Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Airplanes
airworthiness · Rule · Final rule. · Published 2006-09-06 · Effective 2006-10-11 · 71 FR 52421
Document
Document number
E6-14623
Federal Register citation
71 FR 52421
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2006-09-06
Effective date
2006-10-11
FAA docket
Docket No. FAA-2006-24199
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A318, A319, A320, and A321 airplanes. This AD requires revising the Limitations section of the airplane flight manual (AFM); performing a one-time hardness test of certain ribs of the left- and right-hand engine pylons, as applicable, which would terminate the AFM limitations; and performing related corrective actions if necessary. This AD results from a report that certain stainless steel ribs installed in the engine pylon may not have been heat-treated during manufacture, which could result in significantly reduced structural integrity of the pylon. We are issuing this AD to detect and correct reduced structural integrity of the engine pylon, which could lead to separation of the engine from the airplane.