Airworthiness Directive · Amendment 39-13308 · McDonnell Douglas Model DC-10-10, -10F, -15, -30, -30F (KC-10A and KDC-10), -40, and -40F Airplanes; and Model MD-10-10F and -30F Airplanes
McDonnell Douglas Model DC-10-10, -10F, -15, -30, -30F (KC-10A and KDC-10), -40, and -40F Airplanes; and Model MD-10-10F and -30F Airplanes
The Federal Register printed this AD without its applicability text. Read it at the link below.
This document corrects an error that appeared in airworthiness directive (AD) 2003-19-05 that was published in the Federal Register on September 22, 2003 (68 FR 54992). The error resulted in an incorrect Type Certificate holder name. This AD is applicable to certain McDonnell Douglas Model DC-10-10, -10F, -15, -30, -30F (KC-10A and KDC- 10), -40, and -40F airplanes; and certain Model MD-10-10F and -30F airplanes. This AD requires inspections for cracking and corrosion of the bolt assemblies and bushings on the hinge fittings of the inboard and outboard flaps of the left and right wings, and follow-on and corrective actions.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
