Is AD 2007-24-13 a recurring Airworthiness Directive?

No — AD 2007-24-13 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2007-24-13 apply to?

AD 2007-24-13 applies to Cirrus — models SR22. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2007-24-13

one-time

Official AD 2007-24-13 · FR doc E7-23118 · 2007-11-29 · airframe

Airworthiness Directives; Cirrus Design Corporation Model SR22 Airplanes

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (Cirrus) Model SR22 airplanes. This AD requires you to install a drain hole in the left and right outboard wing tips. This AD results from reports of pilots' inability to move the aileron control without using excessive force when flying in freezing conditions. Moisture from a prior rain shower entered through a gap at the interface of the left and right outboard wing tips and wing structure. The moisture traveled along the aft wing shear web, accumulated below the aileron control pulley, and froze at an altitude with an outside air temperature below freezing. When this moisture is exposed to freezing conditions, operation of the aileron control pulley is impaired. We are issuing this AD to prevent moisture from accumulating along the wing shear web where it may freeze in certain conditions. This condition could result in operational failure of the aileron control pulley, which could lead to loss of control.

Which aircraft AD 2007-24-13 applies to

MakesCirrus

ModelsSR22

Serial-conditional — narrows to serials 2334–2334, 2420–2420, 2438–2749.

Pilots reported inability to move the aileron control without excessive force in freezing conditions; moisture entering at the wingtip/wing structure interface travels along the aft wing shear web, accumulates below the aileron control pulley, and freezes, impairing aileron control and potentially causing loss of control.

Whether AD 2007-24-13 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 2007-24-13 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.