Is AD 2013-02-05 a recurring Airworthiness Directive?

No — AD 2013-02-05 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2013-02-05 apply to?

AD 2013-02-05 applies to Boeing — models -600, -700, -700C, -800, -900, -900ER, 737. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2013-02-05

one-time

Official AD 2013-02-05 · FR doc 2013-01720 · 2013-01-30 · airframe

Airworthiness Directives; the Boeing Company

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 requires, for certain airplanes, installing two warning level indicator lights on each of the P1-3 and P3-1 instrument panels in the flight compartment. This AD also requires, for certain airplanes, replacing the existing P5-16 and P5-10 panels; and, for certain airplanes, replacing the basic P5-16 panel with a high altitude landing P5-16 panel. Additionally, this AD requires revising the airplane flight manual to remove certain requirements of previous AD actions, and to advise the flightcrew of certain changes. This AD was prompted by a design change in the cabin altitude warning system that would address the identified unsafe condition. We are issuing this AD to prevent failure of the flightcrew to recognize and react to a valid cabin altitude warning horn, which could result in incapacitation of the flightcrew due to hypoxia (a lack of oxygen in the body), and consequent loss of control of the airplane.

Which aircraft AD 2013-02-05 applies to

MakesBoeing

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

Applicability limited to airplanes identified in Boeing Alert Service Bulletin 737-31A1332, Revision 3, dated March 28, 2012.

Whether AD 2013-02-05 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 2013-02-05 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.