Fuselage — Structural Parts / Joints — Modification / Reinforcement
- Published
- Effective
- Deadline
- Replaces
- 2016-0208
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators must perform the required structural modifications before exceeding specified Structural Modification Points, following the instructions in the applicable Airbus Service Bulletins. For aircraft already modified, additional work must be completed within 12 months after 18 November 2016. The alternative method for Action 5 can be used if compliance times are met. Stakeholders should consult the referenced Service Bulletins and coordinate with EASA or Airbus for any alternative compliance methods.
Summary
EASA Airworthiness Directive 2016-0208R1 is a regulatory update addressing structural modifications and reinforcements for Airbus A340 series aeroplanes, including models A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643. The directive mandates modifications to fuselage structural parts and joints to prevent widespread fatigue damage that could compromise aircraft integrity and safety.
What changed
This revision introduces an alternative modification method for Action 5 through Airbus Service Bulletin A340-53-4237 and removes the requirements for Actions 1 and 7 based on recent data. It also clarifies the applicability of certain actions and updates editorial content to align with current AD writing standards without altering technical requirements.
Why it matters
This directive is critical for maintaining the structural integrity and safety of affected Airbus A340 aircraft by preventing fatigue-related damage that could lead to rapid depressurisation. Operators, maintenance organizations, and compliance teams must ensure timely implementation of the specified modifications to meet regulatory requirements and uphold continuing airworthiness.
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