EASA AD 2026-0144R1 — Stabilizers – Rudder Outer Skin – Inspection

Summary

EASA Airworthiness Directive 2026-0144R1 is an updated regulatory document addressing inspection requirements for the rudder outer skin on certain Airbus A320 and A321 aircraft models. It applies specifically to Airbus A320-251N, A320-252N, A321-252NX, and A320-271N aeroplanes with specified manufacturer serial numbers. The directive mandates inspections to detect dents caused by storage trolleys that could lead to structural damage and reduced control of the rudder panels.

What Changed

This revision clarifies the compliance time for corrective actions required after inspection of the rudder outer skin. It updates the original AD 2026-0144 issued on 21 July 2026 by specifying deadlines and procedures for corrective measures when discrepancies are found during inspections. The revised AD also provides clearer instructions on reporting requirements and part replacement conditions.

Why It Matters

This directive is critical for aviation professionals to ensure the structural integrity and safe operation of affected Airbus A320 and A321 aircraft. Operators and maintenance organizations must comply to prevent potential rudder damage that could compromise flight control. Timely inspections and corrective actions help maintain continuing airworthiness and regulatory compliance, reducing safety risks and operational disruptions.

What To Do

Operators must determine the rudder serial number within 15 days after 28 July 2026 and perform detailed visual and woodpecker inspections before exceeding 2,000 flight cycles or 12 months from the aeroplane reference date, whichever occurs first. If discrepancies are found, corrective actions must be completed within the time specified in the Airbus Service Bulletin A320-55-1070. Additionally, affected rudder parts can only be replaced after inspection and any necessary corrections. Reporting of rudder serial numbers and inspection results to Airbus is mandatory within specified timeframes.