AD 2002-01-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron | Canada Model 430 | Airworthiness Directives; Bell Helicopter Textron Canada Model 430 Helicopters |
| aircraft | Bell | Helicopter Textron Canada Model 430 | Airworthiness Directives; Bell Helicopter Textron Canada Model 430 Helicopters |
Unsafe Condition
Design deficiencies in the electrical systems may lead to failure of both generators and loss of primary electrical power, resulting in subsequent loss of control of the helicopter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the electrical power distribution system to address design deficiencies. Install necessary modifications to prevent dual generator failure and loss of primary electrical power.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight.
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Affected Aircraft
Bell Helicopter Textron Canada Model 430 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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