Airworthiness Directive 86-10-03

one-time
AD 86-10-03 · 1986-01-01 · airframe

Airworthiness Directives; HEADING: Mitsubishi Models MU-300 and MU-300-10 Airplanes ACTION: SUMMARY: DATES: Effective June 2, 1986. ADDRESSES: FOR FURTHER I

Which aircraft AD 86-10-03 applies to

ModelsMU-300, MU-300-10

Placard requirement referencing MU-300-10 Safety Communique dated April 1986; placard may be removed once Airplane Flight Manual and modification requirements are met.

Whether AD 86-10-03 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 86-10-03 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.