Airworthiness Directive 81-23-05
one-timeAirworthiness Directives; -161 (S/N 28-7716001 through 28-8216066) airplanes certificated in any category. COMPLIANCE: Required prior to further flight and
Which aircraft AD 81-23-05 applies to
PA-28-161 airplanes S/N 28-7716001 through 28-8216066, certificated in any category; install P/N 35669-194 on top of the spar box per Piper Service Bulletin 631B; check rear seat base is properly positioned before each flight; addresses possible inflight fire.
Whether AD 81-23-05 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.