Is AD 2017-05-06 a recurring Airworthiness Directive?

No — AD 2017-05-06 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2017-05-06 apply to?

AD 2017-05-06 applies to Boeing — models 767-200, 767-300, 767. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2017-05-06

one-time

Official AD 2017-05-06 · FR doc 2017-03964 · 2017-03-03 · airframe

Airworthiness Directives; The Boeing Company Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 767-200 and -300 series airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the frame-to-floor-beam joints and frames common to shear ties at certain locations of fuselage structure are subject to widespread fatigue damage (WFD). This AD requires inspections for cracking of certain frame inner chords and webs common to the floor beam joint and at frames common to the shear ties at certain sections, and corrective action if necessary. We are issuing this AD to address the unsafe condition on these products.

Which aircraft AD 2017-05-06 applies to

MakesBoeing

Models767-200, 767-300, 767

Installation of STC ST01920SE does not affect the ability to accomplish the AD actions; no 'change in product' AMOC approval is required for airplanes with this STC installed.

Whether AD 2017-05-06 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 2017-05-06 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.