Airworthiness Directives; 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
airworthiness · Rule · Final rule. · Published 2003-09-22 · Effective 2003-10-27 · 68 FR 54992
Document
Document number
03-23670
Federal Register citation
68 FR 54992
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2003-09-22
Effective date
2003-10-27
FAA docket
Docket No. 2002-NM-164-AD
Abstract
This amendment adopts a new airworthiness directive (AD), 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, that 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. This action is necessary to prevent failure of the bolt and bushing that attach the hinge fitting to the flap, which could result in loss of the flap and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.