Is AD 2016-20-03 a recurring Airworthiness Directive?

Yes — AD 2016-20-03 requires a repetitive inspection. Next-due depends on the aircraft's time in service.

Which aircraft does AD 2016-20-03 apply to?

AD 2016-20-03 applies to Boeing — models 767-200, 767-300, 767-400ER, 767. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2016-20-03

recurring

Official AD 2016-20-03 · FR doc 2016-23076 · 2016-10-18 · airframe

Airworthiness Directives; The Boeing Company Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 767-200, -300, and -400ER series airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the skin lap splice is subject to widespread fatigue damage (WFD). This AD requires repetitive external detailed and surface high frequency eddy current (HFEC) inspections of the outer skin for cracking around fastener heads common to the inboard fastener row of the skin lap splice and corrective action. We are issuing this AD to detect and correct fatigue cracking of the skin lap splice, which could grow and result in possible rapid decompression and reduced structural integrity of the airplane.

Repetitive inspection. Re-inspect. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 2016-20-03 applies to

MakesBoeing

Models767-200, 767-300, 767-400ER, 767

As identified in Boeing Alert Service Bulletin 767-53A0260, dated August 26, 2014. Installation of STC ST01920SE does not affect the ability to accomplish the AD actions; no change-in-product AMOC approval is necessary for airplanes with STC ST01920SE installed.

Whether AD 2016-20-03 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 2016-20-03 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.