Is AD 2001-06-12 a recurring Airworthiness Directive?

No — AD 2001-06-12 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2001-06-12 apply to?

AD 2001-06-12 applies to The Boeing Company — models 767. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2001-06-12

one-time

Official AD 2001-06-12 · FR doc 01-7701 · 2001-04-02 · airframe

Airworthiness Directives; Boeing Model 767 Series Airplanes Powered by General Electric Engines

What this AD requires

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 767 series airplanes powered by General Electric engines, that requires modification of the nacelle strut and wing structure. This amendment is prompted by reports indicating that the actual operational loads applied to the nacelle are higher than the analytical loads that were used during the initial design. Such an increase in loading can lead to fatigue cracking in the primary strut structure prior to an airplane reaching its design service objective. The actions specified by this AD are intended to prevent fatigue cracking in the primary strut structure and consequent reduced structural integrity of the strut.

Which aircraft AD 2001-06-12 applies to

MakesThe Boeing Company

Models767

Whether AD 2001-06-12 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 2001-06-12 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.