AD 92-10-01
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
The overwing escape slide may be damaged by sharp edges of the rub strip on the inboard spoilers.
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Required Actions
Modify the inboard edges of the rub strip on the inboard spoilers in accordance with Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991. For airplanes with part numbers 113T4100-37, -38, -41, -42, -45, and -46, the modification must be done within 9 months after the effective date of this AD. An alternative method of compliance may be used if approved by the FAA.
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Compliance Time
Within the next 9 months after August 29, 1991 (the effective date of amendment 39-7077) for most airplanes, or within the next 9 months after the effective date of this AD (June 11, 1992) for airplanes with specified part numbers.
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Affected Aircraft
Boeing Model 767 series airplanes listed in Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991; 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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