Airworthiness Directive 92-10-03
one-timeAirworthiness Directives; 180 days for a period of two years after the initial inspections, perform a visual inspection of the in-line splices in the Auxili
Which aircraft AD 92-10-03 applies to
Visual inspection of in-line splices in the Auxiliary Power Unit (APU) and integrated drive generator circuits for heat damage, per British Aerospace Inspection Service Bulletin 24-84, dated January 22, 1991; repeat at 180-day intervals for two years after initial inspection.
Whether AD 92-10-03 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.