EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350224Airbus A330221Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941134Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787116Show all...

EASA AD 2019-0193

Aug 7, 2019

Tail Rotor – Tail Rotor Servo Actuator / Duplex Bearing – Inspection /; Check

EASA Airworthiness Directive 2019-0193 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all serial numbers of Leonardo S.p.A. AW169 and AW189 helicopters. The directive addresses inspections and monitoring of the tail rotor servo actuator and duplex bearing to prevent potential loss of yaw control. It mandates repetitive inspections, thermal strip installations, and reporting requirements to ensure continued airworthiness and safety of these helicopter models.

Airworthiness DirectiveSuperseded
  • Leonardo S.P.A. Helicopters AW169
  • Leonardo S.P.A. Helicopters AW189
  • Leonardo AW169
  • Leonardo AW189

EASA AD 2019-0192

Aug 5, 2019

Electrical Power — Ram Air Turbine Free Rotation — Manual Check

EASA Airworthiness Directive 2019-0192 is an airworthiness directive addressing the Airbus A380 aeroplanes equipped with specific Ram Air Turbine (RAT) parts, identified by part numbers 1704287G and 1704287H with serial numbers AAB4000001 to AAB4000333. This directive mandates a manual free rotation check of the RAT to detect water ingress and corrosion that could impair RAT operation and electrical power generation. It applies to Airbus A380 models -841, -842, and -861 with specified manufacturer serial numbers.

Airworthiness Directive
  • Airbus A380

EASA AD 2019-0187

Aug 2, 2019

[Correction] Powerplant — Engine Cooling Fan — Replacement

EASA Airworthiness Directive 2019-0187 is a corrective directive addressing the replacement of engine cooling fans on Hélicoptères Guimbal Cabri G2 helicopters. It applies to specific aluminium cooling fan part numbers G52-00-000, G52-00-001, and G52-04-100, requiring replacement with a serviceable composite front flange cooling fan P/N G52-04-101. The directive aims to prevent engine in-flight shutdowns caused by cooling fan failures.

Airworthiness Directive
  • Guimbal, Helicopteres CABRI
  • Hélicoptères Guimbal Cabri G2

EASA AD 2018-0249R1

Aug 2, 2019

[Correction] Wings — Centre Wing Box Fastener Holes at Frame 40 Vertical Web — Inspection / Modification

EASA Airworthiness Directive 2018-0249R1 is a regulatory update addressing inspection and modification requirements for the centre wing box fastener holes at Frame 40 vertical web on Airbus A330 and A340 aeroplanes. It applies to multiple A330 and A340 variants, excluding those with specific Airbus Repair Instructions embodied. The directive mandates repetitive special detailed inspections and corrective actions to ensure structural integrity of the centre fuselage.

Airworthiness Directive
  • Airbus A330
  • Airbus A340

EASA AD CF-2002-39R2

Aug 2, 2019

Fuselage Pressure Floor Skin

Airworthiness Directive CF-2002-39R2 addresses the fuselage pressure floor skin on Bombardier Inc. model CL-600-2B19 aeroplanes, serial numbers 7003 through 8999. This directive mandates revised inspection requirements to detect and correct fatigue cracks that could lead to rapid decompression during flight. It updates maintenance schedules and inspection tasks to enhance structural safety of the affected aircraft.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2B19

EASA AD CF-2010-30R2

Aug 1, 2019

Cracking of the Nacelle Attachment Fitting(s)

The Canadian Airworthiness Directive CF-2010-30R2 addresses cracking issues in the nacelle attachment fittings of De Havilland Aircraft of Canada Limited model DHC-8-400, -401, and -402 aeroplanes, serial numbers 4001 and subsequent. It mandates inspections and modifications to ensure structural integrity and safe landing operations. The directive applies to specific part numbers of nacelle attachment fittings and outlines inspection and replacement procedures.

Airworthiness Directive
  • De Havilland Canada DHC-8
  • De Havilland DHC-8-400
  • De Havilland DHC-8-401
  • De Havilland DHC-8-402

EASA AD CF-2014-08R1

Aug 1, 2019

Doors — Translating Doors Loose Bolts

The Airworthiness Directive CF-2014-08R1 is issued by Transport Canada and applies to De Havilland Aircraft of Canada Limited model DHC-8-400, -401, and -402 aeroplanes with serial numbers 4001 through 4530. It addresses the issue of loose bolts in the translating door crank assemblies, which can prevent emergency exits from opening. This directive mandates inspections and modifications to ensure the secure retention of door crank assembly bolts on emergency and reclassified doors.

Airworthiness Directive
  • De Havilland Canada DHC-8
  • De Havilland DHC-8-400
  • De Havilland DHC-8-401
  • De Havilland DHC-8-402

EASA AD 2019-0191-E

Jul 31, 2019

Equipment / Furnishings – Hoist Carrier Assembly Bracket / Bolts – Inspection / Replacement

EASA Airworthiness Directive 2019-0191-E is an emergency directive addressing safety concerns for all serial numbers of PZL W-3A helicopters manufactured by WSK “PZL-ŚWIDNIK” S.A. It mandates inspections and replacements related to the hoist carrier assembly brackets and bolts, specifically parts with numbers 39.30.205.03.01, 39.30.213.00.00, and hoists type 76378. The directive aims to prevent potential detachment of the hoist bracket that could cause damage, injury, or loss of life.

Airworthiness DirectiveSuperseded
  • Wsk Pzl-Swidnik PZL W-3A
  • PZL W-3A

EASA AD 2019-0188

Jul 31, 2019

Hydraulic Power — Hydraulic Reservoir Air Pressurization System Lines — Functional Tests

EASA Airworthiness Directive 2019-0188 is an airworthiness directive affecting Airbus A300-600, A300-600ST, and A310 aeroplanes. It mandates functional tests of the hydraulic reservoir air pressurization system lines to detect pipe ruptures and air leaks. The directive ensures continued airworthiness by requiring specific maintenance tasks related to hydraulic power systems.

Airworthiness Directive
  • Airbus A300-600
  • Airbus A300-600ST (Beluga)
  • Airbus A310
  • Airbus A300-600ST

EASA AD 2019-0189

Jul 31, 2019

Superseded by EASA AD 2020-0125

EASA Airworthiness Directive 2019-0189 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A320-251N, A320-253N, A320-271N, and A320-273N aeroplanes. This directive addresses a potential reduced efficiency of the angle of attack protection in certain flight configurations and maneuvers, which could lead to excessive pitch attitude and increased pilot workload. The directive requires amendments to the Aircraft Flight Manual to incorporate specific temporary revisions.

Airworthiness DirectiveSuperseded
  • Airbus A320251N253N271N273N

EASA AD 2019-0186

Jul 30, 2019

Rotors Flight Control - Main Rotor / Non-Rotating Scissor Link - Replacement

EASA Airworthiness Directive 2019-0186 is an airworthiness directive addressing the replacement of the main rotor non-rotating scissor link, part number G41-10-200, on Hélicoptères Guimbal Cabri G2 helicopters. This directive applies to all serial numbers of the Cabri G2 and mandates the replacement of affected parts with serviceable parts having part number G41-10-201. The directive aims to ensure continued safe flight control by mitigating risks associated with cracked rotor components.

Airworthiness Directive
  • Guimbal, Helicopteres CABRI
  • Hélicoptères Guimbal Cabri G2

EASA AD 2019-0185

Jul 30, 2019

Rotors Flight Control — Main Rotor / Swashplate Guide Bellcrank Bushing — Replacement

EASA Airworthiness Directive 2019-0185 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Hélicoptères Guimbal Cabri G2 helicopters. It addresses the replacement of metal bushings installed on the main rotor swashplate guide bellcrank with plastic bushings to prevent potential structural failure. This directive applies to all serial numbers of the Cabri G2 helicopter.

Airworthiness Directive
  • Guimbal, Helicopteres CABRI
  • Hélicoptères Guimbal Cabri G2

EASA AD 2019-0184

Jul 29, 2019

Rotors Flight Control — Main Rotor Servo Actuators — Inspection

EASA Airworthiness Directive 2019-0184 is an airworthiness directive addressing the inspection of main rotor servo actuators on Airbus Helicopters models SA 365, AS 365, EC155, AS 350, EC 130, and AS355. The directive targets specific part numbers of main rotor servo actuators to ensure the correct installation of the threaded-shouldered bushing to prevent potential loss of helicopter control.

Airworthiness Directive
  • Airbus Helicopters AS 350
  • Airbus Helicopters EC 130
  • Airbus Helicopters AS 355
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Airbus Helicopters SA 365
  • Airbus Helicopters EC155
  • Airbus Helicopters AS355

EASA AD 2019-0183

Jul 26, 2019

Electric and Electronic Common Installation — Cargo Lining Gutter Assemblies — Modification

EASA Airworthiness Directive 2019-0183 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes. It mandates a modification to the electric and electronic common installation, specifically the cargo lining gutter assemblies, to improve water drainage and prevent potential water spillage risks. This directive applies to all Airbus A350-941 aircraft except those with Airbus modification 111827 incorporated in production.

Airworthiness Directive
  • Airbus A350941

EASA AD CF-2019-28

Jul 26, 2019

Flight Controls — Swashplate Assembly — Improperly Staked Bearings

Canadian Airworthiness Directive CF-2019-28 addresses an issue with improperly staked bearings in the swashplate assembly of Bell Helicopter Textron Canada Limited model 505 helicopters, serial numbers 65011 through 65211. The directive mandates inspection and correction of the swashplate assembly bearings to ensure safe flight controls. This AD aims to prevent potential loss of helicopter control caused by bearing migration and subsequent control system failure.

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

EASA AD 2019-0182

Jul 26, 2019

Landing Gear — Enhanced Main Landing Gear Strut Assembly — Inspection

EASA Airworthiness Directive 2019-0182 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Leonardo S.p.A. A109 helicopters, specifically the A109E, A109LUH, A109S, and AW109SP models. It addresses inspection requirements for the enhanced main landing gear strut assemblies with certain part numbers and serial numbers due to reported failures. The directive mandates repetitive inspections and corrosion prevention measures to ensure continued airworthiness.

Airworthiness Directive
  • Leonardo S.P.A. Helicopters A109
  • Leonardo S.P.A. Helicopters A119
  • Leonardo A109E
  • Leonardo A109LUH
  • Leonardo A109S
  • Leonardo AW109SP

EASA AD 2019-0180

Jul 25, 2019

Engine Fuel & Control — Fuel Filter Pre-blockage Pressure Switch — Operational Check

EASA Airworthiness Directive 2019-0180 is an airworthiness directive addressing SAFRAN Helicopter Engines ARRIEL 2 series engines installed on various helicopters including Airbus Helicopters AS 350 B3, EC 130 B4, AS 365 N3, EC 155 B, and Sikorsky S-76C. The directive mandates operational checks and visual inspections of the fuel filter pre-blockage pressure switch to ensure proper functionality and prevent uncommanded engine shutdowns due to fuel contamination.

Airworthiness Directive
  • Safran ARRIEL 2
  • Airbus Helicopters AS 350 B3
  • Airbus Helicopters EC 130 B4
  • Airbus Helicopters AS 365 N3
  • Airbus Helicopters EC 155 B
  • Sikorsky S-76C

EASA SIB CASA-2019-04

Jul 25, 2019

Pratt & Whitney Canada PT6B-37A Engines - Compliance with AD CF-2019-05

The document titled 'Pratt & Whitney Canada PT6B-37A Engines - Compliance with AD CF-2019-05' is a Civil Aviation Safety Alert issued by Transport Canada. It addresses the mandatory replacement of fuel control units on Pratt & Whitney Canada PT6B-37A engines installed on Leonardo A119 and AW119MKII helicopter models. The alert informs operators and maintainers about the upcoming compliance deadline for Airworthiness Directive CF-2019-05.

Safety Directive