Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Series Airplanes
airworthiness · Rule · Final rule. · Published 2004-02-10 · Effective 2004-03-16 · 69 FR 6139
Document
Document number
04-2583
Federal Register citation
69 FR 6139
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-02-10
Effective date
2004-03-16
FAA docket
Docket No. 2003-NM-154-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, -106, -201, - 202, -301, -311, and -315 series airplanes, that requires repetitive inspections for discrepancies of certain rear spar fittings between the flex shaft of the flap secondary drive and the wing-to-fuselage structure, and corrective action if necessary. This action also provides for an optional modification of the flex shaft installation, which terminates the repetitive inspections. This action is necessary to find and fix damage and prevent subsequent failure of the rear spar fittings, which could result in loss of the wing. This action is intended to address the identified unsafe condition.