Airworthiness Directive 93-10-11

one-time
AD 93-10-11 · 1993-01-01 · airframe

Airworthiness Directives; Instructions section of Avions Mudry & Cie SB CAP10B No. 15 (ATA 57-003), dated April 14, 1992. If cracks are found, prior to furt

Which aircraft AD 93-10-11 applies to

MakesAvions Mudry & Cie
ModelsCAP 10B, CAP 10

Inspect per the Accomplishment Instructions section of Avions Mudry & Cie Service Bulletin CAP10B No. 15 (ATA 57-003), dated April 14, 1992; if cracks are found, obtain an FAA-approved repair scheme from the manufacturer through the Brussels Aircraft Certification Office and incorporate it prior to further flight.

Whether AD 93-10-11 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 93-10-11 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.