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AD Issued on Mini-Nimbus B and HS-7; 2006-22-10; flap torque drive.

This new directive (AD) is for Mini-Nimbus B or HS-7 sailplanes certificated in any category. A torsional flap drive failed at the lever arm weld. Within 90 days after December 1, 2006, owners must reinforce the flap weld per Schempp-Hirth Technical Note No. 286-35/No. 328-13.

This Ad becomes effective on December 1, 2006. Full text of the AD may be found at FAA.gov

C. Brickner
Govt. Liaison Committee

Posted: 10/30/2006


Government Liaison Committee 

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