Summary
We are adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model DC-9-81 (MD-81) and DC-9-82 (MD-82) airplanes. This AD requires, for certain airplanes, inspecting for cracking of the fuselage skin at the upper corners of the forward passenger doorjamb, installing or replacing doublers as applicable, and doing applicable repairs. This AD results from reports of fatigue cracking in the fuselage skin at the upper corners of the forward passenger doorjamb. We are issuing this AD to prevent cracking of the fuselage skin at the upper corners of the forward passenger doorjamb, which could lead to loss of overall structural integrity of the airplane.
Directive Details
AD Number
FAA-2007-29226
Document Number
E7-23687
Type
Rule
Publication Date
December 10, 2007
Effective Date
January 14, 2008
Affected Manufacturer
McDonnell Douglas Model DC-9-81 (MD-81) and DC-9-82 (MD-82)
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2007-29226
Topics
Official Documents
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