Airworthiness Directives; Boeing Model 747-200, -300, and -400 Series Airplanes
airworthiness · Rule · Final rule. · Published 1996-11-06 · Effective 1996-12-06 · 61 FR 57291
Document
Document number
96-26952
Federal Register citation
61 FR 57291
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1996-11-06
Effective date
1996-12-06
FAA docket
Docket No. 94-NM-226-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 747-200, -300, and -400 series airplanes, that requires modification of the left and right inboard elevator servo assemblies and the hydraulic routing of the right inboard elevator power control package (PCP). This amendment is prompted by a report of an uncommanded right elevator deflection after takeoff and reports of elevator/control column bumps during landing gear retraction on these airplanes. The actions specified by this AD are intended to prevent uncommanded elevator deflection, which could result in structural damage and reduced controllability of the airplane.