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Airworthiness Directive 02-31999

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AD 02-31999 · 2002-12-19 · turbine engine

Airworthiness Directives; General Electric Company CF34-8C1 Turbofan Engines, Correction

What this AD requires

This document makes a correction to a previous correction to Airworthiness Directive (AD) 2002-23- 02 applicable to General Electric Company CF34-8C1 turbofan engines that was published in the Federal Register on December 11, 2002 (67 FR 76111). A typographical error was made in the AD number in line three of the Summary. This document corrects that number. In all other respects, the original document remains the same.

Which aircraft AD 02-31999 applies to

MakesGeneral Electric Company Cf34-8C1 Turbofan

Whether AD 02-31999 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 02-31999 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.