AD 95-20-51
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes |
| aircraft | The Boeing Company | 767-300 Series | Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes |
Unsafe Condition
Stress corrosion cracking in the outer cylinder of the aft trunnion assembly, which could initiate at the crossbolt hole or aft trunnion bushing fillet seal, leading to main landing gear collapse under certain loading conditions.
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Required Actions
Perform an external general visual inspection of the lower half of the aft trunnion of the main landing gear within 48 clock hours after the effective date to detect damage, cracking, missing pieces, or corrosion. Discrepancies must be repaired using FAA-approved methods. Inspections are required in addition to those in AD 95-19-10 for airplanes with MLG 4 years old or older.
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Compliance Time
Within 48 clock hours after the effective date of this AD
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Affected Aircraft
Boeing Model 767-200 and 767-300 series airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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