AD 2007-24-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; GROB-WERKE GMBH & CO KG Models G102 CLUB ASTIR III, G102 CLUB ASTIR IIIb, and G102 STANDARD ASTIR III Gliders |
Unsafe Condition
Cracks on welded parts of the flight control system progress slowly from the welding seams periphery and may eventually result in rupture at a matured stage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the welded parts of the flight control system for cracks, deformations, or distortions within 25 hours time-in-service or 6 calendar months after January 3, 2008, whichever occurs first. If cracks are found, replace the affected part before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 25 hours time-in-service or 6 calendar months after January 3, 2008, whichever occurs first.
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Affected Aircraft
GROB-WERKE GMBH & CO KG Models G102 CLUB ASTIR III (SNs 5501-C through 5652-C), G102 CLUB ASTIR IIIb (SNs 5501-Cb through 5652-Cb), and G102 STANDARD ASTIR III (SNs 5502-S through 5652-S).
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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