← FAA Federal Register actions

Airworthiness Directives; Airbus Airplanes

airworthiness · Rule · Final rule. · Published 2016-08-19 · Effective 2016-09-23 · 81 FR 55358

Document

Document number
2016-19486
Federal Register citation
81 FR 55358
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2016-08-19
Effective date
2016-09-23
FAA docket
Docket No. FAA-2016-4226

Abstract

We are superseding Airworthiness Directive (AD) 2003-25-07 for certain Airbus Model A319 and A320 series airplanes, and AD 2005-13-39 for certain Airbus Model A321 series airplanes. AD 2003-25-07 required a revision to the airplane flight manual (AFM) and replacement of both elevator aileron computers (ELACs) having L80 standards with new ELACs having L81 standards. AD 2005-13-39 required a revision to the AFM, replacement of existing ELACs with ELACs having L83 or L91 standards, as applicable; and a concurrent action. Since we issued AD 2003-25-07 and AD 2005-13-39, we have determined that new ELAC standards must be incorporated. The ELAC standards have been upgraded to version L97+, which implements enhanced angle-of-attack (AOA) monitoring to better detect AOA blockage, including multiple AOA blockages. This AD requires replacing existing ELACs with new ELACs having L97+ standards or revising the software in an existing ELAC to the L97+ standards, as applicable, which terminates the requirements of AD 2003-25-07 and AD 2005-13-39. This AD also expands the applicability to include all Airbus Model A318, A319, A320, and A321 series airplanes. We are issuing this AD to prevent inadvertent activation of the AOA protections. Inadvertent activation of the AOA protections could result in a continuous nose-down pitch rate that could result in reduced controllability of the airplane.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown