Is AD 2013-24-10 a recurring Airworthiness Directive?

No — AD 2013-24-10 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2013-24-10 apply to?

AD 2013-24-10 applies to Boeing — models 757-200, 757-200PF, 757-200CB, 757-300, 767-200, 767-300, 767-300F, 767-400ER. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2013-24-10

one-time

Official AD 2013-24-10 · FR doc 2013-28441 · 2013-12-03 · 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 and Model 767 airplanes. This AD was prompted by a standby power relay failure and subsequent illumination of the "STANDBY BUS OFF" light, which led the flightcrew to set the standby power switch to the "BAT" position, isolating the battery and standby buses, disabling the battery charger, and eventually causing the main battery to be depleted. This AD requires doing wiring changes and installing a new air/ground relay to the battery charger system. We are issuing this AD to prevent discharge of the main battery, which could result in multiple system degradation, reduced airplane controllability, and runway excursion upon landing.

Which aircraft AD 2013-24-10 applies to

MakesBoeing

Models757-200, 757-200PF, 757-200CB, 757-300, 767-200, 767-300, 767-300F, 767-400ER, 757, 767

Model 757 series identified in Boeing Special Attention Service Bulletin 757-24-0132, Revision 1, dated June 19, 2012; Model 767 series identified in Boeing Special Attention Service Bulletin 767-24-0200, Revision 1, dated September 13, 2012. Installation of STC ST01920SE or STC ST01518SE does not affect applicability/ability to accomplish the required actions.

Whether AD 2013-24-10 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 2013-24-10 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.