Is AD 2005-03-06 a recurring Airworthiness Directive?

Yes — AD 2005-03-06 requires a repetitive inspection every 2000 hours. Next-due depends on the aircraft's time in service.

Which aircraft does AD 2005-03-06 apply to?

AD 2005-03-06 applies to Rolls-Royce Deutschland Ltd. & Co Kg — models Tay 611-8, Tay 620-15, Tay 650-15, Tay 651-54, Tay. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2005-03-06

recurring

Official AD 2005-03-06 · FR doc 05-2370 · 2005-02-10 · turbine engine

Airworthiness Directives; Rolls-Royce Deutschland Ltd. & Co KG (formerly Rolls-Royce plc), Model Tay 611-8, 620-15, 650-15, and 651-54 Turbofan Engines

What this AD requires

The FAA is superseding an existing airworthiness directive (AD) for Rolls-Royce Deutschland Ltd. & Co KG (RRD) (formerly Rolls- Royce plc) Model Tay 611-8, 620-15, 650-15, and 651-54 turbofan engines, with low pressure (LP) fuel tube, part number (P/N) JR33021A, installed. That AD currently requires initial and repetitive inspections of the LP fuel tubes. This AD requires the same inspections and adds a requirement to replace the fuel tube with a new design tube, as mandatory terminating action to the repetitive inspections. This AD results from the manufacturer introducing a new design fuel tube, which eliminates the unsafe condition. We are issuing this AD to prevent a dual-engine flameout due to fuel exhaustion, which could lead to forced landing and possible damage to the airplane.

Repetitive inspection. Re-inspect every 2000 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 2005-03-06 applies to

MakesRolls-Royce Deutschland Ltd. & Co Kg

ModelsTay 611-8, Tay 620-15, Tay 650-15, Tay 651-54, Tay

Part-conditional — JR33021A.

Applies only to engines with low pressure (LP) fuel tube, part number JR33021A, installed. These engines are installed on, but not limited to, Fokker F.28 Mark 0100 airplanes (STC SA842SW), Boeing 727 airplanes, and Gulfstream G-IV airplanes.

Whether AD 2005-03-06 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 2005-03-06 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.