Is AD 2013-11-07 a recurring Airworthiness Directive?

Yes — AD 2013-11-07 requires a repetitive inspection. Next-due depends on the aircraft's time in service.

Airworthiness Directive 2013-11-07

Q: Which aircraft does AD 2013-11-07 apply to?

AD 2013-11-07 applies to Embraer — models ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 ECJ, ERJ 190-100 IGW, ERJ 190-200 STD, ERJ 190-200 LR, ERJ 190-200 IGW, ERJ 190. Serial/part conditions may narrow it to specific aircraft.

recurring

Official AD 2013-11-07 · FR doc 2013-12900 · 2013-06-04 · airframe

Airworthiness Directives; Embraer S.A. Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Embraer S.A. Model ERJ 190 airplanes. This AD was prompted by reports of cracks on the side stay of the main landing gear (MLG). This AD requires repetitive measurements of the left-hand (LH) and right-hand (RH) MLG side stay support fitting to detect bushing migration, and eventual replacement of the bushing; and a detailed inspection for damage on the LH and RH MLG side stay support assembly, and related investigative and corrective actions if necessary. We are issuing this AD to prevent excessive bearing friction, which might compromise the MLG free fall extension and cause fatigue cracking on the MLG side stay and on its support assembly, resulting in reduced structural integrity of the MLG.

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 2013-11-07 applies to

MakesEmbraer

ModelsERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 ECJ, ERJ 190-100 IGW, ERJ 190-200 STD, ERJ 190-200 LR, ERJ 190-200 IGW, ERJ 190

As identified in EMBRAER Service Bulletin 190-57-0036, Revision 02, dated August 12, 2011, and EMBRAER Service Bulletin 190LIN-57-0016, dated June 10, 2011.

Whether AD 2013-11-07 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 2013-11-07 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.