EASA AD 2020-0205
SUPERSEDED BY EASA AD 2021-0281
Summary
EASA Airworthiness Directive 2020-0205 is an airworthiness directive issued for Airbus A330 series aeroplanes, including models A330-201 through A330-343. It addresses a risk of engine bleed system over-temperature where the engine bleed valve may fail to close, potentially causing damage to the bleed manifold and surrounding structures. The directive mandates amendments to the Aircraft Flight Manual (AFM) to incorporate specific temporary revisions for operational procedures in case of such faults.
What Changed
EASA Airworthiness Directive 2020-0205 requires operators of affected Airbus A330 aircraft to amend their AFM by incorporating one of three specified temporary revisions depending on the installed Flight Warning Computer software standard. This amendment provides procedures to manage engine bleed system over-temperature events. The directive also allows removal of these AFM revisions once a certain Flight Warning Computer software standard (T9-0 or later) is installed.
Why It Matters
This directive is critical for aviation professionals to prevent potential structural damage caused by engine bleed system over-temperature that could compromise aircraft safety. Operators and maintenance teams must ensure compliance to maintain airworthiness and avoid unsafe conditions. It also impacts flight crews who need to be informed and trained on the updated AFM procedures to handle bleed air faults effectively.
What To Do
Operators of Airbus A330 aircraft must amend the applicable AFM within 30 days of 1 October 2020 by incorporating the relevant temporary revision and inform all flight crews. After installing Flight Warning Computer software T9-0 standard or later, the AFM temporary revision procedures can be removed. Compliance with these actions is mandatory to continue operating the affected aircraft legally.
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