AD 2001-19-52
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
Failure of a main rotor pendulum weight support resulting in shedding of the weights and increased main rotor vibration.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove from service all main rotor pendulum weight supports, part number 222-011-114-103, with a serial number having the prefix 'HD', and replace them with airworthy supports.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 25 hours time-in-service or 3 months, whichever occurs first.
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Affected Aircraft
Bell Helicopter Textron Canada Model 222 (S/N 47006-47089), Model 222B (S/N 47131-47156), Model 222U (S/N 47501-47574), and Model 230 (S/N 23001-23038) helicopters, certificated in any category.
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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