Airworthiness Directives; Schempp-Hirth K.G. Model Cirrus Sailplanes
airworthiness · Rule · Final rule. · Published 1998-08-27 · Effective 1998-10-12 · 63 FR 45681
Document
Document number
98-22825
Federal Register citation
63 FR 45681
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1998-08-27
Effective date
1998-10-12
FAA docket
Docket No. 98-CE-51-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to certain Schempp-Hirth K.G. (Schemmp-Hirth) Model Cirrus sailplanes. This AD requires modifying or replacing the connecting rod between the airbrake bellcranks, and replacing the existing 6 millimeter (mm) bolt with an 8 mm bolt. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent the threaded bolt that is welded to the connecting rod between the airbrake bellcranks from breaking, which could result in loss of airbrake control with a possible reduction/loss of sailplane control.