Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Series Airplanes
airworthiness · Rule · Final rule. · Published 1999-10-06 · Effective 1999-11-10 · 64 FR 54199
Document
Document number
99-25768
Federal Register citation
64 FR 54199
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1999-10-06
Effective date
1999-11-10
FAA docket
Docket No. 98-NM-321-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, -106, - 201, -202, -301, -311, and -315 series airplanes, that currently requires a one-time inspection to detect chafing of electrical wires in the cable trough below the cabin floor; repair, if necessary; installation of additional tie-mounts and tie-wraps; and application of sealant to rivet heads. This amendment requires the accomplishment of these same actions on additional airplanes. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent chafing of electrical wires, which could result in an uncommanded shutdown of an engine during flight.