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Airworthiness Directives; Airbus Airplanes

airworthiness · Rule · Final rule. · Published 2017-06-29 · Effective 2017-08-03 · 82 FR 29363

Document

Document number
2017-13407
Federal Register citation
82 FR 29363
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2017-06-29
Effective date
2017-08-03
FAA docket
Docket No. FAA-2016-9573

Abstract

We are superseding Airworthiness Directive (AD) 2015-23-13, for all Airbus Model A318 and A319 series airplanes, Model A320-211, - 212, -214, -231, -232, and -233 airplanes, and Model A321-111, -112, - 131, -211, -212, -213, -231, and -232 airplanes. AD 2015-23-13 required modification of the pin programming of the flight warning computer (FWC) to activate the stop rudder input warning (SRIW) logic; and an inspection to determine the part numbers of the FWC and the flight augmentation computer (FAC), and replacement of the FWC and FAC if necessary. This new AD, for certain airplanes, also requires accomplishment of additional modification instructions to install the minimum FWC and FAC configuration compatible with SRIW activation. This AD was prompted by a determination that, in specific flight conditions, the allowable load limits on the vertical tail plane could be reached and possibly exceeded. We are issuing this AD to address the unsafe condition on these products.

Source

Authoritative
Federal Register document
Machine
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