AD 75-09-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bell Helicopter Textron Canada Limited | 206A | Airworthiness Directives; Bell Model 206A and 206B Helicopters |
| aircraft | Bell Helicopter Textron Canada Limited | 206A-1 (OH-58A) | Airworthiness Directives; Bell Model 206A and 206B Helicopters |
| aircraft | Bell Helicopter Textron Canada Limited | 206B | Airworthiness Directives; Bell Model 206A and 206B Helicopters |
| aircraft | Bell Helicopter Textron Canada Limited | 206B-1 | Airworthiness Directives; Bell Model 206A and 206B Helicopters |
Unsafe Condition
Failure of the tail rotor control tube assembly, P/N 206-010-743-13.
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Required Actions
Compliance with items 1 through 5 of Bell Helicopter Company Service Bulletin 206-75-2, dated February 18, 1975, or later FAA approved revision is required. This includes inspection, modification, or replacement as specified in the service bulletin.
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Compliance Time
within the next 100 hours' time in service after the effective date of this AD
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Affected Aircraft
Bell Helicopter Textron Canada Limited Model 206A, 206A-1 (OH-58A), 206B, 206B-1 helicopters, serial numbers 4 through 497
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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