Is AD 2014-06632 a recurring Airworthiness Directive?

Yes — AD 2014-06632 requires a repetitive inspection. Next-due depends on the aircraft's time in service.

Which aircraft does AD 2014-06632 apply to?

AD 2014-06632 applies to Rolls-Royce Deutschland Ltd & Co Kg (Rrd) — models Tay 620-15, Tay 650-15, Tay 651-54, Tay. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2014-06632

recurring

AD 2014-06632 · 2014-04-03 · turbine engine

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Turbofan Engines

What this AD requires

We are superseding airworthiness directive (AD) 2007-03-02 for all Rolls-Royce Deutschland (RRD) Tay 620-15, Tay 650-15, and Tay 651- 54 turbofan engines. AD 2007-03-02 required an ultrasonic inspection (UI) of low-pressure (LP) compressor fan blades for cracks on certain serial number (S/N) Tay 650-15 engines. AD 2007-03-02 also required, for all Tay 611-8, 620-15, Tay 650-15, and Tay 651-54 engines, initial and repetitive UIs of LP compressor fan blades. AD 2007-03-02 also required, for Tay 650-15 and Tay 651-54 engines, UIs of LP compressor fan blades whenever the blade set is removed from one engine and installed on a different engine. This AD requires additional inspections for the affected engines and removal of the Tay 611-8 engine from the applicability. This AD was prompted by a report of an additional engine failure due to multiple fan blade separation. We are issuing this AD to prevent failure of the LP compressor fan blade, engine failure, 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 2014-06632 applies to

MakesRolls-Royce Deutschland Ltd & Co Kg (Rrd)

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

Part-conditional — M01100AA, M01100AB, M01300AA, M01300AB.

Applies to Tay 620-15 engines with low-pressure (LP) compressor module, part number M01100AA or M01100AB, installed; and Tay 650-15 and Tay 651-54 engines with LP compressor module, part number M01300AA or M01300AB, installed.

Whether AD 2014-06632 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

Supersession

Supersedes AD 2007-03-02.

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 2014-06632 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.