Airworthiness Directive 2012-24-07

one-time
Official AD 2012-24-07 · FR doc 2012-29405 · 2012-12-05 · 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 787-8 airplanes. This AD requires ensuring that lockwire is installed correctly on the engine fuel feed manifold couplings. This AD also requires inspecting the assembly of the engine fuel feed manifold rigid and full flexible couplings. This AD was prompted by reports of fuel leaks due to improperly assembled engine fuel feed manifold couplings. We are issuing this AD to detect and correct improperly assembled couplings, which could result in fuel leaks and consequent fuel exhaustion, engine power loss or shutdown, or leaks on hot engine parts that could lead to a fire.

Which aircraft AD 2012-24-07 applies to

MakesBoeing
Models787-8, 787
Serial-conditional — narrows to serials 34485–34485, 34486–34486, 34488–34488, 34490–34490, 34493–34493, 34494–34494, 34497–34497, 34502–34502, 34506–34508, 34514–34514, 34515–34515, 34521–34521, 34744–34747, 34822–34822, 34824–34824, 34829–34829, 34832–34832, 34834–34838, 35938–35938, 36276–36278, 38319–38319, 38320–38320, 38330–38330, 38466–38466, 38471–38471, 40748–40748, 40899–40899.

Limited to the specific serial numbers listed, not all 787-8 airplanes.

Whether AD 2012-24-07 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2012-24-07 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.