AD 2002-08-54
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron | Canada Model 222 | Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 Helicopters |
| aircraft | Bell | Helicopter Textron Canada Model 222 | Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 Helicopters |
Unsafe Condition
Fatigue cracks in the main rotor grip assembly and pitch horn could lead to failure of these components and subsequent loss of control of the helicopter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually check each main rotor grip assembly and pitch horn at specified intervals. Inspect each affected grip and pitch horn using a 10-power or higher magnifying glass for cracks at specified intervals. Replace any unairworthy grip or pitch horn with an airworthy part if a crack is found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight if a crack is found.
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Affected Aircraft
Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 helicopters.
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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