AD Amdt-39-10917

final rule
Data completeness: 70%

Airworthiness Directives; Stemme GmbH & Co. KG Models S10, S10-V, and S10-VT Sailplanes

AD Number
Amdt-39-10917
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-CE-106-AD
FR Citation
63 FR 65057

Unsafe Condition

Cracks in certain areas of the flight control system could result in flight control system failure, leading to reduced or loss of control of the sailplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect certain areas in the flight control system for cracks. Immediately replace any cracked parts. Eventually replace all longitudinal coupling with modified coupling, regardless of whether cracks are found.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

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Affected Aircraft

Stemme GmbH & Co. KG Models S10, S10-V, and S10-VT sailplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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View Official Source ↗