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Airworthiness Directives; Schempp-Hirth K.G. Models Nimbus-2B, Mini-Nimbus B, Discus a, and Discus b Sailplanes

airworthiness · Rule · Final rule; correction. · Published 1998-04-07 · Effective 1998-04-17 · 63 FR 16883

Document

Document number
98-8582
Federal Register citation
63 FR 16883
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Publication date
1998-04-07
Effective date
1998-04-17
FAA docket
Docket No. 96-CE-19-AD

Abstract

This document clarifies information in an existing airworthiness directive (AD) that applies to certain Schempp-Hirth K.G. (Schempp-Hirth) Models Standard-Cirrus, Nimbus-2, Nimbus-2B, Mini- Nimbus HS-7, Mini-Nimbus B, Discus a, and Discus b sailplanes. That AD currently requires accomplishing a load test of the elevator control system, and replacing the elevator vertical actuating tube either immediately or at a certain time period depending on the results of the load test. The actions specified in that AD are intended to prevent corrosion in the elevator caused by water entering the elevator control rod, which could result in elevator failure and consequent loss of control of the sailplane. The Schempp-Hirth Models Nimbus 2, Mini- Nimbus HS-7, and Standard Cirrus sailplanes are not equipped with elevator control systems, and should not be affected by the current AD. This action eliminates all reference to the Shempp-Hirth Models Nimbus 2, Mini-Nimbus HS-7, and Standard Cirrus sailplanes in the current AD.

Source

Authoritative
Federal Register document
Machine
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