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Airworthiness Directives; McDonnell Douglas Model DC-8-62, DC-8-63, DC-8-62F, and DC-8-63F Airplanes

airworthiness · Rule · Final rule. · Published 2007-02-14 · Effective 2007-03-21 · 72 FR 6921

Document

Document number
E7-2416
Federal Register citation
72 FR 6921
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2007-02-14
Effective date
2007-03-21
FAA docket
Docket No. FAA-2006-26084

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model DC-8-62, DC-8-63, DC-8-62F, and DC-8- 63F airplanes. This AD requires revising the wiring for the engine thrust brake circuit and indicating circuit and other specified actions, or rerouting the wiring at plug P1-1762A on the electrical power center generator control panel, as necessary. This AD results from the determination that the thrust reverser systems on these airplanes do not adequately preclude inadvertent deployment of the thrust reversers. We are issuing this AD to prevent inadvertent deployment of the thrust reversers during takeoff or landing, which could result in loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
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