AD 95-10-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | MD-11 | Airworthiness Directives; McDonnell Douglas Model MD-11 Series Airplanes |
| aircraft | The Boeing Company | MD-11F | Airworthiness Directives; McDonnell Douglas Model MD-11 Series Airplanes |
Unsafe Condition
Inadvertent deployment of the slats while the airplane was in flight at cruise altitude could result in an abrupt pitch up of the airplane and consequent injury to crew and passengers, as well as significant vibrations and damage to the elevators.
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Required Actions
Install an electrically controlled slat control system in accordance with McDonnell Douglas MD-11 Service Bulletin 27-36, Revision 1, dated December 9, 1994. This modification must be completed within 24 months after the effective date of this AD.
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Compliance Time
Within 24 months after the effective date of this AD
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Affected Aircraft
McDonnell Douglas Model MD-11 series airplanes as listed in McDonnell Douglas MD-11 Service Bulletin 27-36, Revision 1, dated December 9, 1994, 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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