Summary
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.
Directive Details
AD Number
FAA-2006-26084
Document Number
E7-2416
Type
Rule
Publication Date
February 14, 2007
Effective Date
March 21, 2007
Affected Manufacturer
McDonnell Douglas Model DC-8-62, DC-8-63, DC-8-62F, and DC-8-63F
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2006-26084
Topics
Official Documents
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