EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

EASA AD 2019-0059

SUPERSEDED BY EASA AD 2021-0261

EASA Airworthiness Directive 2019-0059 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 aeroplanes, including models A330-201 through A330-343. It mandates compliance with the Airbus A330 Airworthiness Limitations Section (ALS) Part 2, Revision 03, which includes damage tolerant airworthiness limitation items critical for continued airworthiness. This directive ensures operators maintain updated maintenance programs aligned with the latest safety requirements.

Mar 20, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD US-2019-01-06

Fuselage - Frame Web and Doubler - Inspection

The Federal Aviation Administration's Airworthiness Directive 2019-01-06 addresses all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. This directive mandates repetitive surface high frequency eddy current inspections of the fuselage frame web and doubler at body station 303.9, specifically at the stop fitting at stringer 16 left, to detect cracks. The directive aims to ensure structural integrity and prevent potential rapid decompression.

Mar 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD US-2019-01-03

Landing Gear - Trunnion Pin Assemblies - Inspection / Lubrication / Replacement

The Federal Aviation Administration's Airworthiness Directive 2019-01-03 addresses inspection, lubrication, and replacement requirements for the forward and aft trunnion pin assemblies of the main landing gears on certain Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This directive updates previous requirements to include all affected airplanes and prohibits installation of certain landing gear components unless specific conditions are met. It aims to prevent corrosion and chrome damage that could lead to landing gear collapse.

Mar 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-600Boeing 737-700Boeing 737-700CBoeing 737-800Boeing 737-900Boeing 737-900ER

EASA AD 2019-0055-E

SUPERSEDED BY EASA AD 2019-0253-E

EASA Airworthiness Directive 2019-0055-E is an emergency directive addressing a fuel pump assembly issue in BRP-Rotax GmbH & Co KG Rotax 912 iSc2 Sport, 912 iSc3 Sport, and 915 iSc3 A engines. The directive mandates inspection and possible replacement of specific fuel pump assemblies identified by part numbers 889696 and 889698 with serial numbers from 180500 to 189999. These engines are commonly installed on various general aviation aircraft either by original manufacturer installation or Supplemental Type Certificate modifications.

Mar 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBrp-Rotax Gmbh & Co Kg 912 iScBrp-Rotax Gmbh & Co Kg 915

EASA AD 2019-0056

SUPERSEDED BY EASA AD 2020-0080

EASA Airworthiness Directive 2019-0056 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses the Safe Life Airworthiness Limitation Items specified in the Airbus Airworthiness Limitations Section (ALS) Part 1 Revision 06 issue 2. The directive ensures that operators comply with updated maintenance and replacement requirements for life-limited components to maintain continued airworthiness.

Mar 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2019-0054

Nacelles / Pylons — Engine Mounting Structure — Modification

EASA Airworthiness Directive 2019-0054 is an airworthiness directive issued by EASA affecting SAAB 2000 aeroplanes, excluding serial numbers 006, 043, 056, and 061. It addresses a potential unsafe condition related to the engine mounting structure on these aircraft. The directive mandates a modification to the nacelle upper longeron and associated engine mounting structure to prevent structural failures.

Mar 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtSaab Ab 2000SAAB 2000

EASA AD US-2019-01-08

SUPERSEDED BY FAA AD 2021-19-15

FAA Airworthiness Directive 2019-01-08 is a final rule addressing certain Boeing 777-200, -200LR, -300, and -300ER series airplanes. It mandates modifications to galley-mounted flight attendant seat fittings due to identified non-compliance issues that could cause seat failure in high-G crash conditions. This directive aims to enhance flight attendant safety and ensure their ability to assist in passenger evacuation.

Mar 18, 2019
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 777Boeing 777-200Boeing 777-200LRBoeing 777-300Boeing 777-300ER

EASA AD 2019-0052

Exhaust — Exhaust Ducts and Clamps — Inspection / Modification

EASA Airworthiness Directive 2019-0052 is an airworthiness directive addressing exhaust ducts and clamps on all serial numbers of PZL SW-4 helicopters manufactured by WSK “PZL – ŚWIDNIK” S.A. It mandates inspections and modifications to prevent clamp cracking and exhaust duct damage that could compromise helicopter control. The directive includes detailed inspection, repair, and replacement instructions to ensure continued airworthiness.

Mar 14, 2019
Airworthiness DirectiveMaintenanceSafety MgmtWsk Pzl-Swidnik SW4PZL SW-4

EASA AD US-2019-05-01

Engine - Diffuser & High Pressure Turbine Case - Inspection

The Federal Aviation Administration's Airworthiness Directive 2019-05-01 addresses Pratt & Whitney turbofan engines including models PW2037, PW2037D, PW2037M, PW2040, PW2040D, PW2043, PW2143, PW2643, and F117-PW-100. This directive mandates inspections of the engine diffuser and high-pressure turbine (HPT) cases to detect potential cracks and prevent flange ruptures. It updates previous inspection requirements to enhance engine safety and reliability.

Mar 13, 2019
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney PW2000

EASA SIB 2019-05

Rockwell Collins GPS Receiver GPS-4000S - Reduced Availability of Localizer Performance with Vertical Guidance Procedures

EASA Safety Information Bulletin 2019-05 is a safety information bulletin addressing the reduced availability of Localizer Performance with Vertical Guidance (LPV) procedures for aircraft equipped with the Collins Aerospace GPS-4000S receiver, Part Number 822-2189-100, mod 14 or less. The bulletin highlights an issue where the GPS-4000S receiver may lose lock on the EGNOS satellite and revert to GPS mode without EGNOS corrections, affecting LPV and RNP APCH approaches using GNSS/SBAS geometric altitude.

Mar 13, 2019
Safety Information BulletinSafety Mgmt

EASA SD SD-2019-01

SUPERSEDED BY EASA SD 2021-01

EASA Safety Directive 2019-01 is an emergency directive addressing the Boeing 737-8 MAX and 737-9 MAX aircraft models. It mandates the suspension of commercial air transport operations of these aircraft into, within, or out of the European Union territory due to safety concerns following two fatal accidents. This directive serves as an interim safety measure pending further investigation and additional actions.

Mar 12, 2019
Safety DirectiveFlight OpsSafety Mgmt

EASA AD 2017-0209R1

Integrated Modular Avionics — Internal Timer — Power Cycle (Reset)

EASA Airworthiness Directive 2017-0209R1 is an updated regulation addressing an internal timer issue in the Integrated Modular Avionics of Airbus A380-841, A380-842, and A380-861 aircraft. It applies to all serial numbers except those with Airbus modifications 77908 and 77909 incorporated during production. The directive mandates repetitive on-ground power cycles to reset the internal timer to prevent loss of communication between avionics systems.

Mar 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2019-0046

SUPERSEDED BY EASA AD 2020-0212

EASA Airworthiness Directive 2019-0046 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters SA 365, AS 365, and EC 155 models. It addresses a safety issue related to the tail rotor drive flange of the main gearbox on these helicopters, specifically concerning the Shur-Lok nut that retains the tail rotor drive flange. The directive mandates a modification to prevent potential loss of tail rotor drive control.

Mar 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters SA 365

EASA AD 2019-0049

SUPERSEDED BY EASA AD 2021-0248

EASA Airworthiness Directive 2019-0049 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 aeroplanes, including models A330-201 through A330-343. This directive mandates compliance with updated airworthiness limitations specified in Airbus A330 Airworthiness Limitations Section Part 3, Revision 06. It ensures operators maintain the continuing airworthiness of these aircraft by following the approved maintenance program.

Mar 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 2019-0050

SUPERSEDED BY EASA AD 2021-0249

EASA Airworthiness Directive 2019-0050 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A340 variants including A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643. It mandates compliance with updated airworthiness limitations as specified in Airbus A340 Airworthiness Limitations Section Part 3, Revision 04. This directive ensures continued airworthiness by enforcing maintenance tasks and intervals approved by EASA.

Mar 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A340Airbus A340-211Airbus A340-212Airbus A340-213Airbus A340-311Airbus A340-312Airbus A340-313Airbus A340-541Airbus A340-542Airbus A340-642Airbus A340-643

EASA AD 2019-0047

SUPERSEDED BY EASA AD 2021-0250

EASA Airworthiness Directive 2019-0047 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 aeroplanes, including models A330-201 through A330-343. It mandates compliance with updated airworthiness limitations related to system equipment maintenance requirements as specified in Airbus A330 Airworthiness Limitations Section Part 4 Revision 07. The directive ensures continued safe operation by enforcing maintenance tasks and life limit replacements.

Mar 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 2019-0048

SUPERSEDED BY EASA AD 2021-0251

EASA Airworthiness Directive 2019-0048 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A340 models, including A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643. This directive mandates compliance with updated airworthiness limitations specified in Airbus A340 Airworthiness Limitations Section Part 4 Revision 06, focusing on system equipment maintenance requirements. It ensures continued airworthiness by enforcing maintenance tasks and life limits for components as approved by EASA.

Mar 11, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A340Airbus A340-211Airbus A340-212Airbus A340-213Airbus A340-311Airbus A340-312Airbus A340-313Airbus A340-541Airbus A340-542Airbus A340-642Airbus A340-643

EASA AD CF-2019-09

Avionic System — Airplane Flight Manual Navigation System Limitations — Prohibit Editing CLIMB TO Altitudes and Use of Temperature Compensation on Flight Management System

Airworthiness Directive CF-2019-09 is issued by Transport Canada and applies to Bombardier Inc. model BD-100-1A10 aircraft, serial numbers 20002 and subsequent, equipped with FMS-5000 software version 4.X. The directive addresses limitations in the airplane flight manual related to the navigation system, specifically prohibiting editing CLIMB TO altitudes and the use of temperature compensation on the Flight Management System (FMS).

Mar 8, 2019
Airworthiness DirectiveFlight OpsSafety MgmtBombardier BD-100Bombardier BD-100-1A10

EASA AD CF-2019-10

Avionic System — Airplane Flight Manual Navigation System Limitations — Prohibit Editing CLIMB TO Altitudes and Use of Temperature Compensation on Flight Management System

Airworthiness Directive CF-2019-10 is issued by Transport Canada and applies to Bombardier Inc. model CL-600-2B16 aircraft, serial numbers 5301 and subsequent, equipped with FMS-6000 software versions 3.3.X through 4.X. This directive addresses limitations in the airplane flight manual related to the navigation system, specifically prohibiting editing of CLIMB TO altitudes and the use of temperature compensation on the Flight Management System (FMS).

Mar 8, 2019
Airworthiness DirectiveFlight OpsSafety MgmtBombardier CL-600 (Challenger)Bombardier CL-600-2B16