Flight Controls – Rudder Pedal Control System – Modification
Superseded. Comply with 2019-0221, which replaces this document.
- Published
- Effective
- Deadline
- Replaces
- 2017-0036
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must inspect the rudder pedal support box and shaft within three months or at the next scheduled A check, whichever comes first, and then every 150 flight hours. If discrepancies are found, approved repair instructions must be obtained and implemented before further flight. Installation of affected parts is only allowed if they are new or have passed inspection per the Airbus Defence & Space AOT instructions.
Summary
EASA Airworthiness Directive 2018-0051 is an airworthiness directive issued by the European Aviation Safety Agency affecting EADS-CASA C-212 aeroplanes, specifically models C-212-CB, CC, CD, CE, DD, DF, and EE. The directive addresses issues with the rudder pedal control system, particularly the rudder pedal support box and shaft parts. It mandates repetitive inspections and corrective actions to ensure continued safe operation of the affected aircraft.
What changed
This directive supersedes EASA AD 2017-0036 and replaces the previously required modification with repetitive inspections of the rudder pedal adjustment system. It introduces improved inspection instructions due to difficulties encountered during the earlier mandated modification and requires operators to inspect affected parts every 150 flight hours or within three months of the effective date.
Why it matters
This directive is critical for aviation professionals as it addresses a potential failure in the rudder control system that could reduce aircraft control. Operators and maintenance teams must comply to prevent unsafe conditions and ensure regulatory compliance. The interim nature of this AD means further actions may follow, requiring ongoing attention from compliance teams.
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