Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1996-05-31 · Effective 1996-06-17 · 61 FR 27253
Document
Document number
96-13496
Federal Register citation
61 FR 27253
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Saab Model SAAB 2000 Series
Publication date
1996-05-31
Effective date
1996-06-17
FAA docket
Docket No. 96-NM-102-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Saab Model SAAB 2000 series airplanes. This action requires inspections to detect cracking of the lower rib of the rudder, and repair, if necessary. This action also provides for an optional terminating action, which, if accomplished, terminates the repetitive inspection requirement. This amendment is prompted by reports of fatigue cracking of the lower rib of the rudder. The actions specified in this AD are intended to prevent such fatigue cracking and subsequent failure of the primary structure of the rudder, which could result in reduced controllability of the airplane.