EASA AD 26-123 — Fuselage – Forward Fuselage Skin Panels – Inspection

Summary

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.

What Changed

This proposed directive supersedes EASA AD 2026-0055R1 and retains its requirements for Group 1 panels while introducing new inspection and mapping requirements for Group 2 and Group 3 panels. It mandates local thickness mapping, general visual inspections, and full panel thickness measurements, along with reporting and corrective actions based on findings. Additionally, it updates restrictions related to the Master Minimum Equipment List (MMEL) and Structural Repair Manual (SRM) tasks.

Why It Matters

This directive is critical for aviation professionals as it addresses a potential unsafe condition that could compromise the structural integrity of affected Airbus aircraft. Operators and maintenance organizations must comply to ensure continued airworthiness and safety. The directive also impacts dispatch conditions and repair procedures, requiring close coordination with Airbus for approved repair instructions and compliance with updated maintenance restrictions.

What To Do

Operators must perform local thickness mapping, visual inspections, and full panel thickness measurements within specified timeframes: Group 1 panels within 6 months after 20 March 2026, Group 2 panels within 6 months after the AD's effective date, and Group 3 panels within 18 months after the AD's effective date. Findings must be reported to Airbus promptly, and any required corrective actions must be completed before further flight. Dispatch restrictions under MMEL items 21-31-01A and 21-31-01B apply until compliance and removal conditions are met.