EASA AD 2022-0030
SUPERSEDED BY EASA AD 2024-0210
Summary
EASA Airworthiness Directive 2022-0030 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates repetitive special detailed inspections of the inner cap and web horizontal flange at frame 68 stringer 22 to detect cracks that could compromise fuselage structural integrity. The directive applies to specific Airbus models except those with certain production modifications or service bulletin embodiments.
What Changed
This directive introduces mandatory repetitive inspections of the affected fuselage area to identify and address cracks reported during previous inspections. It requires compliance with Airbus Service Bulletin A320-53-1491 or approved alternative maintenance instructions. Corrective actions must be taken if discrepancies or cracks are found, but these actions do not terminate the inspection requirements unless otherwise specified.
Why It Matters
This directive is critical for maintaining the structural integrity of affected Airbus aircraft, ensuring continued airworthiness and safety. Operators and maintenance organizations must incorporate these inspections into their maintenance programs to prevent potential fuselage failures. Compliance helps avoid unsafe conditions that could lead to costly repairs or operational disruptions.
What To Do
Operators must perform the initial special detailed inspection before exceeding the specified flight cycle thresholds or within the defined timeframes after the effective date of 2022-03-11. Subsequent inspections must occur at intervals not exceeding 19,700 flight cycles. If cracks or discrepancies are detected, operators must contact Airbus for approved corrective actions and implement them within the specified compliance times. Alternative approved maintenance instructions may be used if applicable.
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