AD 2023-14-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Helicopters Model EC120B | Airworthiness Directives; Airbus Helicopters |
Unsafe Condition
Corrosion detected on certain part-numbered landing gear assemblies.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect for cracks and corrosion; borescope inspect; remove corrosion; measure thickness; interpret results of measurements; apply chemical conversion coating and primer; remove affected parts (landing gear assembly) and affected part sub-assemblies (front or rear crossbeam or left-hand or right-hand skid assembly) from service and replace with airworthy parts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Helicopters Model EC120B, EC130B4, and EC130T2 helicopters with certain part-numbered landing gear assemblies installed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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