Is AD 2006-15-13 a recurring Airworthiness Directive?

No — AD 2006-15-13 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2006-15-13

Q: Which aircraft does AD 2006-15-13 apply to?

AD 2006-15-13 applies to Mccauley Propeller Systems — models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, C5JFR36C1104/L114HCA-0, B5JFR36C1101/114GCA, C5JFR36C1102/L114GCA, B5JFR36C1103/114HCA, C5JFR36C1104/L114HCA. Serial/part conditions may narrow it to specific aircraft.

one-time

Official AD 2006-15-13 · FR doc E6-11799 · 2006-07-26 · propeller

Airworthiness Directives; McCauley Propeller Systems Propeller Models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for McCauley Propeller Systems propeller models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/ L114HCA-0. This AD requires a onetime fluorescent penetrant inspection (FPI) and eddy current inspection (ECI) of propeller blades for cracks, and if any crack indications are found, removing the blade from service. This AD results from a report of two propeller blades on the same propeller assembly, found cracked during propeller overhaul. We are issuing this AD to detect cracks in the propeller blade that could cause failure and separation of the propeller blade and loss of control of the airplane.

Which aircraft AD 2006-15-13 applies to

MakesMccauley Propeller Systems

ModelsB5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, C5JFR36C1104/L114HCA-0, B5JFR36C1101/114GCA, C5JFR36C1102/L114GCA, B5JFR36C1103/114HCA, C5JFR36C1104/L114HCA

Installed on BAE Systems (Operations) Limited Jetstream Model 4100 and 4101 series airplanes (Jetstream 41).

Whether AD 2006-15-13 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 2006-15-13 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.