022-0263 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes. It addresses the main landing gear bogie pivot pin, specifically requiring updated greasing procedures to prevent damage to the High Velocity Oxygen Fuel coating on these parts. The directive aims to ensure continued airworthiness and prevent potential landing gear collapse.

Airworthiness Directive
  • Airbus A350941

EASA AD 2022-0262

Dec 21, 2022

Wings – Front and Rear Spars – Inspection

EASA Airworthiness Directive 2022-0262 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aircraft. It mandates inspections of specific wing spars, including the outer rear spar, outer inner front spar, and outer front spar, to detect cracks that could compromise wing structural integrity. This directive updates previous inspection requirements and applies to all manufacturer serial numbers of the Airbus A380.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2022-0261

Dec 20, 2022

Fire Protection — Fire Detectors — Replacement

EASA Airworthiness Directive 2022-0261 is an airworthiness directive addressing fire detector replacements on Airbus Helicopters AS 365 N3, EC 155 B, and EC 155 B1 models. It targets specific fire detectors with identified manufacturing non-compliance that may cause spurious engine fire warnings. The directive mandates replacement of affected fire detectors to ensure continued safe operation of these helicopters.

Airworthiness Directive
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Safran ARRIEL 2
  • Airbus Helicopters AS 365 N3
  • Airbus Helicopters EC 155 B
  • Airbus Helicopters EC 155 B1

EASA SIB 2022-12

Dec 20, 2022

Loss of Air Traffic Control Tracking on Boeing 787 Aeroplanes in European Airspace

EASA Safety Information Bulletin 2022-12 is a safety information bulletin addressing the loss of air traffic control tracking on Boeing 787 aeroplanes operating in European airspace. The bulletin highlights intermittent transponder malfunctions causing degraded radar tracking and potential loss of track display for air traffic controllers. This issue affects Boeing 787 aircraft and may impact surveillance quality and Short-Term Conflict Alert functionality.

Safety Information Bulletin
  • Boeing 787

EASA AD 2022-0258

Dec 20, 2022

Main Rotor Drive — Main Transmission Support Case — Inspection / Replacement

EASA Airworthiness Directive 2022-0258 is an airworthiness directive addressing the main rotor drive main transmission support case for Leonardo S.p.A. AB212, AB412, and AB412EP helicopters. It mandates inspections and possible replacement of the main transmission support case to detect and correct cracks caused by corrosion, which could compromise helicopter control.

Airworthiness Directive
  • Leonardo S.P.A. Helicopters AB212
  • Leonardo S.P.A. Helicopters AB412
  • Leonardo AB212
  • Leonardo AB412
  • Leonardo AB412EP

EASA AD 2022-0259

Dec 20, 2022

Superseded by EASA AD 2024-0062

EASA Airworthiness Directive 2024-0062 is an airworthiness directive concerning Rolls-Royce Deutschland Ltd & Co KG Trent 1000 engines. This directive supersedes previous related directives and addresses safety and maintenance requirements for these engine models. It is relevant for operators and maintenance organizations managing aircraft equipped with Trent 1000 engines.

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

EASA AD 2022-0260

Dec 20, 2022

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 — Airworthiness Limitations Items and Safe Life Items — Implementation

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 — Airworthiness Limitations Items and Safe Life Items — Implementation is a regulatory document issued by FOKKER SERVICES for the F28 aircraft type. It addresses the implementation of airworthiness limitations related to time limits, maintenance checks, and safe life items to ensure continued airworthiness. The document provides updated instructions for operators and maintenance organizations regarding mandatory maintenance tasks and life limits of components.

Other
  • Fokker F28

EASA AD ISR-I-24-2018-09-7R2

Dec 19, 2022

Electrical Power - Upper and Lower Front Relay Box Replacement

The Electrical Power - Upper and Lower Front Relay Box Replacement Airworthiness Directive issued by the State of Israel Ministry of Transport Civil Aviation Authority applies to GALP model G150 aircraft with serial numbers 201 through 326. This directive mandates the replacement of specific upper and lower front relay boxes to address potential corrosion issues in the relay box connector solder joints. The replacement involves upgraded parts with acrylic conformal coating to enhance reliability and safety.

Airworthiness Directive
  • Gulfstream (Galp) G150
  • GALP G150