Is AD 2007-10-05 a recurring Airworthiness Directive?

No — AD 2007-10-05 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2007-10-05 apply to?

AD 2007-10-05 applies to General Electric — models GE90-110B1, GE90-113B, GE90-115B, GE90. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2007-10-05

one-time

Official AD 2007-10-05 · FR doc E7-8990 · 2007-05-10 · turbine engine

Airworthiness Directives; General Electric Company (GE) GE90 Series Turbofan Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for GE GE90-110B1, -113B, and -115B series turbofan engines with certain Turbine Center Frames (TCFs) installed. This AD requires removing certain TCFs, listed by part number (P/N) in this AD, from service before exceeding 14,300 flight cycles. This AD results from a report that GE inadvertently omitted some TCF P/Ns from the Airworthiness Limitations Section (ALS) of the engine manual. We are issuing this AD to prevent structural failure of the TCF with uncontained failure of low pressure turbine (LPT) rotating parts. Uncontained failure of the LPT rotating parts could result in damage to the airplane and possible loss of control of the airplane.

Which aircraft AD 2007-10-05 applies to

MakesGeneral Electric

ModelsGE90-110B1, GE90-113B, GE90-115B, GE90

Part-conditional — 2061M60G09, 2061M60G22, 2061M60G23, 2061M60G24, 2061M60G26, 2061M60G27.

Applies only to engines with a Turbine Center Frame (TCF) bearing one of the listed part numbers installed. Installed on, but not limited to, Boeing 777-200LR and 777-300ER series airplanes.

Whether AD 2007-10-05 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 2007-10-05 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.