Airworthiness Directives; Airbus Model A300, A300-600, and A310 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2000-01-25 · Effective 2000-02-09 · 65 FR 3799
Document
Document number
00-1595
Federal Register citation
65 FR 3799
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2000-01-25
Effective date
2000-02-09
FAA docket
Docket No. 2000-NM-09-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Airbus Model A300 and all Model A300-600 and A310 series airplanes. This action requires performing a pitch trim system test to detect any continuity defect in the autotrim function, and follow-on corrective actions, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to prevent a sudden change in pitch due to an out- of-trim condition combined with an autopilot disconnect, which could result in reduced controllability of the airplane.