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Airworthiness Directive 04-10429

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AD 04-10429 · 2004-05-07 · turbine engine

Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines; Correction

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2004-07-13. That AD applies to General Electric Company (GE) CF6- 80C2 series turbofan engines. That AD was published in the Federal Register on April 1, 2004 (69 FR 17033). The amendatory text in the Applicability section is incorrect. This document corrects the aircraft models that these engines are installed on. In all other respects, the original document remains the same.

Which aircraft AD 04-10429 applies to

MakesGeneral Electric
ModelsCF6-80C2

Federal Register correction notice for AD 04-7235 (GE CF6-80C2 series turbofan engines); corrects applicability text from 'A300 and A330' to 'A300 and A310'; source text is a correction fragment, not the full applicability paragraph

Whether AD 04-10429 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 04-10429 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.