# 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
> **Rule** · Final rule. · Published 2003-09-22 · Effective 2003-10-27 · 68 FR 54992
## Document
- **Document number:** 03-23670
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 68 FR 54992
- **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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2003/09/22/03-23670/airworthiness-directives-mcdonnell-douglas-model-dc-10-10--10f--15--30--30f-kc-10a-and-kdc-10--40)
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