Airworthiness Directive 81-23-05

one-time
AD 81-23-05 · 1981-01-01 · airframe

Airworthiness 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

MakesPiper
ModelsPA-28-151, PA-28-161, PA-28
Serial-conditional — narrows to serials 28-7716001–28-8216066.
Part-conditional35669-194.

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:

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 81-23-05 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.