AD 79-15-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-10-10 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -30, -30F, -40 Series Airplanes |
| aircraft | The Boeing Company | DC-10-10F | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -30, -30F, -40 Series Airplanes |
| aircraft | The Boeing Company | DC-10-30 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -30, -30F, -40 Series Airplanes |
| aircraft | The Boeing Company | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -30, -30F, -40 Series Airplanes |
| aircraft | The Boeing Company | DC-10-40 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -30, -30F, -40 Series Airplanes |
Unsafe Condition
Asymmetric wing slat condition could lead to inadequate stall warning due to reliance on single angle of attack sensors and insufficient input from outboard wing slat group positions.
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Required Actions
Install two auto throttle/speed control computers or modify the stall warning and auto slat system to incorporate inputs from two angle of attack sensors and both outboard wing slat groups. Add a takeoff warning system slat function requirement to the Airplane Flight Manual limitations section within 30 days.
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Compliance Time
Before further flight and within 30 days after the effective date of this AD
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Affected Aircraft
McDonnell Douglas DC-10-10, -10F, -30, -30F (KC-10A, KDC-10), -40 series airplanes certificated in all categories.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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