AD 2022-05-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | GROB Aircraft AG | Various | Airworthiness Directives; GROB Aircraft SE (Type Certificate Previously Held by GROB Aircraft AG) Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; GROB Aircraft SE (Type Certificate Previously Held by GROB Aircraft AG) Airplanes |
Unsafe Condition
in-flight detachment of a rudder actuator hinge bracket, which could lead to failure or detachment of a control surface, possibly resulting in loss of control of the aeroplane
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
performing visual and x-ray inspections of the support structure at the attachment bolts of all flight control surfaces, and taking corrective actions if discrepancies are detected, repairing the support structure at the attachment bolts on certain flight control surfaces as terminating action for the inspection
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Compliance Time
Before further flight
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Affected Aircraft
GROB Aircraft SE, Model G 115EG airplanes
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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