Is AD 2005-10-05 a recurring Airworthiness Directive?

No — AD 2005-10-05 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2005-10-05 apply to?

AD 2005-10-05 applies to Cfm International — models CFM56-5, CFM56-5B, CFM56-5C, CFM56. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2005-10-05

one-time

Official AD 2005-10-05 · FR doc 05-9275 · 2005-05-10 · turbine engine

Airworthiness Directives; CFM International CFM56-5, -5B, and -5C Series Turbofan Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for CFM International CFM56-5, -5B, and -5C series turbofan engines. This AD requires removing certain part number (P/N) air turbine starters from service. This AD results from several reports of uncontained failures of air turbine starters where high-energy particles were not contained within the containment feature of the starter. We are issuing this AD to prevent uncontained failures of air turbine starters, which could result in damage to the airplane.

Which aircraft AD 2005-10-05 applies to

MakesCfm International

ModelsCFM56-5, CFM56-5B, CFM56-5C, CFM56

Part-conditional — 3505582-24, 3505582-25, 3505582-40, 3505582-41, 3505582-42, 3505582-60, 3505582-61, 3505582-62.

Applies only to engines with the listed air turbine starter part numbers installed (cross-referenced VIN P/Ns: 301-807-004-0, 301-807-005-0, 301-781-203-0, 301-806-602-0, 301-806-802-0, 301-790-903-0, 301-806-702-0, 301-806-902-0). Installed on, but not limited to, Airbus A319, A320, A321, and A340 airplanes.

Whether AD 2005-10-05 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 2005-10-05 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.