EASA Regulations & Airworthiness Directives

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

EASA AD US-2019-16-13

Oct 14, 2019

Fuel - Water and Fuel Scavenge System - Operating Limitations / Modification

Airworthiness Directive 2019-16-13 is a final rule issued by the Federal Aviation Administration affecting certain Boeing 777-200 and 777-300 series airplanes. It addresses issues with the water and fuel scavenge system that can cause trapped fuel and unavailable fuel reserves. The directive mandates operating limitations or modifications to the fuel scavenge and jettison systems, electrical wiring, and software installations to ensure safe operation.

Airworthiness Directive
  • Boeing 777200300

EASA SIB 2019-13

Oct 11, 2019

Controller Pilot Data Link Communications over Very High Frequency Data Link Mode 2 — Airborne Multi-Frequency Capability

EASA Safety Information Bulletin 2019-13 is an informational bulletin addressing the requirement for airborne multi-frequency capability in Controller Pilot Data Link Communications (CPDLC) over Very High Frequency Data Link Mode 2 (VDL Mode 2) systems. It applies to operators of aircraft equipped with VDL Mode 2 datalink installations operating within Single European Sky airspace. The bulletin emphasizes the need for automatic tuning (autotune) capability to support effective communication and compliance with relevant Commission Regulations.

Safety Information Bulletin

EASA AD 2019-0253-E

Oct 11, 2019

Engine fuel and Control — Fuel Pump Assembly — Replacement

EASA Airworthiness Directive 2019-0253-E is an emergency directive addressing the replacement of fuel pump assemblies in BRP-Rotax GmbH & Co KG Rotax 912 iSc2 Sport, 912 iSc3 Sport, and 915 iSc3 A engines. These engines are commonly installed on various general aviation aircraft either by the manufacturer or through Supplemental Type Certificates. The directive targets specific fuel pump assemblies with part numbers 889696 and 889698 within certain serial number ranges due to manufacturing deviations.

Airworthiness Directive
  • Brp-Rotax Gmbh & Co Kg 912 iSc
  • Brp-Rotax Gmbh & Co Kg 915

EASA AD US-2019-20-07

Oct 11, 2019

Flight Controls - Leading Edge Outboard Slats - Operational Checks; Airplane Flight Manual - Amendment

The Federal Aviation Administration's Airworthiness Directive 2019-20-07 addresses all Boeing 787-8, 787-9, and 787-10 airplanes. It mandates repetitive operational checks of the leading edge outboard slats and requires revising the airplane flight manual to prohibit flap retraction under icing conditions. The directive also updates maintenance or inspection programs to include new operational checks to ensure flight safety.

Airworthiness Directive
  • Boeing 7878910

EASA AD 2019-0252

Oct 10, 2019

Rotors Flight Control – Yaw Pedal Assemblies – Modification / Rework

EASA Airworthiness Directive 2019-0252 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Leonardo S.p.A. AW169 helicopters. It addresses a safety issue related to the pilot and co-pilot yaw pedal assemblies, specifically parts with certain part numbers that lack a required modification marking. The directive mandates modification or replacement of these affected parts to ensure continued safe operation of the helicopters.

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

EASA AD 2019-0248

Oct 9, 2019

CANCELLED BY EASA AD 2020-0240

EASA Airworthiness Directive 2019-0248 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Rolls-Royce Trent 1000 series engines installed on Boeing 787 aircraft. It mandates repetitive inspections of the intermediate pressure compressor (IPC) Rotor 1 and Rotor 2 blades and shaft to detect cracks that could lead to blade release and potential loss of aircraft control. The directive applies to multiple Trent 1000 engine variants except those modified with Rolls-Royce mod 72-J941.

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

EASA AD 2019-0250

Oct 9, 2019

Engine – Intermediate Pressure Compressor Blades / Shaft – Inspection

EASA Airworthiness Directive 2019-0250 is issued for Rolls-Royce Deutschland Trent 1000 series engines installed on Boeing 787 aircraft. It mandates repetitive inspections of intermediate pressure compressor (IPC) Rotor 1 and Rotor 2 blades and shaft assemblies to detect cracks that could lead to in-flight blade release. The directive updates inspection procedures and intervals to enhance engine safety.

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

EASA AD CF-2019-35

Oct 9, 2019

Fuselage Structure — Fretting or Cracking of Airframe Truss Clevis Lower Lug

Canadian Airworthiness Directive CF-2019-35 addresses fretting or cracking issues in the fuselage structure of Bell Helicopter Textron Canada Limited model 505 helicopters, serial number 65011 and subsequent. The directive mandates inspections and corrective actions for the airframe truss clevis lower lug to prevent potential structural failure. It applies specifically to the transmission restraint aft attachment hardware and related truss assemblies.

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

EASA AD 2019-0251

Oct 9, 2019

Pneumatic – Air Conditioning / Engine Bleed Air System – Software Update; Airplane Flight Manual / Master Minimum Equipment List – Air Conditioning / Engine Bleed Air System – Amendment

EASA Airworthiness Directive 2019-0251 is an airworthiness directive issued for Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses issues related to the pneumatic air conditioning and engine bleed air systems, specifically requiring software updates and operational changes to prevent overpressure and structural damage during take-off. The directive also mandates changes to the Airplane Flight Manual and Master Minimum Equipment List for affected aircraft.

Airworthiness DirectiveSuperseded
  • Airbus A380

EASA AD US-2019-19-12

Oct 8, 2019

Engine Fuel & Control - Engine Collective Position Transducer - Inspection

Airworthiness Directive 2019-19-12 is a final rule issued by the FAA addressing Sikorsky Aircraft Corporation Model S-76C helicopters equipped with Turbomeca Arriel 2S1 or 2S2 engines that have engine collective position transducers (CPT) part numbers 76900-01821-104 or 76900-01821-105 installed. This directive mandates inspections and potential replacement of the CPT to prevent failure that could lead to engine control issues. It updates and expands upon the previous AD 2018-10-07 by including an additional CPT part number.

Airworthiness Directive
  • Sikorsky S-76
  • Sikorsky S-76C

EASA SIB CE-19-09

Oct 7, 2019

Mitsubishi MU-2B aeroplanes - Wing Spacer Plates Inspection

The Special Airworthiness Information Bulletin SAIB: CE-19-09 is an FAA informational bulletin addressing wing spacer plate inspections for Mitsubishi Heavy Industries Ltd. Models MU-2B series airplanes, including MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, MU-2B-25, MU-2B-26, MU-2B-26A, MU-2B-30, MU-2B-35, MU-2B-36, MU-2B-36A, MU-2B-40, and MU-2B-60. It informs owners and operators about procedures to detect and correct cracks in wing spacer plates to maintain wing structural integrity.

Safety Information Bulletin

EASA AD 2019-0247-E

Oct 4, 2019

Engine — Module 01 26-Teeth Bevel Gear — Replacement

EASA Airworthiness Directive 2019-0247-E is an emergency directive addressing SAFRAN HELICOPTER ENGINES MAKILA 2A and 2A1 engines installed on helicopters such as the Airbus Helicopters EC 225 LP. It mandates the replacement of Module 01 26-tooth bevel gears with specific part numbers and serial numbers due to a manufacturing quality issue causing gear tooth rupture. The directive aims to prevent engine in-flight shutdowns and potential loss of helicopter power.

Airworthiness Directive
  • Safran MAKILA 2
  • Airbus Helicopters EC 225 LP

EASA AD US-2019-18-08

Oct 4, 2019

Superseded by FAA AD 2021-26-04

Airworthiness Directive 2019-18-08 is a final rule issued by the FAA affecting all Engine Alliance GP7270 and GP7277 model turbofan engines. This directive addresses an unsafe condition related to potential cracks and damage in the engine fan hub assembly, which could lead to uncontained engine failure. It mandates inspections and possible part replacements to ensure continued airworthiness.

Airworthiness Directive
  • Engine Alliance GP7200

EASA AD US-2019-20-02

Oct 3, 2019

Superseded by FAA AD 2019-22-10

FAA Airworthiness Directive 2019-20-02 is a final rule addressing all Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes. It mandates repetitive inspections for cracking in the left and right side outboard chords of the station 663.75 frame fittings and failsafe straps adjacent to stringer S-18A straps, with required repairs if cracking is found. This directive aims to maintain structural integrity and prevent potential loss of airplane control.

Airworthiness Directive
  • Boeing 737600700700C800900900ER

EASA AD 2019-0245

Oct 1, 2019

Burner — Modification

Burner — Modification is a regulatory document addressing modifications to burners used in various hot air balloon models, including AEROSTATS MA Series, BALLONS CHAIZE CS, JZ, and JZX Series, BALLONS LIBERT, BALLONSERVICE & TECHNIK Schoen, CAMERON Special Shape, Gas and Helium Hot Air Balloons, Sky Hot Air Balloons, KUBICEK FACTORY AB 2 and AB 8, AEROTECHNIK AB, BB, Special Shape Hot Air Balloons, LINDSTRAND TECHNOLOGIES 203T HiFlyer, SCHROEDER FIRE BALLOONS G and S, and ULTRAMAGIC Hot Air Balloons. The document specifies modifications applicable to burners installed on these hot air balloon types.

Airworthiness Directive
  • Aerostats MA Series Hot Air Balloons
  • Ballons Chaize CS SERIES HOT AIR BALLOONS
  • Ballons Chaize JZ SERIES HOT AIR BALLOONS
  • Ballons Chaize JZX SERIES HOT AIR BALLOONS
  • Ballons Libert Libert Hot Air Balloons
  • Ballonservice & Technik Schoen Hot Air Balloons
  • Cameron Balloons Cameron Special Shape Hot Air Balloons
  • Cameron Balloons Gas Balloons
  • Cameron Balloons Helium-Hot Air Balloons
  • Cameron Balloons Hot Air Balloons
  • Cameron Balloons Sky Hot Air Balloons
  • Kubicek Factory S.R.O AB 2 Hot Air Balloons
  • Kubicek Factory S.R.O AB 8 Hot Air Balloons
  • Kubicek Factory S.R.O AEROTECHNIK AB Hot Air Balloons
  • Kubicek Factory S.R.O BB Hot Air Balloons
  • Kubicek Factory S.R.O Special Shape Hot Air Balloons
  • Lindstrand Technologies 203T HiFlyer
  • Schroeder Fire Balloons fire balloons G
  • Schroeder Fire Balloons fire balloons S - Special Shape Balloons
  • Ultramagic Hot Air Balloons
  • Ultramagic Special Shape Hot Air Balloons
  • AEROSTATS MA Series
  • BALLONS CHAIZE CS Series
  • BALLONS CHAIZE JZ Series
  • BALLONS CHAIZE JZX Series
  • BALLONS LIBERT
  • BALLONSERVICE & TECHNIK Schoen
  • CAMERON Special Shape
  • Gas and Helium Hot Air Balloons
  • Sky Hot Air Balloons
  • KUBICEK FACTORY AB 2
  • KUBICEK FACTORY AB 8
  • AEROTECHNIK AB
  • AEROTECHNIK BB
  • Special Shape Hot Air Balloons
  • SCHROEDER FIRE BALLOONS G
  • SCHROEDER FIRE BALLOONS S

EASA AD 2019-0219

Oct 1, 2019

[Correction] Fuselage — Fuselage Bulk Cargo Door Frames — Inspection / Repair

The document titled '[Correction] Fuselage — Fuselage Bulk Cargo Door Frames — Inspection / Repair' is an airworthiness directive correction applicable to Airbus Defence & Space S.A. EASA STC 10034690 and Airbus S.A.S. A330 aircraft. It addresses inspection and repair requirements specifically for the fuselage bulk cargo door frames on these aircraft models. The directive aims to ensure continued structural integrity and safety of the affected fuselage components.

Airworthiness Directive
  • Airbus A330
  • Airbus Defence & Space A330

EASA AD CF-2017-05R2

Oct 1, 2019

Fuel System — Motive Flow Line Fouling, Motive Flow Line and Pressure Relief Line Broken P-Clamps, and Vent Line TeflonTM Sleeve Installation

The Canadian Airworthiness Directive CF-2017-05R2 titled 'Fuel System — Motive Flow Line Fouling, Motive Flow Line and Pressure Relief Line Broken P-Clamps, and Vent Line TeflonTM Sleeve Installation' applies to De Havilland DHC-8-400 series aircraft with serial numbers 4001, 4003, and subsequent. It addresses issues related to broken P-clamps on fuel system lines, interference causing wear on the motive flow line, and improper installation of Teflon sleeves on vent lines that could lead to fuel tank ignition risks during lightning strikes.

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

EASA AD US-2019-17-01

Oct 1, 2019

Fuselage - Upper Fuselage Skin - Inspection / Repair

Federal Register Airworthiness Directive 2019-17-01 is a final rule issued by the FAA addressing certain Learjet, Inc. Model 60 airplanes. It mandates inspections and repairs of the upper fuselage skin to detect and correct corrosion that could compromise structural integrity. This directive updates previous requirements by clarifying inspection areas and compliance times.

Airworthiness Directive
  • Learjet, 60
  • Learjet 60

EASA AD 2019-0246

Oct 1, 2019

Rotors Flight Control — Collective Controls / Protective Cover — Modification

EASA Airworthiness Directive 2019-0246 is an airworthiness directive addressing Airbus Helicopters EC 155 B and EC 155 B1 models. It focuses on the modification of the protective cover for the "SHEAR" control pushbutton on pilot and copilot collective sticks to prevent mechanical deformation and potential unintended shearing of the hoist cable.

Airworthiness Directive
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Airbus Helicopters EC 155 B
  • Airbus Helicopters EC 155 B1

EASA AD 2019-0244

Sep 30, 2019

Engine Controls – Push-pull Control and Beta Switch – Inspection /; Replacement

EASA Airworthiness Directive 2019-0244 is an airworthiness directive addressing safety issues in GE Aviation Czech H80-200 and H85-200 engines installed on Aircraft Industries L 410 UVP-E20, L 410 UVP-E20 CARGO, and L 410 NG aeroplanes. It mandates inspections, adjustments, and modifications of the engine push-pull control and beta switch components to prevent uncommanded propeller reverse and potential loss of aircraft control. The directive applies to specific engine configurations and propeller combinations.

Airworthiness DirectiveSuperseded
  • Ge Aviation Czech H75, H80, H85
  • Aircraft Industries L 410 UVP-E20
  • Aircraft Industries L 410 UVP-E20 CARGO
  • Aircraft Industries L 410 NG