Browse 252 EASA regulations with AI-powered summaries.
EASA AD 2022-0026
Feb 16, 2022EASA Airworthiness Directive 2023-0029 addresses safety concerns related to Airbus S.A.S. aircraft models A319, A320, and A321. This directive provides updated regulatory requirements to ensure continued airworthiness and operational safety of these aircraft types. It supersedes previous directives to incorporate the latest findings and corrective actions.
EASA AD 2022-0007
Jan 19, 2022EASA Airworthiness Directive 2022-0007 is an airworthiness directive addressing the LEAP-1A series engines manufactured by CFM International, installed on Airbus A319, A320, and A321 aircraft. It mandates compliance with updated airworthiness limitations and maintenance checks as specified in the LEAP-1A Engine Shop Manual Chapter 05 and related service bulletins. The directive applies to various LEAP-1A engine models and specific life-limited parts identified by part and serial numbers.
EASA AD 2021-0279
Dec 15, 2021The document titled Equipment / Furnishings — Doghouse Placard — Installation is a regulatory communication concerning the installation of doghouse placards on Airbus S.A.S. aircraft models A318, A319, A320, and A321. It addresses specific equipment and furnishing requirements related to these aircraft types. The document provides guidance on proper placard installation to ensure compliance with safety and operational standards.
EASA AD 2021-0256
Nov 16, 2021EASA Airworthiness Directive 2021-0256 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes. It addresses potential fatigue cracking in the bottom wing skin panel 2 around the wing manhole access panels on aircraft equipped with Sharklets. The directive mandates repetitive detailed visual inspections to detect and correct any cracks to maintain structural integrity.
EASA AD 2021-0242
Nov 8, 2021The document titled 'Fuselage — Door Stop Fitting Holes at Frame 66/68 — Inspection / Repair' is an AIRBUS S.A.S. type designation applicable to the A318, A319, A320, and A321 aircraft models. It addresses inspection and repair requirements related to the door stop fitting holes located at fuselage frames 66 and 68. The document provides guidance to ensure structural integrity and safety of the affected aircraft components.
EASA AD 2021-0241
Nov 8, 2021EASA Airworthiness Directive 2021-0241 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses the inspection and maintenance of the wing front spar vertical stringers to detect and prevent cracks that could compromise the structural integrity of the aircraft. This directive applies to various Airbus models except those modified with specific structural reinforcements related to sharklet installations.
EASA AD 2021-0229
Nov 5, 2021EASA Airworthiness Directive 2021-0229 is an airworthiness directive addressing Airbus A318, A319, A320, and A321 aeroplanes. It focuses on the identification, inspection, and replacement of outer flaps and tabs that may have been improperly heat-treated or manufactured from the wrong material. The directive mandates inspections and corrective actions to ensure the structural integrity of these flap components.
EASA AD 2021-0236
Oct 29, 2021EASA Airworthiness Directive 2021-0236 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses potential structural failures in Nose Landing Gear (NLG) and Main Landing Gear (MLG) sliding tubes due to overheat damage and improper repairs. The directive mandates inspections and replacement of affected landing gear sliding tubes to ensure continued airworthiness.
EASA AD 2021-0228
Oct 12, 2021EASA Airworthiness Directive 2021-0228 mandates repetitive inspections of the centre and outer wing box lower panels and stiffeners at the Rib 1 junction on Airbus A318, A319, A320, and A321 aircraft. This directive addresses potential structural integrity issues caused by non-compliant taperlok fasteners in the wing-to-fuselage junction. The inspections include both internal and external special detailed inspections as specified in Airbus Service Bulletins.
EASA AD 2021-0227
Oct 11, 2021EASA Airworthiness Directive 2021-0227 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses the detection of cracks in the double joggle areas at fuselage frames 16 and 20, which could compromise structural integrity. The directive mandates repetitive special detailed inspections and provides optional modification instructions to reinforce the affected areas.
EASA AD 2015-0036R4
Oct 8, 2021EASA Airworthiness Directive 2015-0036R4 is an updated regulatory requirement addressing inspection and repair of fuselage external skin repairs on Airbus A318, A319, A320, and A321 aircraft. It mandates ultrasonic, eddy current, or visual inspections of specific fuselage skin doubler installations to detect cracks that could compromise structural integrity. The directive applies to all manufacturer serial numbers of these Airbus models and references updated Structural Repair Manuals and Airbus Alert Operators Transmission A53N007-14.
EASA AD 2021-0183R1
Sep 20, 2021EASA Airworthiness Directive 2021-0183R1 is an updated safety directive addressing inspection requirements for forward-facing galleys installed on Airbus A318, A319, A320, and A321 aircraft. The directive mandates repetitive general visual inspections of specified galley parts to detect damage such as delamination and corrosion that could compromise trolley retention during emergency landings. It applies to all manufacturer serial numbers of the affected Airbus models and references specific Airbus Service Bulletins for inspection procedures.
EASA AD 2020-0085R1
Aug 6, 2021EASA Airworthiness Directive 2020-0085R1 is a regulatory update addressing the replacement and inspection of aft engine mount retainers on Airbus A318, A319, A320, and A321 aircraft equipped with CFM56-5A/5B engines. The directive focuses on preventing in-flight loss of aft engine mount links due to cracked or broken retainers caused by vibration and surface finish issues. It applies to specific part numbers of aft engine mount assemblies and includes instructions for inspections, replacements, and modifications.
EASA AD 2021-0111R1
Aug 5, 2021EASA Airworthiness Directive 2021-0111R1 is a regulatory update addressing inspection requirements for windshields installed on Airbus A318, A319, A320, and A321 aeroplanes. It mandates detailed and electrical test inspections of specific affected windshield parts to ensure structural integrity and prevent in-flight windshield failure. The directive applies to all serial numbers of the listed Airbus models and specifies affected part numbers grouped by risk level.
EASA AD 2017-0132R2
Aug 3, 2021EASA Airworthiness Directive 2017-0132R2 is an updated regulatory requirement addressing the replacement of forward engine mount main beam snouts on Airbus A318, A319, A320, and A321 aircraft equipped with CFM56-5A and CFM56-5B engines. The directive targets specific part numbers 642-2006-501 and 642-2006-503 of the forward engine mount main beam assemblies due to potential wear issues that could lead to engine detachment. It mandates inspections and replacement actions to ensure continued airworthiness and safety.
EASA AD 2021-0175
Jul 23, 2021EASA Airworthiness Directive 2021-0175 is a corrective AD addressing inspection requirements for main landing gear sliding tubes on Airbus A318, A319, A320, and A321 aircraft. It mandates repetitive general visual inspections of affected landing gear sliding tubes identified in three batches, with specific part and serial numbers, to detect cracks caused by improper magnetic particle inspections during overhaul. The AD applies to all manufacturer serial numbers of the specified Airbus models and includes instructions for corrective actions and terminating actions.
EASA AD 2021-0172
Jul 20, 2021EASA Airworthiness Directive 2022-0120 addresses safety requirements for Airbus S.A.S. aircraft models A318, A319, A320, and A321. This directive supersedes previous related directives to update and consolidate airworthiness instructions for these aircraft types. It ensures continued operational safety and regulatory compliance for operators of these Airbus models.
EASA AD 2021-0167
Jul 14, 2021EASA Airworthiness Directive 2021-0167 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspection and modification of the stringer attachments at wing ribs 2 to 7 to address potential structural integrity issues. The directive applies to various serial numbers and configurations except those already modified by specific Airbus modifications or service bulletins.
EASA AD 2021-0115R1
Jul 5, 2021EASA Airworthiness Directive 2021-0115R1 is a regulatory document addressing a safety issue with fuel pumps, Part Number P99C38-605, installed on Airbus A318, A319, A320, and A321 aircraft. The directive mandates the replacement of affected fuel pumps due to a potential manufacturing defect that could lead to an ignition source in the fuel tank. This AD applies to all manufacturer serial numbers of the specified aircraft models.
EASA AD 2021-0150
Jun 25, 2021EASA Airworthiness Directive 2021-0150 is an interim safety directive affecting Airbus A319, A320, and A321 neo family aircraft. It addresses potential unreliable airspeed indications during take-off caused by erroneous pitot probe data, which could lead to unstable flight paths and reduced aircraft control. The directive mandates updates to the Airplane Flight Manual and Master Minimum Equipment List to mitigate this risk.