AD 2002-19-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron | Various | Airworthiness Directives; Bell Helicopter Textron, Inc. Model 212 Helicopters |
| aircraft | Bell | Helicopter Textron | Airworthiness Directives; Bell Helicopter Textron, Inc. Model 212 Helicopters |
Unsafe Condition
Failure of the vertical fin spar cap due to cracking, disbonding, corrosion, or loose fasteners, which could lead to loss of a tail rotor 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 inspect certain vertical fin left-hand spar caps for cracking, loose fasteners, corrosion, or disbonding. Repair any corrosion or loose fasteners found. Replace any cracked or disbonded spar cap with an airworthy part. Replace certain spar caps within 24 months.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 24 months of the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bell Helicopter Textron, Inc. Model 212 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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