AD 76-03-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 200 | Airworthiness Directives; Beech Models 200 and A100-1 Airplanes |
| aircraft | Textron Aviation Inc. | A100-1 (U-21J) | Airworthiness Directives; Beech Models 200 and A100-1 Airplanes |
Unsafe Condition
Loose rivets securing the adapters to the aluminum tube of the P/N 101-524062-1 aft rudder push rod assembly could cause loss of rudder control.
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Required Actions
Inspect the P/N 101-524062-1 aft rudder push rod assembly for loose rivets as per Beechcraft Service Instruction 0778-153. Replace any affected assembly with airworthy P/N 101-524062-1 or P/N 101-524265-1. Notify FAA with FAA Form 8330-2 if defects are found.
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Compliance Time
within the next 50 hours' time in service after the effective date of this AD
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Affected Aircraft
Beech Models 200 and A100-1 (Serial Numbers BB-2 through BB-58)
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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