airworthiness · Rule · Final rule. · Published 1999-01-28 · Effective 1999-03-12 · 64 FR 4290
Document
Document number
99-1827
Federal Register citation
64 FR 4290
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1999-01-28
Effective date
1999-03-12
FAA docket
Docket No. 98-CE-52-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to certain Schempp-Hirth K.G. (Schempp-Hirth) Models Standard- Cirrus, Nimbus-2, JANUS, and Mini-Nimbus HS-7 sailplanes. This AD requires installing a safety device for the tailplane locking hook. 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 locking hook on the tailplane attachment bracket from disengaging, which could result in the horizontal tailplane coming loose from the fin with possible loss of longitudinal control of the sailplane.