← FAA Federal Register actions

Airworthiness Directives; Saab Model SAAB SF340A, SAAB 340B, and SAAB 2000 Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-06-25 · Effective 1998-07-30 · 63 FR 34587

Document

Document number
98-16697
Federal Register citation
63 FR 34587
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1998-06-25
Effective date
1998-07-30
FAA docket
Docket No. 96-NM-212-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Saab Model SAAB SF340A, SAAB 340B, and SAAB 2000 series airplanes, that requires repetitive operational tests of the pitch trim system of the elevator trim-tab of the flight control unit to ensure that the system operates correctly, and repair if necessary. This amendment is prompted by a report of uncommanded movement of the right-hand elevator trim-tab to a maximum deflection position, which was apparently due to a failure in the aircraft harness and a fault in the pitch trim synchronizer. The actions specified by this AD are intended to prevent such uncommanded movement of the elevator trim-tab, which could lead to structural overload of the horizontal stabilizers at speeds above 180 knots, and consequent reduced controllability of the airplane.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown