EASA Regulations for Airbus A321-271NX

6 airworthiness directives and regulations affecting Airbus A321-271NX.

EASA AD 2024-0187

Doors — Overwing Exit Door Latch Bracket Bushes — Inspection

EASA Airworthiness Directive 2024-0187 is an airworthiness directive addressing inspection requirements for the overwing exit door latch bracket bushes on Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. The directive mandates repetitive detailed inspections and corrective modifications to prevent potential structural integrity issues caused by bush migration on the latch shaft of the emergency overwing exit door. It applies to specific bracket assembly latch and door assembly overwing part numbers identified by Airbus.

Sep 25, 2024

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321Airbus A321-251NXAirbus A321-252NXAirbus A321-253NXAirbus A321-271NXAirbus A321-272NX

EASA AD 2024-0057

SUPERSEDED BY EASA AD 2025-0151

EASA Airworthiness Directive 2024-0057 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. It addresses inspection and replacement requirements for escape slide and offwing slide inflation reservoir venting holes orifice fittings with specific part numbers. The directive ensures continued airworthiness by mandating inspections and corrective actions for affected parts to prevent potential in-flight deployment failures.

Feb 28, 2024

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321Airbus A321-251NXAirbus A321-252NXAirbus A321-253NXAirbus A321-271NXAirbus A321-272NX

EASA AD 2024-0048

SUPERSEDED BY EASA AD 2024-0057

EASA Airworthiness Directive 2024-0048 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. It addresses a potential unsafe condition related to the escape slide and offwing slide inflation reservoir venting holes, specifically concerning certain orifice fittings installed on these reservoirs. The directive mandates inspection and possible replacement of affected parts to ensure continued airworthiness.

Feb 16, 2024

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321Airbus A321-251NXAirbus A321-252NXAirbus A321-253NXAirbus A321-271NXAirbus A321-272NX

EASA AD 2022-0176

SUPERSEDED BY EASA AD 2025-0151

EASA Airworthiness Directive 2022-0176 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. It addresses a safety issue related to the escape slide inflation reservoir regulator valve protective cover that may cause uncommanded door 3 escape slide release during flight. The directive mandates modification of affected parts to prevent deployment of a non-inflated escape slide.

Aug 24, 2022

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321Airbus A321-251NXAirbus A321-252NXAirbus A321-253NXAirbus A321-271NXAirbus A321-272NX

EASA AD 2020-0053

Nacelles / Pylons — Engine Pylon Nose Fire Seals — Inspection / Replacement

EASA Airworthiness Directive 2020-0053 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A320-271N, A321-271N, A321-271NX, and A321-272N aeroplanes. It addresses inspection and replacement requirements for engine pylon nose fire seals with Part Number D0003109300000 to ensure firewall integrity. The directive mandates a detailed inspection and corrective actions to prevent potential loss of fire protection in case of an engine fire.

Mar 10, 2020

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320Airbus A321Airbus A320-271NAirbus A321-271NAirbus A321-271NXAirbus A321-272N

EASA AD 2018-0110

Engine — Modification

EASA Airworthiness Directive 2018-0110 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A320-271N, A321-271N, A321-272N, A321-271NX, and A321-272NX aeroplanes. It addresses a software issue in the Full Authority Digital Engine Control Electronic Engine Controllers (FADEC EEC) that could prevent engine restart under certain conditions. The directive mandates modification of affected FADEC EECs to software standard FCS4.4 to ensure safe engine restart capability.

May 18, 2018

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320Airbus A321Airbus A320-271NAirbus A321-271NAirbus A321-272NAirbus A321-271NXAirbus A321-272NX