Is AD 2005-14-09 a recurring Airworthiness Directive?

No — AD 2005-14-09 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2005-14-09

Q: Which aircraft does AD 2005-14-09 apply to?

AD 2005-14-09 applies to Rolls-Royce Plc — models RB211 Trent 768-60, RB211 Trent 772-60, RB211 Trent 772B-60, RB211 Trent. Serial/part conditions may narrow it to specific aircraft.

one-time

Official AD 2005-14-09 · FR doc 05-13425 · 2005-07-08 · turbine engine

Airworthiness Directives; Rolls-Royce plc Models RB211 Trent 768-60, Trent 772-60, and Trent 772B-60 Turbofan Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce plc (RR) models RB211 Trent 768-60, Trent 772-60, and Trent 772B-60 turbofan engines. This AD requires removal of certain Engine Electronic Controller (EEC) part numbers from service. This AD results from nine reports of loss of engine parameters displayed in the airplane cockpit, with the simultaneous loss of capability to change thrust of the affected engine. We are issuing this AD to prevent loss of airplane control after an aborted takeoff due to asymmetric thrust.

Which aircraft AD 2005-14-09 applies to

MakesRolls-Royce Plc

ModelsRB211 Trent 768-60, RB211 Trent 772-60, RB211 Trent 772B-60, RB211 Trent

Part-conditional — EEC2000.06.BB.1, EEC2000-06-BE-1, EEC2000-06-BG-1, EEC2000-06-BH-1, EEC2000-06-BL-1, EEC2000-06-BM-1, EEC2000.07.BB.1, EEC2000-07-BE-1.

Applies only to engines with the listed Engine Electronic Controller (EEC) part numbers installed. These engines are installed on, but not limited to, Airbus A330 series airplanes.

Whether AD 2005-14-09 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 2005-14-09 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.