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Airworthiness directives › 2015-22-10

AD 2015-22-10 Airworthiness Directives; Airbus Airplanes

2015-12-15
2015-11-10
39-18315
FAA-2014-0574
Airframe
—

Models named: A318-111, -112, -121, -122, A319-111, -113, -114, -115, -131, -132. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to the Airbus airplanes specified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes. (4) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Within 24 months after the effective date of this AD: Inspect the airplane maintenance records to determine if the rudder composite side shell panel has been repaired since first installation of the rudder on an airplane.

Unsafe condition

This AD was prompted by a report of skin disbonding on a composite side shell panel of a rudder. We are issuing this AD to detect and correct skin disbonding on the rudder, which could affect the structural integrity of the rudder, possibly resulting in reduced control of the airplane.

Affected ADs

None.

Read the original on the Federal Register →

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1