AD 79-17-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 76 | Airworthiness Directives; BEECH Model 76 Airplanes |
Unsafe Condition
Collapse of the main landing gear due to insufficient clevis pin strength.
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Required Actions
Install new part number MS20392-2C67 clevis pins in the left and right main landing gear fork and fork pin within 25 hours time-in-service after the effective date. Use Beechcraft Service Instructions Number 1073 and specified tools including a 3/16 inch diameter carbide tip drill bit, drill press, and clamping equipment.
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Compliance Time
within the next twenty-five (25) hours time-in-service after the effective date of this AD
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Affected Aircraft
BEECH Model 76 Airplanes (Serial Numbers ME-1 through ME-228)
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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