EASA AD 2020-0222: Fuselage — Door Frame Drill Starts — Inspection

What to do

Operators of affected Airbus A321-211, A321-231, and A321-232 aeroplanes must perform a detailed visual inspection of specified door frame parts before exceeding 15,000 flight cycles since first flight. If damage is found, corrective actions must be taken as per Airbus Service Bulletin A320-53-1473. Additionally, inspection results must be reported to Airbus within 90 days after inspection completion.

Summary

EASA Airworthiness Directive 2020-0222 is an airworthiness directive addressing certain Airbus A321-211, A321-231, and A321-232 aeroplanes with specific manufacturer serial numbers. It mandates inspection of left-hand and right-hand side door frames with designated part numbers for potential drill start defects near latch hook mounting holes. The directive aims to ensure structural integrity by requiring a one-time detailed visual inspection and corrective actions if damage is found.

What changed

EASA Airworthiness Directive 2020-0222 introduces a new mandatory inspection requirement for specific door frame parts on Airbus A321 aircraft due to potential manufacturing defects causing unintended drill starts. It requires operators to perform a detailed visual inspection before 15,000 flight cycles and to report findings to Airbus. This directive does not supersede any previous ADs.

Why it matters

This directive is critical for maintaining the structural integrity of affected Airbus A321 aircraft by identifying and correcting potential damage caused by manufacturing errors. Operators, maintenance organizations, and compliance teams must ensure timely inspections and repairs to prevent possible safety risks. Compliance with this AD is mandatory to continue lawful operation of the affected aircraft.

What to do

Summary

What changed

Why it matters

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