Is AD 2013-03-19 a recurring Airworthiness Directive?

Yes — AD 2013-03-19 requires a repetitive inspection every 15000 hours. Next-due depends on the aircraft's time in service.

Which aircraft does AD 2013-03-19 apply to?

AD 2013-03-19 applies to Boeing — models -100 long body, -200, -100B long body, -100B short body, -300, -300B, -300C, -400. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2013-03-19

recurring

Official AD 2013-03-19 · FR doc 2013-03267 · 2013-02-14 · airframe

Airworthiness Directives; The Boeing Company Airplanes

What this AD requires

We are superseding an existing airworthiness directive (AD) for certain The Boeing Company Model 707 airplanes, and Model 720 and 720B series airplanes. That AD currently requires replacing wiring for the fuel boost pumps and override pumps with new wiring, installing Teflon sleeving on the wiring, and doing associated actions; and doing repetitive inspections to detect damage of the wiring or evidence of a fuel leak. This new AD reduces the repetitive inspection interval. This AD was prompted by a determination that an inspection interval must be reduced. We are issuing this AD to detect and correct damaged wiring for the fuel boost pumps and override pumps, which could cause electrical arcing that could puncture the conduit containing the wire, and result in a fuel tank explosion or a fire adjacent to the fuel tank.

Repetitive inspection. Re-inspect every 15000 hours. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 2013-03-19 applies to

MakesBoeing

Models-100 long body, -200, -100B long body, -100B short body, -300, -300B, -300C, -400, 720B, 707, 720

Serial-conditional — narrows to serials 1–941.

Range given in the AD as line numbers 1 through 941 inclusive (not serial numbers).

Whether AD 2013-03-19 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 2013-03-19 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.