Airworthiness Directive 93-09-12
one-timeAirworthiness Directives; March 8, 1991. (1) If no crack is found, prior to further flight, mark the upper members in accordance with Fokker Service Bulleti
Which aircraft AD 93-09-12 applies to
Wing upper member crack inspection, marking, replacement, and rework per Fokker Service Bulletin F27/32-162, dated March 8, 1991.
Whether AD 93-09-12 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.