EASA Regulations for Airbus A380-842

56 airworthiness directives and regulations affecting Airbus A380-842.

EASA AD 2022-0106

Jun 10, 2022

Time Limits / Maintenance Checks – Damage Tolerant Airworthiness Limitation Items – Airworthiness Limitations Section Part 2 – Amendment

EASA Airworthiness Directive 2022-0106 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with the updated Airbus A380 Airworthiness Limitations Section Part 2 Revision 10, which includes damage tolerant airworthiness limitation items necessary for continued safe operation of these aircraft.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2022-0094

May 25, 2022

Pneumatic — Air Conditioning / Engine Bleed Air System — Software Update; Airplane Flight Manual / Master Minimum Equipment List — Air Conditioning / Engine Bleed Air System — Amendment; Pneumatic — Engine Bleed Air Supply Over-pressure Valve — Replacement; Ice and Rain Protection — Anti-ice Control Unit — Replacement

EASA Airworthiness Directive 2022-0094 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses issues related to the pneumatic air conditioning and engine bleed air systems, including software updates, replacement of engine bleed air supply over-pressure valves, and replacement of anti-ice control units. The directive also amends the Airplane Flight Manual and Master Minimum Equipment List for these systems.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2022-0075

Apr 28, 2022

Landing Gear – Body Landing Gear Rear Axle – Replacement

EASA Airworthiness Directive 2022-0075 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses the replacement of right-hand and left-hand body landing gear rear axles that have been identified as affected due to corrosion and potential failure. The directive mandates inspection and replacement of these parts to ensure continued airworthiness.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2022-0022

Feb 2, 2022

Flight Controls — Aileron Servo Controls — Replacement

EASA Airworthiness Directive 2022-0022 is an official regulatory document addressing the replacement of aileron servo controls on Airbus A380-841, A380-842, and A380-861 aeroplanes. The directive targets specific part numbers of aileron servo controls that may suffer from a fatigue issue potentially leading to failure or detachment, which could reduce aircraft control. It mandates removal of affected parts and installation of serviceable parts to ensure continued airworthiness.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2022-0019

Jan 31, 2022

Wings – Front and Rear Spars – Inspection

EASA Airworthiness Directive 2022-0019 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. 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 structural integrity. This directive applies to all manufacturer serial numbers and wing box assembly dates as specified.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2021-0284

Dec 17, 2021

Engine Fuel & Control — Electronic Engine Control Software — Update

EASA Airworthiness Directive 2021-0284 is an airworthiness directive affecting Airbus A380-841 and A380-842 aeroplanes equipped with Rolls-Royce Trent 900 engines. It addresses the Electronic Engine Control (EEC) software, specifically requiring an update to a newer software standard to prevent engine thrust control loss. The directive applies to all manufacturer serial numbers of these aircraft models.

Airworthiness Directive
  • Airbus A380841842

EASA AD 2021-0221

Oct 1, 2021

Air Conditioning — Belly Fairing Air Cooling Pack Discharge Duct Adjustable Rods — Replacement / Electrical Power — Generator and Ground Power Control Unit — Replacement / Software Update / Equipment / Furnishings — Modified Door Lining Panels — Installation / Fuel — Refuel Diffusers / Engine Feed Fuel Pipe End Fittings — Replacement / Fuselage — Nose Landing Gear Bay Bulkhead Panel — Inspection / Powerplant — Redesigned Fan Cowl Latch Access Panels — Installation

EASA Airworthiness Directive 2021-0221 is an official regulatory document addressing multiple modifications, replacements, inspections, and software updates for Airbus A380-841, A380-842, and A380-861 aeroplanes. It covers components including air conditioning belly fairing air cooling pack discharge duct adjustable rods, electrical power generator and ground power control units, door lining panels, fuel refuel diffusers and engine feed fuel pipe end fittings, nose landing gear bay bulkhead panel, and redesigned fan cowl latch access panels. The directive applies to specific manufacturer serial numbers of Airbus A380 aircraft.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2021-0219

Sep 28, 2021

Landing Gear — Wing / Body Landing Gear Retraction Actuators — Modification / Replacement

EASA Airworthiness Directive 2021-0219 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses the wing and body landing gear retraction actuator assemblies with specific part numbers and serial numbers. The directive mandates modification or replacement of these affected parts to ensure continued airworthiness.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2021-0145

Jun 18, 2021

Wings — Wing Tip Assembly — Modification

EASA Airworthiness Directive 2021-0145 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses a potential structural integrity issue in the wing tip assemblies caused by parts made from 7449 aluminium alloy. The directive mandates modification of the wing tip assemblies to a new design using 7010 aluminium alloy to prevent cracking.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2021-0087

Mar 24, 2021

Engine Fuel & Control — Master Minimum Equipment List — Handling Bleed Valve Inoperative — Amendment

EASA Airworthiness Directive 2021-0087 is an amendment addressing the Airbus A380-841 and A380-842 aeroplanes. It focuses on the engine fuel and control system, specifically handling the bleed valve inoperative condition as outlined in the Master Minimum Equipment List (MMEL). This directive mandates changes to dispatch restrictions to ensure continued airworthiness and safety.

Airworthiness Directive
  • Airbus A380841842

EASA AD 2021-0082

Mar 19, 2021

Nacelles / Pylons — Aft Pylon Fairing Rear Drain Pipes Sealing — Modification

EASA Airworthiness Directive 2021-0082 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses a sealing issue around the aft pylon fairing rear drain pipes on engine pylons, specifically for Rolls-Royce and Engine Alliance GP7200 engine pylons. The directive mandates a modification to prevent fluid leakage inside the aft pylon fairing.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2021-0063R1

Mar 15, 2021

Oxygen — Steel Braided Polyurethane Flexible Hoses — Replacement

EASA Airworthiness Directive 2021-0063R1 is an updated safety directive addressing oxygen system components on Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates the replacement of certain steel braided polyurethane flexible hoses (Part Number 32209 series) used in crew and passenger oxygen distribution systems with improved hoses (Part Number 32309 series) to prevent oxygen leakage. This directive applies to all manufacturer serial numbers of the Airbus A380 models listed.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2021-0007

Jan 7, 2021

Nacelles / Pylons — Inboard Pylon Box Dog Head Fitting Holes — Inspection

EASA Airworthiness Directive 2021-0007 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes equipped with Rolls-Royce Trent 900 or Engine Alliance GP7200 engines. The directive mandates inspections of the inboard pylon box Dog Head fitting fastener holes to detect cracks that could compromise structural integrity. It applies to all manufacturer serial numbers of these aircraft models.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2020-0285

Dec 18, 2020

Indicating / Recording Systems — Flight Data Recording System — Modification (Software Update)

EASA Airworthiness Directive 2020-0285 is an official regulatory document addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates a software update to the Flight Data Recording System (FDRS) to correct a software error that could cause partial loss of flight data recording. This directive ensures continued airworthiness and compliance with European aviation safety regulations.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2020-0286

Dec 18, 2020

Pneumatic – Pylon / Wing Interface Bleed Duct and Fuel Pipe – Inspection

EASA Airworthiness Directive 2020-0286 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses inspection requirements for the bleed duct and fuel pipe at the pylon/wing interface to prevent potential fire hazards caused by bracket weld failures. This directive mandates repetitive inspections and corrective actions to ensure continued airworthiness.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2020-0198

Sep 15, 2020

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

EASA Airworthiness Directive 2020-0198 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with updated airworthiness limitations specified in Airbus A380 Airworthiness Limitations Section Part 1 Variation 11.1 to ensure continued safe operation of these aircraft.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2017-0188R1

Jun 16, 2020

Fuselage — Frame 94 Upper Shell — Inspection

EASA Airworthiness Directive 2017-0188R1 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes, excluding MSN 0162 and 0167 and those with Airbus modification 74725 incorporated in production. The directive mandates repetitive inspections of the fuselage frame 94 upper shell to detect and address potential structural damage. It also provides an optional terminating modification to eliminate the need for repetitive inspections.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2020-0089

Apr 17, 2020

Nacelles / Pylons — Inboard Pylon Box at Rib 14 Fasteners — Inspection / Replacement

EASA Airworthiness Directive 2020-0089 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes equipped with Engine Alliance GP7200 or Rolls-Royce Trent 900 engines. The directive addresses inspection and possible replacement of fasteners attaching the lateral panel to Rib 14 at the inboard pylon box for engines #2 and #3. It mandates repetitive inspections to detect cracks that could lead to in-flight detachment of the lateral panel.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2020-0058

Mar 17, 2020

Equipment / Furnishings — Emergency Locator Transmitter Protection — Modification

EASA Airworthiness Directive 2020-0058 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses a safety issue related to the Emergency Locator Transmitter (ELT) protection on these aircraft, specifically targeting ELTs with Part Number 01N65900. The directive mandates a modification to improve protection against potential battery fires caused by current injection.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2018-0043R1

Dec 12, 2019

Power Plant — Rear Engine Mount Assembly — Inspection

EASA Airworthiness Directive 2018-0043R1 is a regulatory document addressing inspection requirements for the rear engine mount assembly on Airbus A380-841 and A380-842 aeroplanes. It mandates inspections of specific rear engine mount beams and assemblies, particularly those with part numbers L7121076120000 and related assemblies, to detect cracks caused by manufacturing defects. The directive ensures continued airworthiness by requiring detailed or high-frequency eddy current inspections and, if necessary, replacement of affected parts.

Airworthiness Directive
  • Airbus A380841842