Airworthiness Directive 90-17-15

one-time
AD 90-17-15 · 1990-01-01 · airframe

Airworthiness Directives; Wytwornia Sprzetu Komunikacyjnego Pzl-Mielec Model M18 Series Airplanes

Which aircraft AD 90-17-15 applies to

ModelsM18

Applies to Wytwornia Sprzetu Komunikacyjnego PZL-Mielec Model M18 series airplanes (Amendment 39-6678, Docket No. 90-CE-26-AD, effective September 17, 1990); inspect for cracks/damage in the vertical [stabilizer/fin, text truncated] per PZL-Mielec Mandatory Engineering Bulletin (MEB) No. K/02.135/89, dated December 29, 1989.

Whether AD 90-17-15 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 90-17-15 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.