Summary
We are adopting a new airworthiness directive (AD) for the products listed above that supersedes an existing AD. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: * * * * * Engineering analysis using the new calculated loads has shown that the structural integrity of the forward engine mount cannot be guaranteed after either thrust link has accumulated 15500 Flight Cycles (FC). * * * * * A loss of structural integrity of the forward engine mounts could lead to the loss of the load path for the forward engine mount and damage to other engine mount structures, which could result in failure of the forward engine mount, possible separation of the engine from the airplane, damage to the wing, or loss of control of the airplane. This AD requires actions that are intended to address the unsafe condition described in the MCAI.
Directive Details
AD Number
FAA-2010-0476
Document Number
2010-11187
Type
Rule
Publication Date
May 13, 2010
Effective Date
May 28, 2010
Affected Manufacturer
Airbus Model A340-200 and A340-300 Series
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2010-0476
Topics
Official Documents
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