Is AD 2010-06-18 a recurring Airworthiness Directive?

No — AD 2010-06-18 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2010-06-18

Q: Which aircraft does AD 2010-06-18 apply to?

AD 2010-06-18 applies to International Aero Engines — models V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5. Serial/part conditions may narrow it to specific aircraft.

one-time

Official AD 2010-06-18 · FR doc 2010-5860 · 2010-03-18 · turbine engine

Airworthiness Directives; International Aero Engines (IAE) V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 Turbofan Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for IAE V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines. This AD requires a onetime fluorescent penetrant inspection of certain vortex reducers for cracks. This AD results from reports of fractured vortex reducers found at shop visits. We are issuing this AD to inspect for cracks in the vortex reducer. Cracks in the vortex reducer could result in an uncontained failure of the high-pressure (HP) compressor stage 3-8 drum and subsequent damage to the airplane.

Which aircraft AD 2010-06-18 applies to

MakesInternational Aero Engines

ModelsV2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2533-A5, V2500

Part-conditional — 6A4900, 6A5467, 6A6473, 6A7383, 6A7384, 6A7385, 6A7401.

Applies only to engines with high-pressure (HP) compressor stage 3-8 drum, P/N 6A4900, 6A5467, 6A6473, 6A7383, 6A7384, 6A7385, or 6A7401, installed.

Whether AD 2010-06-18 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 2010-06-18 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.