Exhaust — Thrust Reverser Cascades and Aft Frame Attachment — Inspection / Modification
- Published
- Effective
- Deadline
- Replaces
- 2019-0229
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must modify the affected thrust reversers and aft frame junctions within 40 months of the directive's effective date and perform detailed inspections after modification but within the same timeframe. Any discrepancies found during inspections require immediate corrective action before further flight. Installation of affected parts is restricted after compliance deadlines unless they have passed inspection or modification requirements.
Summary
EASA Airworthiness Directive 2019-0229R1 is an updated regulatory requirement addressing inspection and modification of the thrust reverser cascades and aft frame attachments on Airbus A380-861 aeroplanes equipped with GP7200 engines. It mandates detailed inspections and modifications of specific thrust reverser parts identified by part and serial numbers to prevent potential part failure and detachment. The directive references Airbus and SAFRAN Nacelles service bulletins for compliance procedures.
What changed
This revision of EASA AD 2019-0229 corrects the sequence and compliance times for inspection and modification tasks, ensuring that inspections are not performed before the required modifications. It updates the compliance timeline and clarifies installation restrictions for affected thrust reverser components after the specified deadlines.
Why it matters
This directive is critical for aviation professionals because it addresses a safety risk involving possible fractures and detachment of thrust reverser components, which could create runway hazards. Operators and maintenance organizations must comply to ensure continued airworthiness and prevent in-service failures that could lead to operational disruptions or accidents.
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