Is AD 2011-03-15 a recurring Airworthiness Directive?

No — AD 2011-03-15 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2011-03-15 apply to?

AD 2011-03-15 applies to Boeing — models 767-200, 767-300, 767-300F, 767-400ER, 767. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2011-03-15

one-time

Official AD 2011-03-15 · FR doc 2011-2515 · 2011-02-15 · airframe

Airworthiness Directives; The Boeing Company Model 767 Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Model 767 airplanes. This AD requires doing a detailed inspection for correct main track downstop assembly, thread protrusion, and damaged and missing parts of the main track downstop assemblies of the outboard slats, and related investigative and corrective actions if necessary. This AD also requires doing a detailed inspection for foreign objects, debris and damage to the wall of the track housing of the outboard slats, and corrective actions if necessary. This AD results from reports of broken bolts in the outboard slat main track downstop assembly. We are issuing this AD to detect and correct incorrectly installed main track downstop assemblies, which can allow the main track downstop hardware to fall into the track housing and cause a puncture in the track housing when the slat is retracted. This condition, if not corrected, could result in a fuel leak and an increased risk of fire.

Which aircraft AD 2011-03-15 applies to

MakesBoeing

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

Applies to airplanes identified in Boeing Special Attention Service Bulletin 767-57-0118, Revision 1, dated October 21, 2010.

Whether AD 2011-03-15 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 2011-03-15 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.