AD 92-16-02
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
Inadvertent deployment of a thrust reverser during flight.
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Required Actions
Revise the wiring in certain panels, wing-body disconnects, and wing-strut disconnects in accordance with Boeing Alert Service Bulletin 767-78A0052, Revision 1 or 2, depending on the airplane's listing in the bulletin. Procedures previously accomplished under Revision 1 that remain unchanged in Revision 2 need not be repeated.
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Compliance Time
Within 60 days after March 18, 1992 for airplanes listed in Revision 1, and within 60 days after July 27, 1992 for those listed in Revision 2.
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Affected Aircraft
Boeing Model 767 series airplanes equipped with General Electric CF6-80C2 engines, 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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