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

No — AD 2013-19-03 is a one-time directive. Verify it was complied with in the aircraft's records.

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

AD 2013-19-03 applies to Boeing — models 737-600, 737-700, 737-700C, 737-800, 737-900, 737-900ER, 737. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2013-19-03

one-time

Official AD 2013-19-03 · FR doc 2013-23464 · 2013-09-30 · 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 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD was prompted by a report of chafing damage to a wire bundle that was arcing to hydraulic tubing and caused by insufficient separation between the wire bundle and the hydraulic tubing in the main landing gear (MLG) wheel well. This AD requires an inspection for damage of wire bundles and hydraulic tubing on the right side of the forward bulkhead of the MLG wheel well; installation of new clamps; and corrective actions, as applicable. We are issuing this AD to detect and correct possible damage caused by insufficient separation between the wire bundles and hydraulic tubing to prevent electrical arcing in a flammable fluid leakage zone, which could lead to a wheel well fire.

Which aircraft AD 2013-19-03 applies to

MakesBoeing

Models737-600, 737-700, 737-700C, 737-800, 737-900, 737-900ER, 737

Serial-conditional — narrows to serials 1060–3289.

Applies to line numbers (L/Ns) 1060 through 3289 inclusive, and 3294, excluding L/Ns 3138, 3158, 3169, 3175, 3216, 3224, 3253, and 3274. Installation of STC ST00830SE does not affect the ability to accomplish the actions required by this AD; a change-in-product AMOC approval request is not necessary for airplanes on which STC ST00830SE is installed.

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