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Airworthiness Directives; Fokker Model F.28 Mark 1000, 2000, 3000, and 4000 Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-06-25 · Effective 1998-07-30 · 63 FR 34569

Document

Document number
98-16451
Federal Register citation
63 FR 34569
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1998-06-25
Effective date
1998-07-30
FAA docket
Docket No. 98-NM-16-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Fokker Model F.28 Mark 1000, 2000, 3000, and 4000 series airplanes, that currently requires an inspection to detect free movement of the actuator servo-valve sub-assembly of the horizontal stabilizer actuator, and replacement, if necessary. This amendment adds a one-time inspection to determine the residual strength of the servo-valve sub-assembly of the horizontal stabilizer actuator, and replacement of the actuator with a new or serviceable actuator, if necessary; and eventual replacement of the horizontal stabilizer actuator with an improved actuator. 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 uncommanded trimming or failure of the trim system of the horizontal stabilizer, and consequent reduced controllability of the airplane.

Source

Authoritative
Federal Register document
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