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importantRule

AD FAA-2006-26084

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

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

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for McDonnell Douglas Model DC-8-62, DC-8-63, DC-8-62F, and DC-8-63F →

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