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Airworthiness Directives; Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes

airworthiness · Rule · Final rule. · Published 2004-08-20 · Effective 2004-10-04 · 69 FR 51549

Document

Document number
04-18923
Federal Register citation
69 FR 51549
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Raytheon
Publication date
2004-08-20
Effective date
2004-10-04
FAA docket
Docket No. 2004-CE-04-AD

Abstract

The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company (Raytheon) 65, 90, 99, 100, 200, 300, and 1900 series airplanes. This AD requires you to repetitively inspect the engine controls/cross shaft/pedestal for proper installation and torque, re-torque the cross shaft attach bolt, modify the pedestal, and replace the engine controls cross shaft hardware. Modification of the pedestal and replacement of the engine controls cross shaft hardware is terminating action for the repetitive inspection requirements. This AD is the result of numerous reports of loose bolts on the pedestal attachment of the throttle/prop cross shaft assembly. We are issuing this AD to detect and correct loose bolts not securing the pedestal cross shaft, which could result in limited effectiveness of the control levers. This failure could lead to an aborted takeoff.

Source

Authoritative
Federal Register document
Machine
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