Airworthiness Directive

AD 2004-17-02 Amendment 39-13774

Federal Aviation Administration · 14 CFR part 39

FR document
04-18923
Amendment
39-13774
Published
2004-08-20
Models covered
1
Last live check
Not yet re-verified
AD

2004-17-02

FR doc 04-18923

AD 2004-17-02Published 2004-08-20Effective 2004-10-04

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.

Full official 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.

Applies to 1 model in our index