Is AD 2008-14-15 a recurring Airworthiness Directive?

No — AD 2008-14-15 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2008-14-15

Q: Which aircraft does AD 2008-14-15 apply to?

AD 2008-14-15 applies to International Aero Engines — models V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5. Serial/part conditions may narrow it to specific aircraft.

one-time

Official AD 2008-14-15 · FR doc E8-15686 · 2008-07-16 · turbine engine

Airworthiness Directives; International Aero Engines AG (IAE) V2500 Series Turbofan Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for IAE V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, and V2528-D5 turbofan engines. This AD requires removing certain No. 4 bearing oil system components from service at the next shop visit or by an end date determined by the engine model. This AD results from instances of oil loss from the No. 4 bearing compartment. We are issuing this AD to prevent heat damage to high- pressure turbine (HPT) and low-pressure turbine (LPT) critical life limited hardware such as the HPT stage 1-2 airseal. Damage to the HPT stage 1-2 airseal could cause uncontained engine failure and damage to the airplane.

Which aircraft AD 2008-14-15 applies to

MakesInternational Aero Engines

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

Applies only to engines that have a specific part installed, identified by part number in the AD's part-number table (not included in the retrieved applicability excerpt). Installed on, but not limited to, Airbus A319/A320/A321 and McDonnell Douglas MD-90 airplanes.

Whether AD 2008-14-15 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 2008-14-15 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.