AD 77-13-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 200 | Beech Model 200 Airplanes |
Unsafe Condition
Failure of the aileron control system to carry the 50 feet/second gust design loads due to improper droop of the right and left ailerons.
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Required Actions
Within 50 hours' time in service after July 1, 1977, rerig the droop of right and left ailerons to zero degrees with a tolerance of plus one-half degree up, minus zero degrees down using Beechcraft Service Instructions Number 0906 or approved revisions. Equivalent methods require approval from the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
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Compliance Time
within 50 hours' time in service after the effective date of this AD
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Affected Aircraft
Beech Model 200 airplanes (Serial Numbers BB-2 thru BB-250) certificated in all categories.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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