AD 2013-25-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron | Canada Limited | Airworthiness Directives; Bell Helicopter Textron Canada Limited Helicopters |
| aircraft | Bell | Helicopter Textron Canada Limited | Airworthiness Directives; Bell Helicopter Textron Canada Limited Helicopters |
Unsafe Condition
A crack in a tailboom attachment fitting, which could lead to loss of the tailboom 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
Inspect the upper left tailboom attachment fitting for a crack, corrosion, damage, or a loose rivet. Replace the fitting if there is a crack or corrosion/damage beyond acceptable limits. Repair the fitting if corrosion or damage is within acceptable limits. Replace any loose rivet.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 110 flight hours after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bell Helicopter Textron Canada Limited Model 206L, 206L-1, 206L-3, and 206L-4 helicopters with an upper left attachment fitting part number 206-032-409-001 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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