Stabilizers — Elevator Hinge Fittings — Inspection
- Published
- Effective
- Deadline
- Replaces
- 2016-0075
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators of affected CN-235 aeroplanes must perform initial inspections of elevator hinge fittings before exceeding 600 flight hours or within 300 flight hours after 3 May 2016, whichever is later. Repetitive inspections must continue until the optional terminating modification is accomplished per the specified service bulletin. Any discrepancies found during inspections require immediate corrective actions before further flight.
Summary
EASA Airworthiness Directive 2016-0075R1 is a regulatory document addressing inspection requirements for elevator hinge fittings on Airbus Defence & Space CN-235 aeroplanes, including CN-235-100, CN-235-200, and CN-235-300 models. The directive mandates inspections to detect excessive play, misalignment, and cracking in stabilizer elevator hinge fittings to ensure continued airworthiness and flight safety.
What changed
This revision introduces an optional terminating action through modification in accordance with Airbus Defence & Space Service Bulletin SB-235-55-0014C, which allows operators to end repetitive inspections. Additionally, the directive removes C-295 aeroplanes from its applicability and updates the document to comply with the latest AD writing standards.
Why it matters
This directive is critical for aviation professionals as it addresses a potentially unsafe condition that could lead to structural failure and reduced aircraft control. Operators and maintenance organizations must comply to prevent elevator hinge fitting failures, ensuring aircraft safety and regulatory compliance. The revision provides clarity on terminating actions, reducing inspection burdens once modifications are applied.
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