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AD AD 2007-02-02

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

Summary

This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-8 airplanes. This AD requires a one-time inspection for previous repairs of the aft fuselage skin panel at the longeron 28 skin splice; repetitive inspections for cracks of the same area; and related investigative and corrective actions. This AD also provides optional actions for extending the repetitive inspection intervals. The actions specified by this AD are intended to detect and correct cracks in the aft fuselage skin at the longeron 28 skin splice, which could lead to loss of structural integrity of the aft fuselage, resulting in rapid decompression of the airplane. This action is intended to address the identified unsafe condition.

Directive Details

AD Number

AD 2007-02-02

Document Number

E7-710

Type

Rule

Publication Date

January 24, 2007

Effective Date

February 28, 2007

Affected Manufacturer

McDonnell Douglas Model DC-8-55, DC-8F-54, and DC-8F-55

Criticality

routine

Emergency

No

Docket ID

Docket No. 2001-NM-183-AD

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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