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Airworthiness Directive 05-8883

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AD 05-8883 · 2005-05-05 · turbine engine

Airworthiness Directives; General Electric Company (GE) CF6-80A1/A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie A300-600 and A310 Series Airplanes; Correction

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2005-06-07. That AD applies to GE CF6-80A1/A3 and CF6-80C2A series turbofan engines. We published AD 2005-06-07 in the Federal Register on March 21, 2005, (70 FR 13365). A service bulletin number in the compliance section is incorrect. This document corrects that service bulletin number. In all other respects, the original document remains the same.

Which aircraft AD 05-8883 applies to

MakesGeneral Electric Company (Ge) Cf6-80A1/A3 And Cf6-80C2A

Whether AD 05-8883 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 05-8883 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.