Is AD 2007-05-14 a recurring Airworthiness Directive?

No — AD 2007-05-14 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2007-05-14

Q: Which aircraft does AD 2007-05-14 apply to?

AD 2007-05-14 applies to General Electric — models CF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2A8, CF6-80C2A5F, CF6-80C2B1, CF6-80C2B2. Serial/part conditions may narrow it to specific aircraft.

one-time

Official AD 2007-05-14 · FR doc 07-986 · 2007-03-05 · turbine engine

Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for GE CF6-80C2 series turbofan engines. This AD requires replacing certain installed part number (P/N) and serial number (SN) cast titanium weld- repaired forward engine mount platforms and cast titanium forward mount yokes, with a forged titanium or a non-welded cast titanium part. This AD results from the discovery of cracks, in a weld-repaired area on a forward engine mount platform and a forward engine mount yoke, found during a fluorescent penetrant inspection (FPI). These parts were weld- repaired during manufacture. We are issuing this AD to prevent cracks in the forward engine mount platform and forward engine mount yoke that could result in possible separation of the engine from the airplane.

Which aircraft AD 2007-05-14 applies to

MakesGeneral Electric

ModelsCF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2A8, CF6-80C2A5F, CF6-80C2B1, CF6-80C2B2, CF6-80C2B4, CF6-80C2B6, CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F, CF6-80C2B5F, CF6-80C2B6F, CF6-80C2B6FA, CF6-80C2B7F, CF6-80C2B8F, CF6-80C2D1F, CF6-80C2

Part-conditional — 1292M13G06, 1301M28G08, 1459M70G07, 1846M24G04, 9383M43G14, 9383M43G16.

Applies only when a listed cast titanium engine mount platform P/N or engine mount yoke P/N is installed on the affected CF6-80C2 engine models. Installed on but not limited to Boeing 747, Boeing 767, MD-11, and Airbus A300-600 and A310 airplanes.

Whether AD 2007-05-14 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 2007-05-14 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.