AD 80-03-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-10-10 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10, -10F, -30, -30F, -40 Series Airplanes |
| aircraft | The Boeing Company | DC-10-10F | Airworthiness Directives; MCDONNELL DOUGLAS DC-10, -10F, -30, -30F, -40 Series Airplanes |
| aircraft | The Boeing Company | DC-10-30 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10, -10F, -30, -30F, -40 Series Airplanes |
| aircraft | The Boeing Company | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; MCDONNELL DOUGLAS DC-10, -10F, -30, -30F, -40 Series Airplanes |
| aircraft | The Boeing Company | DC-10-40 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10, -10F, -30, -30F, -40 Series Airplanes |
Unsafe Condition
Complete failure of the stall warning function
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install two auto throttle/speed control computers receiving information from both outboard wing slat groups and other inputs; install a stick shaker at the First Officer's position, with both stick shakers actuated by either computer using approved design data.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
On or before 210 days after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas DC-10, -10F, -30, -30F (KC-10A, KDC-10), -40 series airplanes certificated in all categories
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.