Airworthiness Directives; Airbus Model A310 and A300-600 Series Airplanes
airworthiness · Rule · Final rule. · Published 1998-09-21 · Effective 1998-10-26 · 63 FR 50135
Document
Document number
98-24906
Federal Register citation
63 FR 50135
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A310 and A300-600 Series
Publication date
1998-09-21
Effective date
1998-10-26
FAA docket
Docket No. 97-NM-310-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain Airbus Model A310 and A300-600 series airplanes, that currently requires, among other things, repetitive inspections to ensure correct synchronization of the hydraulic control valves of the trimmable horizontal stabilizer (THS) actuator; replacement of the horizontal stabilizer actuator motors with new or serviceable motors and resynchronization of the valves, or adjustment of the synchronization, if necessary; and a functional test of the THS. This amendment adds a requirement to replace the hydraulic motor of the THS with an improved motor, which constitutes terminating action for the repetitive inspections. This amendment also expands the applicability to include additional airplanes. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent desynchronization of the hydraulic control valves, which could result in runaway of the horizontal stabilizer to its full up or down position, subsequent reduced maneuvering capability, and potential pitch upset.