Is AD 2007-24-06 a recurring Airworthiness Directive?

No — AD 2007-24-06 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2007-24-06 apply to?

AD 2007-24-06 applies to Sma — models 1, SR305-230. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2007-24-06

one-time

Official AD 2007-24-06 · FR doc E7-22812 · 2007-11-28 · reciprocating engine

Airworthiness Directives; Societe de Motorisations Aeronautiques (SMA) SR305-230 and SR305-230-1 Reciprocating Engines

What this AD requires

We are superseding an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) provided by the European Aviation Safety Agency (EASA) to identify and correct an unsafe condition on SMA SR305-230 and SR305-230-1 reciprocating engines. The MCAI states the following:

Which aircraft AD 2007-24-06 applies to

MakesSma

Models1, SR305-230

Part-conditional — SF01160009-0, SF01160011-0, SP01160013, SP01160051-0, SP01160051-1, SP01160051-2, SP01160051-3, SP01160051-4.

Applies only to engines equipped with an electronic control unit (ECU) having one of the listed part numbers; engines installed on Cessna 182 series airplanes with Supplemental Type Certificate SA03302AT applied.

Whether AD 2007-24-06 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 2007-24-06 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.