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Airworthiness Directive 86-16-02

one-time
AD 86-16-02 · 1986-01-01 · airframe

Airworthiness Directives; -29, dated October 1, 1985. (b) If a defective lever is found during the inspection required by Paragraph (a) of this AD, before f

Which aircraft AD 86-16-02 applies to

MakesGrob (Burkhart Grob / Grob Werke Gmbh)
ModelsG103 TWIN II, G103A TWIN II ACRO, G103

Glider (sailplane); airbrake operating lever inspection/replacement per Grob TM 315-29, dated October 1, 1985.

Whether AD 86-16-02 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 86-16-02 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.