Is AD 2013-06174 a recurring Airworthiness Directive?

No — AD 2013-06174 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2013-06174 apply to?

AD 2013-06174 applies to Rolls-Royce Deutschland — models Spey 511-8, Spey 511. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2013-06174

one-time

AD 2013-06174 · 2013-03-20 · turbine engine

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

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Rolls-Royce Deutschland Ltd & Co KG (RRD) Spey 511-8 turbojet engines. This AD requires inspection and, if necessary, replacement of affected bolts and, if any bolt is found broken, inspection of the adjacent disc(s) for damage. This AD was prompted by a recent quality review determination that bolts with reduced material properties may have been installed in some engines. We are issuing this AD to prevent uncontained turbine disc fracture and damage to the airplane.

Which aircraft AD 2013-06174 applies to

MakesRolls-Royce Deutschland

ModelsSpey 511-8, Spey 511

Serial-conditional — narrows to serials 8847–8847, 8853–8853, 8879–8879, 8989–8989, 8994–8994, 9817–9817.

Applies only to the listed serial numbers with a date of last shop visit before November 15, 2007.

Whether AD 2013-06174 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 2013-06174 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.