AD 86-24-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bell Helicopter Textron Canada Limited | 206A | Airworthiness Directives; BELL HELICOPTER TEXTRON, INC. Model 206A, 206B, and 206L Helicopters |
| aircraft | Bell Helicopter Textron Canada Limited | 206B | Airworthiness Directives; BELL HELICOPTER TEXTRON, INC. Model 206A, 206B, and 206L Helicopters |
| aircraft | Bell Helicopter Textron Canada Limited | 206L | Airworthiness Directives; BELL HELICOPTER TEXTRON, INC. Model 206A, 206B, and 206L Helicopters |
Unsafe Condition
Failure of the T/R pitch links due to the combination of T/R yoke Part Number 206-011-819-101 with T/R crosshead Part Numbers 206-010-741-001 or -003.
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Required Actions
Within the next 25 hours' time in service, inspect T/R assembly to determine if the specified T/R yoke and crosshead combination is installed. If installed, either replace the T/R yoke with P/N 206-011-811-009 or replace the T/R crosshead with P/N 206-011-855-001 or 206-011-857-001.
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Compliance Time
within the next 25 hours' time in service
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Affected Aircraft
Bell Helicopter Textron Inc. Model 206A, 206B, and 206L helicopters equipped with T/R yoke P/N 206-011-819-101 and T/R crosshead P/N 206-010-741-001 or -003.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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