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Fri, Nov 14, 2003

AD: Cessna

AD NUMBER: 2003-23-02

MANUFACTURER: Cessna
SUBJECT: Airworthiness Directive 2003-23-02
SUMMARY: This amendment adopts a new airworthiness directive (AD) that is applicable to certain Cessna Model 560 airplanes. This action requires disengaging and tie-strapping the pitch trim and autopilot servo (servo 1) circuit breakers. This action also provides an optional inspection and follow-on actions that, if accomplished, terminates the requirement to disengage and tie-strap those circuit breakers. This action is necessary to prevent a single-point failure in the trim system from causing a runaway trim condition that the pilot may be unable to stop by using the autopilot disconnect switch. This condition could result in loss of control of the airplane. This action is intended to address the identified unsafe condition.

FMI: http://ftp.atp.com/ADs/pdf/032302.pdf

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