Airworthiness Directive 86-19-12

one-time
AD 86-19-12 · 1986-01-01 · turboshaft engine

Airworthiness Directives; Helicopter Company (Hughes) Models 369F and 369FF aircraft. SIKORSKY AIRCRAFT: Applies to Sikorsky Aircraft Model S-76A helicopter

Which aircraft AD 86-19-12 applies to

MakesAllisonHughes HelicoptersSikorsky Aircraft
Models250-C30, 250-C30S, 369F, 369FF, S-76A, 250

Applies to Allison Model 250-C30 and 250-C30S engines installed in Hughes Helicopters Models 369F and 369FF, and in Sikorsky Aircraft Model S-76A helicopters certificated in any category, to prevent failure/secondary damage. Within 30 days after December 18, 1984 for aircraft in compliance with telegraphic AD T84-16-51, prior to further flight for aircraft not in compliance.

Whether AD 86-19-12 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 86-19-12 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.