Airworthiness Directive 93-10-11
one-timeAirworthiness 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
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:
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.
Look up a tail number →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.