# Airworthiness Directives; McDonnell Douglas Model MD-11 Series Airplanes
> **Rule** · Final rule. · Published 2000-02-17 · Effective 2000-03-23 · 65 FR 8034
## Document
- **Document number:** 00-3620
- **Category:** airworthiness
- **Manufacturer:** McDonnell Douglas Model MD-11 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 8034
- **Publication date:** 2000-02-17
- **Effective date:** 2000-03-23
- **FAA docket:** Docket No. 99-NM-168-AD
## Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to all McDonnell Douglas Model MD-11 series airplanes, that currently requires a one-time inspection to detect discrepancies at certain areas around the entry light connector of the sliding ceiling panel above the forward passenger doors, and repair, if necessary. For certain airplanes, this amendment requires the installation or modification of a flapper door ramp deflector on the forward entry drop ceiling structure. For certain other airplanes, this amendment requires inspection of the wire assembly support installation for evidence of chafing, and corrective actions, if necessary. This amendment is prompted by a report indicating that damaged electrical wires were found above the forward passenger doors due to flapper panels moving inboard and chafing the electrical wire assemblies of this area. The actions specified by this AD are intended to prevent such chafing, which could result in an electrical fire in the passenger compartment.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/02/17/00-3620/airworthiness-directives-mcdonnell-douglas-model-md-11-series-airplanes)
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