EASA AD 2022-0162R1
Nacelles / Pylons — Thrust Reverser Intermediate Frame Fittings — Replacement
Summary
EASA Airworthiness Directive 2022-0162R1 is a regulatory document addressing the replacement of thrust reverser intermediate frame fittings on Airbus A380-841 and A380-842 aeroplanes. It specifically targets affected parts installed on engines #2 and #3 due to reported cracks that could lead to in-flight detachment of the thrust reverser external panel. The directive mandates replacement of these fittings with redesigned titanium parts to ensure continued airworthiness.
What Changed
This revision of EASA AD 2022-0162 clarifies that the affected thrust reverser intermediate frame fittings are only installed on engines #2 and #3 of the Airbus A380. It updates the original directive by specifying the scope of affected parts and reinforces the replacement requirements with new titanium fittings as per Airbus Service Bulletin A380-54-8094.
Why It Matters
This directive is critical for aviation professionals because cracked thrust reverser fittings pose a safety risk that could result in damage to the tail and reduced aircraft control. Operators and maintenance organizations must comply to prevent potential in-flight detachment of components, ensuring the structural integrity and safe operation of the Airbus A380 fleet. Compliance with this AD is mandatory under European regulations, affecting maintenance planning and parts inventory.
What To Do
Operators of Airbus A380-841 and A380-842 aeroplanes must replace the affected thrust reverser intermediate frame fittings on engines #2 and #3 before exceeding 9,000 flight cycles since the aircraft's date of manufacture or within 72 months after 19 August 2022, whichever occurs first. After replacement, installation of any affected parts on the modified aeroplanes is prohibited. Compliance should follow the instructions in Airbus Service Bulletin A380-54-8094.
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