Airworthiness Directive 69-12-01

one-time
AD 69-12-01 · 1969-01-01 · appliance

Airworthiness Directives; restricting air flow through the engine air induction system, accomplish the following: (a) Within the next 10 hours' time in serv

Which aircraft AD 69-12-01 applies to

MakesPiper
Part-conditional63633-43, 760-328.

Air induction inlet hose restricting air flow through the engine air induction system. Within 10 hours TIS, remove air induction inlet hose Piper Part Number 63633-43 and inspect for deterioration, broken or frayed cord wrapping, and other damage; within 50 hours TIS, install a new Piper air induction hose per Piper Kit 760-328.

Whether AD 69-12-01 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 69-12-01 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.