Airworthiness Directive 2010-16-04

one-time
Official AD 2010-16-04 · FR doc 2010-18623 · 2010-08-05 · airframe

Airworthiness Directives; The Boeing Company Model 767-200, -300, and -300F Series Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Model 767-200, -300, and -300F series airplanes. This AD requires inspecting to verify the part number of the low-pressure flex-hoses of the flightcrew and supernumerary oxygen system installed under the oxygen mask stowage box at flightcrew and supernumerary oxygen mask locations, and replacing the flex-hose with a new non-conductive low- pressure flex-hose if necessary. This AD results from reports of low- pressure flex-hoses of the flightcrew oxygen system that burned through due to inadvertent electrical current from a short circuit in an adjacent audio select panel. We are issuing this AD to prevent inadvertent electrical current, which can cause the low-pressure flex- hoses used in the flightcrew and supernumerary oxygen systems to melt or burn, resulting in oxygen system leakage and smoke or fire.

Which aircraft AD 2010-16-04 applies to

MakesBoeing
Models767-200, 767-300, 767-300F, 767
Serial-conditional — narrows to serials 1–763.

Range given is manufacturer line numbers 1 through 763 inclusive (not aircraft serial numbers), except line number 758 which was accomplished in production and is excluded.

Whether AD 2010-16-04 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 2010-16-04 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.