AD 2001-24-28
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-8 | Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes |
Unsafe Condition
Cracking of the rudder pedals adjuster hub assembly, which could lead to loss of rudder pedals control and reduction of braking capability.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the rudder pedals adjuster hub assembly for cracks using visual and eddy current inspections. Replace the assembly with a new one if cracks are detected. Accomplish a terminating action for the repetitive inspections as specified.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 15,000 total landings, or within 3,500 landings after the effective date of this AD.
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Affected Aircraft
McDonnell Douglas Model DC-8 series airplanes, serial numbers 45646 and 45928, and as listed in McDonnell Douglas DC-8 Alert Service Bulletin A27-275, Revision 1, dated February 3, 1992; certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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