# Proposed AD 99-NM-211-AD: McDonnell Douglas Model DC-10-10, -15, -30, -30F, and -40 Series Airplanes, and KC-10A (Military) Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2000-15-05
- Action: Notice of proposed rulemaking (NPRM).
- Published: January 26, 2000, 65 FR 4190
- Comments due: March 13, 2000
- Became: [AD 2000-15-05](https://openairdocs.org/ad/2000-15-05)
- Docket: 99-NM-211-AD
- FR document: 00-1773
- Official PDF: https://openairdocs.org/files/sha256/af/00/af003eeaf6af0b6286efcf057d2a4ed78d97967a19e94d5a96fcdacf76e52664 (from https://www.govinfo.gov/content/pkg/FR-2000-01-26/pdf/00-1773.pdf)
- Federal Register: https://www.federalregister.gov/documents/2000/01/26/00-1773/airworthiness-directives-mcdonnell-douglas-model-dc-10-10--15--30--30f-and--40-series-airplanes-and
- Page: https://openairdocs.org/proposed/99-NM-211-AD

## Summary

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain McDonnell Douglas Model DC-10-10, -15, -30, -30F, and -40 series airplanes, and KC-10A (military) airplanes. This proposal would require a one-time inspection of the wiring and wire bundles of the aft main avionics rack (MAR) to determine if the wires are damaged, or riding or chafing on structure, clamps, braces, standoffs, or clips, and to detect damaged or out of alignment rubber cushions inserts of the wiring clamps; and corrective actions, if necessary. This proposal is prompted by an incident in which the automatic and manual cargo door test in the cockpit was inoperative during dispatch of the airplane, due to wiring of the main avionics rack chafing against clamps as a result of the wire bundles being installed improperly during production of the airplane. The actions specified by the proposed AD are intended to ensure that the wires that route from the main wire bundles to the MAR and associated brackets, clamps, braces, standoffs, and clips are installed properly. Improper installation of such wiring and structure could cause chafing of the wires/wire bundles, which could result in electrical arcing, smoke, and possible fire in the MAR.

## Notices in this docket

- Jan 26, 2000: Notice of proposed rulemaking (NPRM). (first notice), FR document 00-1773, comments due Mar 13, 2000 (https://www.federalregister.gov/documents/2000/01/26/00-1773/airworthiness-directives-mcdonnell-douglas-model-dc-10-10--15--30--30f-and--40-series-airplanes-and)

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