Is AD 2003-23-02 a recurring Airworthiness Directive?

No — AD 2003-23-02 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2003-23-02 apply to?

AD 2003-23-02 applies to Cessna — models 560. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2003-23-02

one-time

Official AD 2003-23-02 · FR doc 03-28166 · 2003-11-13 · airframe

Airworthiness Directives; Cessna Model 560 Airplanes

What this AD requires

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.

Which aircraft AD 2003-23-02 applies to

MakesCessna

Models560

Serial-conditional — narrows to serials 0260–0396.

Excludes airplanes on which Cessna Service Bulletin 560-34-93, dated March 16, 2001, has been accomplished.

Whether AD 2003-23-02 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of compliance — The specific action taken (inspected, replaced, modified) and to what revision.

Date — When the work was done.

Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.

Signature & certificate — The A&P/IA who returned it to service, with certificate number.

Is AD 2003-23-02 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.