Is AD 2010-19-01 a recurring Airworthiness Directive?

Yes — AD 2010-19-01 requires a repetitive inspection. Next-due depends on the aircraft's time in service.

Which aircraft does AD 2010-19-01 apply to?

AD 2010-19-01 applies to Rolls-Royce Corporation (Rrc) — models AE 3007A. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2010-19-01

recurring

Official AD 2010-19-01 · FR doc 2010-22370 · 2010-09-22 · turbine engine

Airworthiness Directives; Rolls-Royce Corporation (RRC) AE 3007A Series Turbofan Engines

What this AD requires

The FAA is superseding an existing airworthiness directive (AD) for RRC AE 3007A series turbofan engines. That AD currently requires performing an eddy current inspection (ECI) or surface wave ultrasonic test (SWUT) inspection on each affected high-pressure turbine (HPT) wheel. This AD requires removing or performing initial and repetitive ECIs or SWUT inspections on HPT stage 2 wheels for cracks. This AD also reduces the approved life limits of certain HPT stage 2 wheels. This AD results from reports of cracked HPT stage 2 wheels. We are issuing this AD to prevent uncontained failure of the HPT stage 2 wheel and damage to the airplane.

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

Which aircraft AD 2010-19-01 applies to

MakesRolls-Royce Corporation (Rrc)

ModelsAE 3007A

Part-conditional — 23069438, 23069592, 23074462, 23074644, 23075345, 23084520.

Applies only to AE 3007A series turbofan engines with a high-pressure turbine (HPT) stage 2 wheel of one of the listed part numbers installed. Installed on, but not limited to, EMBRAER EMB-135 and EMB-145 airplanes.

Whether AD 2010-19-01 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 2010-19-01 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.