airworthiness · Rule · Final rule. · Published 2018-10-24 · Effective 2018-11-28 · 83 FR 53563
Document
Document number
2018-23031
Federal Register citation
83 FR 53563
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2018-10-24
Effective date
2018-11-28
FAA docket
Docket No. FAA-2018-0160
Abstract
We are superseding Airworthiness Directive (AD) 2016-24-03, which applied to certain Bombardier, Inc., Model DHC-8-400 series airplanes. AD 2016-24-03 required repetitive detailed inspections of barrel nuts and cradles, a check of the bolt torque of the preload indicating (PLI) washers, and corrective actions if necessary. This AD retains the requirements of AD 2016-24-03 and requires modifying the airplane by installing a sealing disk to a certain location and replacing certain barrel nuts. This AD was prompted by reports of cracked and corroded barrel nuts found at the mid-spar location of the horizontal-stabilizer-to-vertical-stabilizer attachment joint, and the issuance of new service information that includes a terminal modification. We are issuing this AD to address the unsafe condition on these products.