Summary
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain McDonnell Douglas Model MD-90 series airplanes. This proposal would require a one-time detailed visual inspection to detect fatigue cracking of certain longerons and the attaching frames of the lower left nose; and repair, if necessary. The proposal also would require installation of a preventive modification. This proposal is prompted by several reports of fatigue cracking of certain longerons and the attaching frames. The actions specified by the proposed AD are intended to prevent such fatigue cracking, which could result in reduced structural integrity of the fuselage, and consequent loss of pressurization of the airplane.