Airworthiness Directive 2000-11-08

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Official AD 2000-11-08 · FR doc 00-13447 · 2000-06-01 · airframe

Airworthiness Directives; Boeing Model 747 and 767 Series Airplanes Powered by General Electric Model CF6-80C2 Series Engines

What this AD requires

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 747 and 767 series airplanes, that currently requires revising the FAA-approved Airplane Flight Manual (AFM) to prohibit the use of certain fuels; and either replacing an existing placard with a new placard, or replacing all dribble flow fuel nozzles (DFFN) with standard fuel nozzles, which terminates the requirements for the new placard and AFM revision. This amendment continues these requirements and adds identical requirements applicable to airplanes on which standard fuel nozzles are not installed. This amendment is prompted by a report of an engine flameout due to use of JP-4 or Jet B fuel during certification testing on an engine with DFFN's installed. The actions specified by this AD are intended to prevent such engine flameouts and consequent engine shutdown.

Which aircraft AD 2000-11-08 applies to

MakesBoeing
Models747, 767
Part-conditional9331M72P33, 9331M72P34, 9331M72P41.

Applies to Model 747 series and Model 767 series airplanes on which a dribble flow fuel nozzle (DFFN) having General Electric P/N 9331M72P33, 9331M72P34, or 9331M72P41 is installed on any engine in a specific operator's fleet, per Boeing Alert Service Bulletin 747-11A2052 (or Rev 1) for Model 747 series airplanes, and Boeing Alert Service Bulletin 767-11A0031 (or Rev 1) for Model 767 series airplanes. Restatement of requirements of AD 98-08-23; requires AFM revision and either placarding or DFFN replacement to prohibit/prevent use of JP-4 and Jet B fuel.

Whether AD 2000-11-08 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2000-11-08 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.