EASA AD 2020-0008: Flight Controls — Flap Control System / Bellcrank Assembly — Inspection / Modification | RegNotify

Airworthiness DirectiveEASA AD 2020-0008

Flight Controls — Flap Control System / Bellcrank Assembly — Inspection / Modification

Published: Jan 20, 2020
Effective: Feb 3, 2020

Diamond Aircraft Industries DA 42

AI-generated summary of the official EASA document. Verify against the PDF before acting.

What to do

Operators and maintenance teams of the Diamond DA 42 must perform the specified inspections and modifications on the flap control system's bellcrank assembly as outlined in the document. They should follow the detailed procedures to ensure compliance and maintain safety standards. No explicit compliance deadline is provided.

Summary

The document titled Flight Controls — Flap Control System / Bellcrank Assembly — Inspection / Modification is a directive concerning the Diamond Aircraft Industries DA 42. It addresses inspection and modification requirements for the flap control system's bellcrank assembly to ensure continued airworthiness and safety of the affected aircraft.

What changed

This directive introduces mandatory inspection and modification procedures for the flap control system's bellcrank assembly on the Diamond DA 42. It specifies the inspection criteria and modification steps necessary to address potential issues identified in the flap control mechanism.

Why it matters

This directive is important for aviation professionals because it helps prevent flap control system failures that could compromise flight safety. Operators and maintenance organizations must comply to maintain aircraft airworthiness and avoid operational disruptions.

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