# Airworthiness Directives; McDonnell Douglas Model DC-10-30 and DC-10-30F (KC-10A and KDC-10) Airplanes, Model DC-10-40 and DC-10-40F Airplanes, and Model MD-10-30F Airplanes
> **Rule** · Final rule. · Published 2007-05-30 · Effective 2007-07-05 · 72 FR 29881
## Document
- **Document number:** E7-10110
- **Category:** airworthiness
- **Manufacturer:** McDonnell Douglas Model DC-10-30 and DC-10-30F (KC-10A and KDC-10)
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 72 FR 29881
- **Publication date:** 2007-05-30
- **Effective date:** 2007-07-05
- **FAA docket:** Docket No. FAA-2007-27340
## Abstract

The FAA is adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model DC-10-30 and DC-10-30F (KC-10A and KDC- 10) airplanes, Model DC-10-40 and DC-10-40F airplanes, and Model MD-10- 30F airplanes. This AD requires installing bracket assemblies and jumper wires in the center main wheel well to improve the bonding path between the structure (wall) of the lower auxiliary fuel tank and its internal fuel pumps; measuring the electrical resistance between the fuel pump housings and the fuel tank structure; and doing corrective actions if necessary. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to detect and correct an inadequate bond between the internal fuel pump housings and the structure of the lower auxiliary fuel tank. This condition, if not corrected, could fail to meet fault current requirements and result in a potential ignition source that, in combination with flammable fuel vapors, could cause a fuel tank explosion and consequent loss of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2007/05/30/E7-10110/airworthiness-directives-mcdonnell-douglas-model-dc-10-30-and-dc-10-30f-kc-10a-and-kdc-10-airplanes)
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