AD 99-19-29
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
Cracking of the H-11 tension bolts on the side-of-body kick-load fitting due to stress corrosion, which could result in reduced structural integrity of the wing-to-body joint structure.
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Required Actions
Perform a detailed visual inspection of the four H-11 tension bolts at each side-of-body kick-load fitting and on the lower splice plate located on the wing rear spar to detect damaged or broken bolts. Repeat inspections at intervals not exceeding 90 days or 18 months depending on the chosen option, followed by replacement of existing bolts with improved bolts as terminating action.
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Compliance Time
Within 90 days after the effective date of this AD
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Affected Aircraft
Boeing Model 767 series airplanes, line positions 1 through 177 inclusive, 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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