AD 2001-24-28

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes

AD Number
2001-24-28
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-210-AD
FR Citation
66 FR 64107

Applicability

TypeManufacturerModelDetails
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.

AI-generated summary from the source AD text. Verify against the official source before acting.

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.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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