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Airworthiness Directive 2012-19-05

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Official AD 2012-19-05 · FR doc 2012-23055 · 2012-09-24 · 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 reports of burned contacts in a certain production break plug and its corresponding receptacle. This AD requires modifying galley power supply wiring by disconnecting it from the affected plug/ receptacle and reconnecting the power supply wiring through splices. We are issuing this AD to prevent a high electrical load, which might lead to overheating of the galley power supply wiring and/or the electrical connector and consequent smoke or fire in the galley area, which could result in damage to the airplane and injury to occupants.

Which aircraft AD 2012-19-05 applies to

MakesFokker Services B.V.
ModelsF.28 Mark 0070, F.28 Mark 0100, F.28
Serial-conditional — narrows to serials 11340–11343, 11347–11347, 11348–11348, 11350–11356, 11359–11359, 11360–11360, 11361–11361, 11367–11371, 11374–11378, 11382–11385, 11387–11390, 11394–11397, 11400–11423, 11425–11432, 11434–11439, 11441–11453, 11456–11585.

Whether AD 2012-19-05 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 2012-19-05 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.