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Airworthiness Directive 86-11-05

one-time
AD 86-11-05 · 1986-01-01 · turbine engine

Airworthiness Directives; HEADING: GARRETT TURBINE ENGINE COMPANY Model TFE731-2, -3, and -3R Engines ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMA

Which aircraft AD 86-11-05 applies to

MakesHeading Garrett Turbine
ModelsTFE731-2
Applies to all models of the make above.

Whether AD 86-11-05 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

Supersession

Superseded by AD 2001-23-09 — comply with the superseding directive.

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 86-11-05 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.