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Airworthiness Directive 76-05-10

one-time
AD 76-05-10 · 1976-01-01 · turbine engine

Airworthiness Directives; AIRWORTHINESS DIRECTIVES FINAL RULES: 76-05-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AM

Which aircraft AD 76-05-10 applies to

MakesGeneral Electric
ModelsCF6-6D, CF6-6D1, CF6-50A, CF6-50C, CF6-50D, CF6-50E, CF6-50E1, CF6-50H, CF6

Applies to Models CF6-6D, CF6-6D1, CF6-50A, CF6-50C, CF6-50D, CF6-50E, CF6-50E1 and CF6-50H engines.

Whether AD 76-05-10 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 76-05-10 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.

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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.