Is AD 67-15-04 a recurring Airworthiness Directive?

No — AD 67-15-04 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 67-15-04 apply to?

AD 67-15-04 applies to Sud Aviation. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 67-15-04

one-time

AD 67-15-04 · 1967-01-01 · other

Airworthiness Directives; as indicated. To detect cracks in the tail rotor gear box drive shaft, Sud Aviation P/N 3130-66-22-002, accomplish the following:

Which aircraft AD 67-15-04 applies to

MakesSud Aviation

Part-conditional — 3130-66-22-002, 3130-66-22-007.

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

Whether AD 67-15-04 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.

Date — When the work was done.

Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.

Signature & certificate — The A&P/IA who returned it to service, with certificate number.

Is AD 67-15-04 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.