Is AD 2000-03-09 a recurring Airworthiness Directive?

No — AD 2000-03-09 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2000-03-09 apply to?

AD 2000-03-09 applies to Cessna — models 560. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2000-03-09

one-time

Official AD 2000-03-09 · FR doc 00-3532 · 2000-02-28 · airframe

Airworthiness Directives; Cessna Model 560 Series Airplanes

What this AD requires

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Cessna Model 560 series airplanes, that currently requires revising the FAA-approved Airplane Flight Manual (AFM) to provide the flightcrew with limitations, operational procedures, and performance information to be used during approach and landing when residual ice is present or can be expected. This amendment is prompted by reports indicating that, while operating in icing conditions or when ice is on the wings, some of these airplanes have experienced uncommanded roll at (or slightly higher than) the speed at which the stall warning system is activated. This amendment requires revising the AFM and revises the applicability of the existing AD. This amendment also requires modification of the stall warning system of the angle-of-attack computer. The actions specified by this AD are intended to prevent uncommanded roll of the airplane during approach and landing when residual ice is present or can be expected.

Which aircraft AD 2000-03-09 applies to

MakesCessna

Models560

Serial-conditional — narrows to serials 560-0001–560-0259, 560-0260–560-0437.

Part-conditional — C11606-2, C11606-3.

S/N 560-0001 through 560-0259 = Citation V; S/N 560-0260 through 560-0437 = Citation V Ultra. AD addresses stall warning/angle-of-attack system and prohibits installing an angle-of-attack computer with P/N C11606-2 or C11606-3.

Whether AD 2000-03-09 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 2000-03-09 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.