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Airworthiness Directives; Raytheon Aircraft Company Models B300 and B300C Airplanes

airworthiness · Rule · Final rule. · Published 1999-01-26 · Effective 1999-03-12 · 64 FR 3826

Document

Document number
99-1446
Federal Register citation
64 FR 3826
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Raytheon
Publication date
1999-01-26
Effective date
1999-03-12
FAA docket
Docket No. 97-CE-16-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Models B300 and B300C airplanes (commonly referred to as Beech Models B300 and B300C airplanes). This AD requires modifying the elevator trim tab actuators by incorporating a new elevator trim tab actuator assembly kit, replacing the elevator trim tab pushrod assembly, or modifying the elevator spar opening, whichever is applicable. Reports from operators of ice forming on the elevator trim tab actuators and jamming the trim tab control prompted this action. The actions specified by this AD are intended to prevent jamming of the elevator trim tab actuator caused by ice formations, which could result in loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
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