AD 2007-02-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-8-55 | Airworthiness Directives; McDonnell Douglas Model DC-8-55, DC-8F-54, and DC-8F-55 Airplanes; and Model DC-8-60, DC-8-70, DC-8-60F, and DC-8-70F Series Airplanes |
Unsafe Condition
Cracks in the aft fuselage skin at the longeron 28 skin splice could lead to loss of structural integrity of the aft fuselage, resulting in rapid decompression of the airplane.
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Required Actions
Conduct a one-time inspection for previous repairs of the aft fuselage skin panel at the longeron 28 skin splice. Perform repetitive inspections for cracks in the same area. Take related investigative and corrective actions as necessary.
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Compliance Time
Before further flight
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Affected Aircraft
McDonnell Douglas Model DC-8-55, DC-8F-54, DC-8F-55, DC-8-60, DC-8-70, DC-8-60F, and DC-8-70F Series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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