Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes
airworthiness · Rule · Final rule. · Published 2004-07-09 · Effective 2004-08-13 · 69 FR 41405
Document
Document number
04-15377
Federal Register citation
69 FR 41405
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Saab Model SAAB 2000 Series
Publication date
2004-07-09
Effective date
2004-08-13
FAA docket
Docket No. 2001-NM-316-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain Saab Model SAAB 2000 series airplanes, that currently requires repetitive inspections for discrepancies of the upper and lower areas of the backup struts in the left and right nacelles; and corrective actions, if necessary. This amendment requires repetitive inspections for cracks in the lower areas of the backup struts, and corrective actions if necessary. This action also requires the eventual replacement of the backup struts with new, improved struts, which terminates the repetitive inspections. The actions specified by this AD are intended to prevent failure of the backup struts in the left and right nacelles due to fatigue cracking, which could result in loss of fail-safe redundancy in the design of the nacelle in terms of load capability, and consequent separation of the engine from the airplane and subsequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.