EASA Regulations for Airbus A321-251N

3 airworthiness directives and regulations affecting Airbus A321-251N.

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New ADs and bulletins for Airbus A321-251N, summarized like the ones below, every Monday.

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

EASA AD 2019-0094

Apr 26, 2019

Pneumatic — Bleed Monitoring Computer — Modification / Replacement

EASA Airworthiness Directive 2019-0094 is an airworthiness directive affecting Airbus A320-251N, A320-271N, A321-251N, A321-253N, A321-271N, and A321-272N aeroplanes. It addresses issues with the Bleed Monitoring Computer (BMC) software that regulate pneumatic bleed temperature on these aircraft models. The directive mandates modification or replacement of affected BMC software to ensure safe operation.

Airworthiness Directive

Airbus A320251N271N
Airbus A321251N253N271N272N

EASA AD 2019-0081

Apr 3, 2019

Fire Protection — Pipe Connections — Re-torque

EASA Airworthiness Directive 2019-0081 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A320-251N, A320-271N, A321-251N, A321-253N, A321-271N, and A321-272N aeroplanes. The directive addresses fire protection pipe connections in the pylon area that may have been under-torqued during final assembly. It mandates re-torqueing these connections to ensure proper safety margins in case of engine fire.

Airworthiness Directive

Airbus A320251N271N
Airbus A321251N253N271N272N