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Airworthiness Directive 2004-15-03

recurring
Official AD 2004-15-03 · FR doc 04-17040 · 2004-07-30 · turbine engine

Airworthiness Directives; General Electric Company CF34-3A1 and -3B1 Series Turbofan Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF34-3A1 and -3B1 series turbofan engines with certain serial numbers (SNs) of stage 5 low pressure turbine (LPT) disks, part number (P/N) 6078T92P01, and or certain SNs of stage 6 LPT disks, P/N 6089T89P01. This AD requires initial and repetitive visual and eddy current inspections of those disks. This AD also allows as optional terminating action to the repetitive inspections, replacement of those SN disks. This AD also requires replacement of certain stage 5 and stage 6 LPT disks. This AD results from a report of a stage 5 LPT disk that failed due to cracking from low-cycle-fatigue (LCF) during factory testing. We are issuing this AD to prevent LCF failure of stage 5 LPT disks and stage 6 LPT disks, which could lead to uncontained engine failure.

Repetitive inspection. Re-inspect every 9 months. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 2004-15-03 applies to

MakesGeneral Electric
ModelsCF34-3A1, CF34-3B1, CF34
Part-conditional — 6078T92P01, 6089T89P01.

Applies only to engines with stage 5 LPT disk P/N 6078T92P01 and/or stage 6 LPT disk P/N 6089T89P01 whose serial numbers are listed in Figure 3 of GE Alert Service Bulletin CF34-AL S/B 72-A0173, Revision 3, dated July 20, 2004. Note: source text lists P/N 6089T89P01 here vs 6078T89P01 in AD 04-18635 for an apparently similar/duplicate provision.

Whether AD 2004-15-03 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 2004-15-03 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.