Summary
We are adopting a new airworthiness directive (AD) for certain Model DC-10-10, DC-10-10F, and MD-10-10F airplanes. This AD requires a one-time high frequency eddy current inspection of fastener holes for cracks at the left and right side wing rear spar lower cap at station Xors=345, and other specified and corrective actions if necessary. This AD results from a report of three instances of Model DC-10-10F airplanes having fuel leaks in the wing rear spar lower cap at station Xors=345. We are issuing this AD to prevent cracks in the spar cap, which could lead to cracking of the lower wing skin, fuel leaks, and the inability of the structure to sustain limit load.
Directive Details
AD Number
FAA-2010-0043
Document Number
2010-14982
Type
Rule
Publication Date
June 23, 2010
Effective Date
July 28, 2010
Affected Manufacturer
McDonnell Douglas Corporation Model DC-10-10, DC-10-10F, and MD-10-10F
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2010-0043
Topics
Official Documents
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