Airworthiness Directive 78-16-08

one-time
AD 78-16-08 · 1978-01-01 · airframe

Airworthiness Directives; the area of the oil hose assembly end fittings and in the area of the fluted portion at the oil cooler end tanks for cracks and oi

Which aircraft AD 78-16-08 applies to

MakesPiper
ModelsPA-32R-300, PA-32RT-300, PA-32

Oil hose assembly end fittings and oil cooler end tanks inspected for cracks/leakage; leaking or cracked oil coolers replaced.

Whether AD 78-16-08 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 78-16-08 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.