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Airworthiness Directives; Israel Aircraft Industries (IAI), Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-09-29 · Effective 1998-11-03 · 63 FR 51803

Document

Document number
98-25776
Federal Register citation
63 FR 51803
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Israel
Publication date
1998-09-29
Effective date
1998-11-03
FAA docket
Docket No. 98-NM-108-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to all IAI, Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A series airplanes, that currently requires repetitive inspections of the trim actuator of the horizontal stabilizer to verify jackscrew integrity and to detect excessive wear of the tie rod, and replacement of the actuator or tie rod, if necessary. That AD also provides for optional terminating action for the repetitive inspections. This amendment requires accomplishment of the previously optional terminating action. 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 failure of the trim actuator of the horizontal stabilizer due to failure of the jackscrews, which could result in reduced controllability of the airplane.

Source

Authoritative
Federal Register document
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