Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes
airworthiness · Rule · Final rule. · Published 2007-01-17 · Effective 2007-02-21 · 72 FR 1928
Document
Document number
E7-399
Federal Register citation
72 FR 1928
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A300 B2 and B4 Series
Publication date
2007-01-17
Effective date
2007-02-21
FAA docket
Docket No. FAA-2006-25670
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A300 B2 and B4 series airplanes. This AD requires revising the airplane flight manual (AFM) to include procedures for resetting the trim and pitch trim levers after each landing, determining which servomotor moves the pitch trim control wheel, and doing applicable other specified actions. This AD also provides for optional terminating actions for those requirements. This AD results from a report of a sudden nose-up movement after disengagement of the autopilot in cruise. We are issuing this AD to ensure that the flightcrew is aware of the procedures for resetting the trim and pitch trim levers after each landing and to prevent failure of the servomotors of the pitch trim systems during flight. Failure of the servomotors of the pitch trim systems could result in uncommanded nose- up movement of the control surface of the pitch trim systems after disengagement of the autopilot in cruise.