Airworthiness Directive 79-26-04

one-time
AD 79-26-04 · 1979-01-01 · airframe

Airworthiness Directives; certificated in all categories: PA-32RT-300 Lance II 32R-7885001 to 32R-7885025 Inclusive 32R-7885027 to 32R-7885261 Inclusive 32R

Which aircraft AD 79-26-04 applies to

MakesPiper
ModelsPA-32RT-300, PA-32RT-300T, PA-32RT
Serial-conditional — narrows to serials 32R-7885001–32R-7885025, 32R-7885027–32R-7885261, 32R-7885263–32R-7885285, 32R-7985001–32R-7985035, 32R-7985083–32R-7985085, 32R-7985088–32R-7985090, 32R-7985092–32R-7985097, 32R-7985103–32R-7985105.

applicability read from the AD teaser — confirm exact model/serial from the records

Whether AD 79-26-04 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 79-26-04 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.

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.