EASA Regulations for Airbus A321-252NX

6 airworthiness directives and regulations affecting Airbus A321-252NX.

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New ADs and bulletins for Airbus A321-252NX, summarized like the ones below, every Monday.

EASA PAD 26-123

Oct 13, 2026

Fuselage – Forward Fuselage Skin Panels – Inspection

EASA Airworthiness Directive PAD No. 26-123 is a proposed directive addressing inspection requirements for forward fuselage skin panels on Airbus A319, A320, and A321 aircraft models. It applies to specific serial numbers and panel part numbers identified in the directive. The directive focuses on detecting potential structural integrity issues caused by production quality deviations and certain repair conditions affecting the fuselage panels.

Proposed AD
  • Airbus A319153N
  • Airbus A320251N252N271N
  • Airbus A321251NX252NX271NX272NX

EASA AD 2024-0187

Sep 25, 2024

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.

Airworthiness Directive
  • Airbus A321251NX252NX253NX271NX272NX

EASA AD 2024-0057

Feb 28, 2024

Equipment/Furnishings – Escape Slide and Offwing Slide Inflation Reservoir Venting Holes – Inspection / Replacement

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.

Airworthiness DirectiveSuperseded
  • Airbus A321251NX252NX253NX271NX272NX

EASA AD 2024-0048

Feb 16, 2024

Equipment/Furnishings – Escape Slide and Offwing Slide Inflation Reservoir Venting Holes – Inspection / Replacement

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.

Airworthiness DirectiveSuperseded
  • Airbus A321251NX252NX253NX271NX272NX

EASA AD 2022-0176

Aug 24, 2022

Equipment / Furnishings – Escape Slide Inflation Reservoir Regulator Valve Protective Cover – Removal

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.

Airworthiness DirectiveSuperseded
  • Airbus A321251NX252NX253NX271NX272NX

EASA AD 2022-0089

May 17, 2022

Power Plant — Aft Engine Mount Secondary Load Path — Inspection

EASA Airworthiness Directive 2022-0089 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, and A321-253NX aeroplanes. It mandates repetitive detailed inspections of the aft engine mount secondary load path to detect potential failures. The directive aims to prevent engine mount rupture that could lead to engine loss and loss of aircraft control.

Airworthiness Directive
  • Airbus A321251N251NX252N252NX253N253NX