Is AD 2000-06-01 a recurring Airworthiness Directive?

No — AD 2000-06-01 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2000-06-01 apply to?

AD 2000-06-01 applies to Cessna. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2000-06-01

one-time

Official AD 2000-06-01 · FR doc 00-6615 · 2000-03-22 · airframe

Airworthiness Directives; Cessna Aircraft Company 150, 152, 172, 177, 180, 182, 185, 188, 206, 207, 210, and 337 Series Airplanes

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to Cessna Aircraft Company (Cessna) 150, 152, 172, 177, 180, 182, 185, 188, 206, 207, 210, and 337 series airplanes. This AD requires measuring the visible length of standpipe (tube) in the top assembly of the fuel strainer assembly for the correct length, and replacing any fuel strainer assembly that does not have the correct length of standpipe. This AD is the result of reports that the fuel strainer assemblies on the affected airplanes were manufactured with the fuel standpipes incorrectly installed in the assembly housing top. The actions specified by this AD are intended to prevent foreign material from entering the fuel system and engine, which could result in loss of engine power or complete engine stoppage during flight.

Which aircraft AD 2000-06-01 applies to

MakesCessna

Part-conditional — 0756005-2, 0756005-8, 0756005-9.

Applies to Cessna single- and multi-engine airplanes with a fuel strainer top assembly/fuel strainer assembly (P/N 0756005-2, -8, or -9) installed after December 12, 1996; units shipped between 12/12/1996 and 9/5/1997 may have an undersized internal standpipe that can loosen and dislodge.

Whether AD 2000-06-01 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 2000-06-01 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.