AD 2005-18-07

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; DC-8-50 Series Airplanes; DC-8F-54 and DC-8F-55 Airplanes; DC-8-60 Series Airplanes; DC-8-60F Series Airplanes; DC-8-70 Series Airplanes; and DC-8-70F Series Airplanes

AD Number
2005-18-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2004-19536
FR Citation
70 FR 52285

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-8-11 Airworthiness Directives; McDonnell Douglas Model DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; DC-8-50 Series Airplanes; DC-8F-54 and DC-8F-55 Airplanes; DC-8-60 Series Airplanes; DC-8-60F Series Airplanes; DC-8-70 Series Airplanes; and DC-8-70F Series Airplanes

Unsafe Condition

Fatigue cracks in the fuselage skin in the lower cargo doorjamb corners.

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

Required Actions

Inspect for cracking of the lower cargo doorjamb corners. Perform corrective action if necessary. Modify the lower cargo doorjamb corners for certain airplanes.

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

Compliance Time

Before further flight.

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

Affected Aircraft

McDonnell Douglas Model DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43, DC-8-50 Series, DC-8F-54, DC-8F-55, DC-8-60 Series, DC-8-60F Series, DC-8-70 Series, and DC-8-70F Series airplanes.

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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