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Airworthiness Directives; Boeing Model 747-400, -400D, and -400F Series Airplanes

airworthiness · Rule · Final rule. · Published 2005-02-18 · Effective 2005-03-25 · 70 FR 8239

Document

Document number
05-2843
Federal Register citation
70 FR 8239
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-02-18
Effective date
2005-03-25
FAA docket
Docket No. FAA-2004-18999

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-400, -400D, and -400F series airplanes. This AD requires replacing at least one flap control unit (FCU) in the main equipment center with a new or modified FCU. This AD is prompted by a report indicating that, after takeoff, an airplane was required to return to the airport because the autopilot disengaged. The report also indicated that, after selecting flaps for landing, the flaps indication display did not indicate the flap setting, requiring the airplane to land in alternate flap mode. We are issuing this AD to prevent disconnection of autoland/autopilot functions and loss of primary flaps control and flaps indication display due to disengagement of all three FCUs at the same time, which could lead to a non-normal high speed landing with the flaps retracted, increased pilot workload, and possible runway departure at high speeds during landing.

Source

Authoritative
Federal Register document
Machine
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