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 2022-0175

Aug 23, 2022

Airborne Auxiliary Power — Auxiliary Power Unit Tee Duct — Replacement

The document titled Airborne Auxiliary Power — Auxiliary Power Unit Tee Duct — Replacement addresses maintenance and replacement procedures for the Auxiliary Power Unit (APU) tee duct on AIRBUS S.A.S. A330 and A340 aircraft models. It provides guidance to ensure the continued airworthiness and safe operation of these aircraft by focusing on a critical component of the APU system.

Airworthiness Directive
  • Airbus A330
  • Airbus A340

EASA SIB SAFO22002

Aug 22, 2022

Electronic Flight Bags - Onboard Performance Tool v4.70 for iOS Devices

The Safety Alert for Operators SAFO 22002 addresses issues with Boeing's Onboard Performance Tool (OPT) version 4.70 for iOS devices, used on Boeing airplanes. The document highlights two calculation errors affecting takeoff and landing performance data, which could lead to incorrect runway length information being presented to flight crews. These issues specifically impact the accuracy of landing calculations and intersection takeoff calculations within the OPT software.

Safety Information Bulletin
  • Boeing 737
  • Boeing 747
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Boeing 787

EASA AD 2022-0172

Aug 22, 2022

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 1 / Safe Life Airworthiness Limitations Items – Amendment

EASA Airworthiness Directive 2022-0172 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A310 aeroplanes, including models A310-203, A310-204, A310-221, A310-222, A310-203C, A310-304, A310-308, A310-322, A310-324, and A310-325. This directive mandates updates to the Airworthiness Limitations Section Part 1 Safe Life Airworthiness Limitations Items to ensure continued airworthiness. It requires operators to comply with new or more restrictive maintenance tasks and life limits as specified in the Airbus A310 ALS Part 1 SL-ALI Revision 02 Variation 2.1.

Airworthiness DirectiveSuperseded
  • Airbus A310203204221222203C304308322324325

EASA AD CF-2022-48

Aug 19, 2022

Doors — Passenger Door Functional Test Missing Certain Steps Affecting Rigging

Airworthiness Directive CF-2022-48 is issued by Transport Canada and applies to Bombardier Inc. model BD-700-2A12 aeroplanes, serial numbers 70006 through 70061. This directive addresses missing steps in the passenger door functional test that affect door rigging. It mandates inspections and corrective actions to ensure proper door rigging and prevent premature cracking or in-flight door opening.

Airworthiness Directive
  • Bombardier BD-7002A12

EASA AD 2022-0171

Aug 19, 2022

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 1 / Safe Life Airworthiness Limitations Items — Amendment

The document titled 'Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 1 / Safe Life Airworthiness Limitations Items — Amendment' is an amendment concerning the Airbus A300 aircraft. It addresses updates to the airworthiness limitations related to time limits and maintenance checks, specifically focusing on safe life airworthiness limitation items. This amendment ensures continued compliance with safety standards for the Airbus A300 fleet.

Amendment
  • Airbus A300

EASA AD US-2022-13-10

Aug 17, 2022

Equipment / Furnishings - Boeing Material Specification (BMS) 8-39 Urethane Foam Pads - Replacement

The Federal Aviation Administration's Airworthiness Directive 2022-13-10 addresses certain Boeing 767-200, -300, -300F, and -400ER series airplanes. It mandates the replacement and removal of Boeing Material Specification (BMS) 8-39 urethane foam pads, which have deteriorating fire-retardant properties, with Nomex felt in specified areas. The directive also requires inspection and replacement of affected corner seals and prohibits installation of BMS 8-39 foam in certain locations.

Airworthiness Directive
  • Boeing 767200300300F400ER

EASA AD 2022-0147

Aug 17, 2022

Pneumatic – Overheat Detection System Sensing Elements – Inspection

EASA Airworthiness Directive 2022-0147 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses potential defects in certain overheat detection system (OHDS) sensing elements manufactured before 31 January 2021, which may fail to detect thermal bleed leak events properly. The directive mandates inspection and possible replacement of these affected parts to ensure continued airworthiness.

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

EASA AD 2022-0170-E

Aug 17, 2022

Superseded by EASA AD 2022-0181

EASA Airworthiness Directive 2022-0170-E is an emergency directive affecting Airbus A330-841 and A330-941 aeroplanes. It addresses issues related to leaking Bleed System High Pressure Valves (HPV) that may cause damage to the Pressure Regulating Valve and potentially lead to loss of aircraft control. The directive mandates amendments to the Aircraft Flight Manual and imposes dispatch restrictions to mitigate the risk.

Airworthiness DirectiveSuperseded
  • Airbus A330841941

EASA AD CF-2020-02R1

Aug 16, 2022

Auto Flight System — Airplane Flight Manual Limitations and Procedures — Velocity Decay during Low Level Altitudes Capture in One Engine Inoperative Conditions

The Auto Flight System — Airplane Flight Manual Limitations and Procedures — Velocity Decay during Low Level Altitudes Capture in One Engine Inoperative Conditions is a Canadian Airworthiness Directive CF-2020-02R1 addressing Bombardier CL-600 series aircraft, specifically models CL-600-1A11, CL-600-2A12, and CL-600-2B16. It focuses on the risk of significant airspeed decay during altitude capture modes (ALTSEL, ASEL, ALTS CAP) when operating with one engine inoperative. The directive mandates updates to the Airplane Flight Manual (AFM) to include new limitations and procedures to mitigate this unsafe condition.

Airworthiness Directive
  • Bombardier CL-600 (Challenger)
  • Bombardier CL-600-1A11
  • Bombardier CL-600-2A12
  • Bombardier CL-600-2B16

EASA AD CF-2022-45

Aug 16, 2022

Auto Flight System — Airplane Flight Manual Limitations and Procedures — Velocity Decay during Low Level Altitudes Capture (V) ALTS CAP or (V) ALTV CAP modes in One Engine Inoperative Conditions

Airworthiness Directive CF-2022-45 is issued by Transport Canada and addresses the Auto Flight System limitations and procedures related to velocity decay during low level altitude capture modes (V ALTS CAP or V ALTV CAP) in one engine inoperative conditions. This directive applies specifically to Bombardier Inc. CL-600-2B16 aircraft, serial numbers 5301 through 5665, 5701 through 5988, and 6050 through 6160. It mandates updates to the Airplane Flight Manual (AFM) to ensure safe operation during engine failure scenarios in these flight modes.

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

EASA AD CF-2022-46

Aug 16, 2022

Landing Gear — Forward Crosstube — New Airworthiness Limitation

The Canadian Airworthiness Directive CF-2022-46 addresses the landing gear forward crosstube on Bell Textron Inc. helicopters models 204B, 205A-1, 205B, 212, 214B, 214B-1, 412, 412 CF, and 412 EP modified with Dart Aerospace Ltd. forward crosstube part number D212-664-101/-101B. This directive introduces a new airworthiness limitation concerning the fatigue life of the forward crosstube to enhance safety. It mandates compliance with updated maintenance instructions to prevent structural failure during landing.

Airworthiness Directive
  • Bell Textron Inc. (Bti) 204B
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 212
  • Bell Textron Inc. (Bti) 412
  • Mcdermott 214 Holdings, 214
  • Bell Textron Inc. 204B
  • Bell Textron Inc. 205A-1
  • Bell Textron Inc. 205B
  • Bell Textron Inc. 212
  • Bell Textron Inc. 214B1
  • Bell Textron Inc. 412
  • Bell Textron Inc. 412 CF
  • Bell Textron Inc. 412 EP

EASA AD CF-2022-44

Aug 16, 2022

Superseded by TCCA AD CF-2023-09

Canadian Airworthiness Directive CF-2022-44 is a regulatory document addressing a safety issue in Bombardier BD-100-1A10 Challenger 300 and 350 aircraft. It concerns certain sensitive elements in the bleed air leak detection system that may have insufficient salt filling, potentially preventing detection of hot bleed air leaks. This directive mandates temporary revisions to the aircraft flight manual and prohibits installation of affected parts as spares.

Airworthiness Directive
  • Bombardier BD-1001A10 Challenger 3001A10 Challenger 350

EASA AD US-2022-15-07

Aug 15, 2022

Aircraft Flight Manual - Non-Normal Procedures Section - Amendment

The Aircraft Flight Manual - Non-Normal Procedures Section - Amendment is a final rule airworthiness directive issued by the Federal Aviation Administration (FAA) affecting certain Boeing 747-400 series airplanes with a three air data computer configuration. It addresses an unsafe condition related to loss of power to the right-hand side pitot-static probe heaters and conflicting procedures in the flightcrew operations manual and quick reference handbook.

Airworthiness Directive
  • Boeing 747400

EASA AD 2022-0162R1

Aug 12, 2022

Nacelles / Pylons — Thrust Reverser Intermediate Frame Fittings — Replacement

EASA Airworthiness Directive 2022-0162R1 is a regulatory document addressing the replacement of thrust reverser intermediate frame fittings on Airbus A380-841 and A380-842 aeroplanes. It specifically targets affected parts installed on engines #2 and #3 due to reported cracks that could lead to in-flight detachment of the thrust reverser external panel. The directive mandates replacement of these fittings with redesigned titanium parts to ensure continued airworthiness.

Airworthiness Directive
  • Airbus A380

EASA AD 2022-0169-E

Aug 12, 2022

Tail Rotor – Tail Rotor Blades – Inspection/Replacement

EASA Airworthiness Directive 2022-0169-E is an emergency directive addressing safety concerns for Airbus Helicopters SA 341 G and SA 342 J (Gazelle) models. It mandates inspection and possible replacement of tail rotor blades with specific part numbers due to manufacturing defects that could lead to in-flight tail rotor blade loss. The directive applies to all serial numbers of these helicopter models.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 341
  • Airbus Helicopters 342
  • Airbus Helicopters SA 341 G
  • Airbus Helicopters SA 342 J

EASA AD G-2022-0016

Aug 12, 2022

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

Civil Aviation Authority Airworthiness Directive G-2022-0016 addresses mandatory airworthiness limitations and maintenance requirements for all serial numbers of BAE Systems (Operations) Ltd ATP aeroplanes. It mandates compliance with the revised Aircraft Maintenance Manual Revision 95, dated 15 March 2022, including updated structurally significant item inspections and critical design configuration control limitations for the fuel system. This directive ensures continued airworthiness by enforcing updated life limits and inspection intervals.

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

EASA AD 2020-0098R2

Aug 12, 2022

Wings — Centre Wing Box Upper Cover Panel Fasteners — Inspection

The document titled 'Wings — Centre Wing Box Upper Cover Panel Fasteners — Inspection' is an informational Airworthiness Directive record related to the Airbus A400M military aircraft. It explains that no official EASA Airworthiness Directive exists for this subject because there are currently no Airbus A400M aeroplanes in civil service. The document serves as a recommendation for military airworthiness authorities to issue their own applicable directives.

Other
  • Airbus Military A400M
  • Airbus A400M

EASA AD 2022-0167

Aug 11, 2022

Flight Controls — Aileron Control Rod / Cover Panel Screws — Inspection

EASA Airworthiness Directive 2022-0167 is an airworthiness directive addressing the inspection of aileron control rod assemblies and cover panel screws on Costruzioni Aeronautiche TECNAM P2006T aeroplanes, specifically those with serial numbers up to 345 inclusive and select additional serial numbers. The directive mandates detailed inspections to detect damage and verify screw lengths to prevent potential control rod blockage. This AD applies to aileron control assemblies with part number 26-9-1502-000.

Airworthiness Directive
  • Tecnam P2006T
  • Costruzioni Aeronautiche TECNAM P2006T

EASA AD CF-2022-38R1

Aug 11, 2022

Pneumatic – Non-Conforming Bleed Leak Detection System Sensing Elements

Airworthiness Directive CF-2022-38R1 is issued by Transport Canada and applies to Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aeroplanes with specific serial numbers. It addresses a safety issue involving non-conforming bleed air leak detection system sensing elements that may have insufficient salt fill, potentially preventing detection of hot bleed air leaks. The directive mandates operational restrictions and maintenance actions to mitigate the risk of undetected bleed air leaks.

Airworthiness DirectiveSuperseded
  • Bombardier BD-7001A101A11