Is AD 2016-07-14 a recurring Airworthiness Directive?

No — AD 2016-07-14 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2016-07-14 apply to?

AD 2016-07-14 applies to Airbus — models A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2016-07-14

one-time

Official AD 2016-07-14 · FR doc 2016-07375 · 2016-04-11 · airframe

Airworthiness Directives; Airbus Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Airbus Model A319, A320, and A321 series airplanes. This AD is intended to complete certain mandated programs intended to support the airplane reaching its limit of validity (LOV) of the engineering data that support the established structural maintenance program. This AD was prompted by fatigue testing that determined fatigue damage could appear on clips, shear webs, and angles at certain rear fuselage sections and certain frames. This AD requires replacing the clips, shear webs, and angles, including doing all applicable related investigative actions, and repair if necessary. We are issuing this AD to prevent fatigue damage on the clips, shear webs, and angles; such damage could affect the structural integrity of the airplane.

Which aircraft AD 2016-07-14 applies to

MakesAirbus

ModelsA319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A319, A320, A321

Applies to all manufacturer serial numbers except those on which Airbus Modification 30975 has been embodied in production.

Whether AD 2016-07-14 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 2016-07-14 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.