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Airworthiness Directives; Airbus Airplanes

airworthiness · Rule · Final rule. · Published 2016-07-12 · Effective 2016-08-16 · 81 FR 44989

Document

Document number
2016-16212
Federal Register citation
81 FR 44989
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2016-07-12
Effective date
2016-08-16
FAA docket
Docket No. FAA-2015-3632

Abstract

We are superseding Airworthiness Directive (AD) 2014-14-06 for all Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, - 113, -114, and -115 airplanes; Model A320-111, -211, -212, and -214 airplanes; and Model A321-111, -112, -211, -212, and -213 airplanes. AD 2014-14-06 required inspecting the aft engine mount retainers for surface finish, cracks, and failure, and replacement if necessary. This new AD requires repetitive inspections for damaged, cracked, broken, and missing aft engine mount retainers, and replacement if necessary. This AD was prompted by inspection results that have shown that the main cause of crack initiation in the aft engine mount retainers is the vibration dynamic effect that affects both retainers, either with "dull" or "bright" surface finishes. We are issuing this AD to detect and correct failure of retainer brackets of the aft engine mount and consequent loss of the locking feature of the nuts of the inner and outer pins; loss of the pins will result in the aft mount engine link no longer being secured to the aft engine mount.

Source

Authoritative
Federal Register document
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