Is AD 2012-06-06 a recurring Airworthiness Directive?

No — AD 2012-06-06 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2012-06-06 apply to?

AD 2012-06-06 applies to Boeing — models 757-200, 757-200PF, 757-200CB, 757-300, 757. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2012-06-06

one-time

Official AD 2012-06-06 · FR doc 2012-6642 · 2012-04-05 · airframe

Airworthiness Directives; The Boeing Company Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 757 airplanes. This AD requires replacing the power control relays for the fuel boost pumps and override pumps with new relays having a ground fault interrupter (GFI) feature. This AD also requires an electrical bonding resistance measurement for certain GFI relays to verify that certain bonding requirements are met. This AD also requires, for certain airplanes, an inspection to ensure that certain screws are properly installed, and installing longer screws if necessary. This AD was prompted by fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent damage to the fuel pumps caused by electrical arcing that could introduce an ignition source in the fuel tank, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.

Which aircraft AD 2012-06-06 applies to

MakesBoeing

Models757-200, 757-200PF, 757-200CB, 757-300, 757

Applies to airplanes as identified in the applicable service bulletin: Boeing Service Bulletin 757-28A0078, Revision 2, dated January 11, 2012, for Model 757-200/-200PF/-200CB; or Boeing Service Bulletin 757-28A0079, Revision 2, dated January 11, 2012, for Model 757-300.

Whether AD 2012-06-06 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 2012-06-06 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.