Is AD 2000-15-10 a recurring Airworthiness Directive?

Yes — AD 2000-15-10 requires a repetitive inspection every 600 hours. Next-due depends on the aircraft's time in service.

Which aircraft does AD 2000-15-10 apply to?

AD 2000-15-10 applies to Mccauley — models 4HFR34C653/L106FA-0, 4HFR34. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2000-15-10

recurring

Official AD 2000-15-10 · FR doc 00-19665 · 2000-08-08 · propeller

Airworthiness Directives; McCauley Propeller Model 4HFR34C653/L106FA-0

What this AD requires

This amendment adopts a new airworthiness directive (AD) that is applicable to McCauley Propeller Systems 4HFR34C653/L106FA-0 model propellers that are installed on Jetstream Series 3200 airplanes. This action is also applicable to 4HFR34C653/L106FA-0 model propellers that are installed on Ayres S2R-G5 and S2R-G10 airplanes if the propeller was previously installed on Jetstream Series 3200 airplanes or if installation history of the propeller is unknown. This action requires one-time and repetitive eddy current inspections of the camber side of the blade surface. This amendment is prompted by a report of a crack on the camber side of the blade surface. The crack was found during a dye penetrant inspection as part of a normal overhaul process. The actions specified in this AD are intended to detect cracks that could cause failure of the propeller blade, which can result in loss of control of the airplane.

Repetitive inspection. Re-inspect every 600 hours. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 2000-15-10 applies to

MakesMccauley

Models4HFR34C653/L106FA-0, 4HFR34

Applies to 4HFR34C653/L106FA-0 model propellers installed on Jetstream Series 3200 airplanes; and to the same propeller model installed on Ayres S2R-G5 and S2R-G10 airplanes if the propeller was previously installed on a Jetstream Series 3200 airplane, or if the propeller's installation history is unknown. Applies to each propeller identified regardless of prior modification/alteration/repair in the affected area.

Whether AD 2000-15-10 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 2000-15-10 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.