AD 2006-22-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; Schempp-Hirth GmbH & Co. KG Models Mini-Nimbus B and Mini-Nimbus HS-7 Sailplanes |
Unsafe Condition
Failure in the flap actuating circuit due to the lever at the torsional drive in the fuselage failing at the weld.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Reinforce the flap drive within 90 days after December 1, 2006, following Schempp-Hirth Flugzeugbau GmbH Technical Note No. 286-35/No. 328-13, EASA approved on July 1, 2005.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 days after December 1, 2006
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Affected Aircraft
Schempp-Hirth GmbH & Co. KG Models Mini-Nimbus B and Mini-Nimbus HS-7 sailplanes, all serial numbers, certificated in any U.S. category.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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