Is AD 76-26-03 a recurring Airworthiness Directive?

No — AD 76-26-03 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 76-26-03

Q: Which aircraft does AD 76-26-03 apply to?

AD 76-26-03 applies to Morane Saulnier (Socata) — models MS 892A-150, MS 892E-150, MS 893A, MS 893E, MS 894A, MS 892, MS 893, MS 894. Serial/part conditions may narrow it to specific aircraft.

one-time

AD 76-26-03 · 1976-01-01 · airframe

Airworthiness Directives; FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 76-26-03 MORANE SAULNIER (SOCATA): Amendment 39-2792.

Which aircraft AD 76-26-03 applies to

MakesMorane Saulnier (Socata)

ModelsMS 892A-150, MS 892E-150, MS 893A, MS 893E, MS 894A, MS 892, MS 893, MS 894

Inspect for loose or lost carburetor heat flap retaining screws; replace all screws and nuts if any found loose or missing, per Socata Service Bulletin No. 125/1, dated September 1976.

Whether AD 76-26-03 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 76-26-03 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.