AD 95-17-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Stemme GmbH & Co. KG | Stemme S10 | Airworthiness Directives; Stemme GMBH; Model S10 Gliders |
Unsafe Condition
Rupture of a turnbuckle eye bolt in the rudder control cable system could result in loss of rudder control and eventual loss of control of the glider.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the rudder control cable system in accordance with Stemme Service Bulletin A31-10-018 (pages 4-6), dated June 3, 1994. Special flight permits may be issued to operate the glider to a location where the AD requirements can be accomplished.
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Compliance Time
Required upon the accumulation of 150 hours time-in-service (TIS) or within the next 20 hours TIS after the effective date of this AD, whichever occurs later, unless already accomplished.
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Affected Aircraft
Stemme GmbH & Co. KG Model S10 Gliders (serial numbers 10-03 through 10-58), certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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