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Airworthiness Directives; Alexander Schleicher Model ASW 27 Sailplanes

airworthiness · Rule · Final rule. · Published 2004-06-08 · Effective 2004-07-27 · 69 FR 31870

Document

Document number
04-12574
Federal Register citation
69 FR 31870
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-06-08
Effective date
2004-07-27
FAA docket
Docket No. 2003-CE-53-AD

Abstract

The FAA adopts a new airworthiness directive (AD) for all Alexander Schleicher Model ASW 27 sailplanes equipped with integrated (wet inner surface) water ballast tanks in the wings, which could put the center of gravity (CG) of the sailplane out of the acceptable range. This AD requires you to install a warning placard requiring pilots weighing more than 105 kg (231.5 lbs) to use the rearmost backrest hinge position; and requires you to determine the forward empty CG and make any necessary adjustments. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to correct the CG to the acceptable range when integrated ballast water tanks are installed. Failure of the sailplane to be within the acceptable CG range could result in loss of sailplane control.

Source

Authoritative
Federal Register document
Machine
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