Is AD 2014-07-05 a recurring Airworthiness Directive?

No — AD 2014-07-05 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2014-07-05 apply to?

AD 2014-07-05 applies to Fokker — models F.28 Mark 0070, F.28 Mark 0100, F.28. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2014-07-05

one-time

Official AD 2014-07-05 · FR doc 2014-07821 · 2014-04-16 · airframe

Airworthiness Directives; Fokker Services B.V. Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the butt-joints on the forward fuselage above the passenger door are subject to widespread fatigue damage (WFD). This AD requires inspecting the forward fuselage butt-joints for cracking, repairing any crack, and eventually doing a terminating repair. We are issuing this AD to prevent fatigue cracking of such butt-joints, which could result in reduced structural integrity of the airplane and in- flight decompression of the airplane.

Which aircraft AD 2014-07-05 applies to

MakesFokker

ModelsF.28 Mark 0070, F.28 Mark 0100, F.28

Applies only to airplanes identified in Fokker Service Bulletin SBF100-53-118, Revision 2, dated October 16, 2012.

Whether AD 2014-07-05 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 2014-07-05 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.