Is AD 2010-23-06 a recurring Airworthiness Directive?

No — AD 2010-23-06 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2010-23-06

Q: Which aircraft does AD 2010-23-06 apply to?

AD 2010-23-06 applies to Mccauley Propeller Systems — models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, C5JFR36C1104/L114HCA-0. Serial/part conditions may narrow it to specific aircraft.

one-time

Official AD 2010-23-06 · FR doc 2010-27608 · 2010-11-03 · propeller

Airworthiness Directives; McCauley Propeller Systems Five-Blade Propeller Assemblies

What this AD requires

We are superseding an existing airworthiness directive (AD) for the products listed above. That AD currently requires removing certain propeller hubs from service at new, reduced life limits and eddy current inspections (ECIs) of the propeller hub. This new AD requires removing certain propeller hubs from service before they exceed 6,000 hours time-since-new (TSN). This AD was prompted by a report of a crack in a propeller hub. We are issuing this AD to prevent cracked propeller hubs, which could cause failure of the propeller hub, blade separation, and loss of control of the airplane.

Which aircraft AD 2010-23-06 applies to

MakesMccauley Propeller Systems

ModelsB5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, C5JFR36C1104/L114HCA-0

Installed on BAE Systems (Operations) Limited Jetstream Model 4100 series airplanes.

Whether AD 2010-23-06 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 2010-23-06 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.