AD 85-10-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-10-10 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-10F | Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-15 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-30 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-40 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-40F | Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A Series Airplanes |
Unsafe Condition
The speedbrake lever may latch into either the 2/3 or full speedbrake detent position during lever retraction after landing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the existing MS20470AD6 gate rivet in the speedbrake module assembly with a 4932183-3F034 corrosion-resistant steel rivet within two years after the effective date of this AD. Follow instructions in Chapter 27-62-01, Item 6, of the DC-10 Component Maintenance Manual dated August 1, 1982, or later revisions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within two years after the effective date of this AD
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Affected Aircraft
McDonnell Douglas Model DC-10 and KC-10A series airplanes, fuselage numbers 1 through 370, 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
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