AD 95-14-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Glaser-Dirks Flugzeugbau GmbH | DG-100 | Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG-100 Sailplanes |
Unsafe Condition
Failure of the tailplane main fitting due to welding not covering the entire wall thickness, which could cause loss of control of the sailplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the tailplane main fitting to ensure welding covers the entire wall thickness as per Glaser-Dirks TN 301/15. If not, modify the fitting prior to further flight as per the same technical note.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished
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Affected Aircraft
Glaser-Dirks Flugzeugbau GmbH Model DG-100 sailplanes (all serial numbers) equipped with the main L4 fitting of the all flying tailplane.
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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