Is AD 58-22-04 a recurring Airworthiness Directive?

No — AD 58-22-04 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 58-22-04 apply to?

AD 58-22-04 applies to Sud Aviation. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 58-22-04

one-time

AD 58-22-04 · 1958-01-01 · airframe

Airworthiness Directives; issued the following corrective measures which French SGACC considers mandatory: A. Prior to Next Flight: (1) Remove the tail roto

Which aircraft AD 58-22-04 applies to

MakesSud Aviation

Tail rotor inclined drive shaft assembly removal per French SGACC-mandated corrective measures; specific helicopter model not captured in this excerpt (applicability read from the AD teaser — confirm exact model/serial from the records.)

Whether AD 58-22-04 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 58-22-04 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.