Is AD 2015-02-26 a recurring Airworthiness Directive?

No — AD 2015-02-26 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2015-02-26 apply to?

AD 2015-02-26 applies to Boeing — models 737-100, 737-200, 737-200C, 737-300, 737-400, 737-500, 737-600, 737-700. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2015-02-26

one-time

Official AD 2015-02-26 · FR doc 2015-02074 · 2015-02-04 · airframe

Airworthiness Directives; The Boeing Company Airplanes

What this AD requires

We are superseding Airworthiness Directive (AD) 2013-24-13 for certain The Boeing Company Model 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, and -900 series airplanes. AD 2013-24-13 required replacing the pivot link assembly for certain airplanes, replacing the seat track link assemblies or modifying the existing seat track link assembly for certain airplanes, or modifying the existing seat track link assembly fastener for certain other airplanes. AD 2013-24-13 also required inspecting, changing, or repairing the seat track link assembly for certain other airplanes. Since we issued AD 2013-24-13, a certain paragraph reference in that AD was found to be mis-identified; this AD corrects this paragraph reference. We are issuing this AD to prevent seat detachment in an emergency landing, which could cause injury to occupants of the passenger compartment and affect emergency egress.

Which aircraft AD 2015-02-26 applies to

MakesBoeing

Models737-100, 737-200, 737-200C, 737-300, 737-400, 737-500, 737-600, 737-700, 737-700C, 737-800, 737-900, 737

Applicability defined by inclusion in Boeing Special Attention SB 737-53-1260 Rev 1 (Classic series -100/-200/-200C/-300/-400/-500) and SB 737-53-1244 Rev 5 (NG series -600/-700/-700C/-800/-900)

Whether AD 2015-02-26 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 2015-02-26 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.