AD 95-19-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | Airworthiness Directives; Boeing Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300 Series | Airworthiness Directives; Boeing Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300F Series | Airworthiness Directives; Boeing Model 767 Series Airplanes |
Unsafe Condition
Fractures of the outer cylinder aft trunnion of the main landing gear due to stress corrosion cracking caused by moisture entering between the outer cylinder and a mating bushing.
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Required Actions
Perform visual inspections of the outer cylinder aft trunnion to determine if the fillet seal is cracked or missing, inspect for corrosion in this location, and follow procedures for repair or reapplication of corrosion inhibiting compound (CIC) and greasing based on findings. Repetitive inspections and CIC/grease applications are required every 500 flight hours.
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Compliance Time
Required as indicated, unless accomplished previously.
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Affected Aircraft
Boeing Model 767-200 Series, 767-300 Series, 767-300F Series airplanes, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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