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Airworthiness Directive 83-14-07 R3

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AD 83-14-07 R3 · 1983-01-01 · airframe

Airworthiness Directives; SA2143NM (Machen, Inc., Stall Improvement Kit) alone or in combination with STC SA1658NM (Machen, Inc., Superstar I). f) Paragraph

Which aircraft AD 83-14-07 R3 applies to

MakesMachen, Inc.
Part-conditional — STC SA2143NM, STC SA1658NM, STC SA980NM.

Applies to airplanes modified per Machen, Inc. STCs: SA2143NM (Stall Improvement Kit) alone or combined with SA1658NM (Superstar I), or SA980NM (Superstar II). Compliance may alternatively be accomplished by modifying the airplane per STC SA2143NM alone or combined with SA1658NM. Aircraft make/model not present in the retrieved text.

Whether AD 83-14-07 R3 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 83-14-07 R3 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.

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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.