Is AD 2014-16-10 a recurring Airworthiness Directive?

Yes — AD 2014-16-10 requires a repetitive inspection. Next-due depends on the aircraft's time in service.

Airworthiness Directive 2014-16-10

Q: Which aircraft does AD 2014-16-10 apply to?

AD 2014-16-10 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.

recurring

Official AD 2014-16-10 · FR doc 2014-19017 · 2014-08-19 · turbine engine

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

What this AD requires

We are superseding airworthiness directive (AD) 2013-12-01 for all Rolls-Royce plc (RR) model RB211 Trent 768-60, 772-60, and 772B-60 turbofan engines. AD 2013-12-01 required a one-time ultrasonic inspection (UI) of low-pressure (LP) compressor blades with more than 2,500 flight cycles since new or last inspection. This AD requires initial and repetitive UIs of the affected LP compressor blades. This AD was prompted by LP compressor blade partial airfoil release events. We are issuing this AD to prevent LP compressor blade airfoil separations, damage to the engine, 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 2014-16-10 applies to

MakesRolls-Royce Plc

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

Part-conditional — FK23411, FK25441, FK25968, FW11901, FW15393, FW23643, FW23741, FW23744.

Applies only when low-pressure (LP) compressor blade P/N FK23411, FK25441, FK25968, FW11901, FW15393, FW23643, FW23741, FW23744, KH23403, or KH23404 is installed.

Whether AD 2014-16-10 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 2014-16-10 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.