Is AD 75-26-09 a recurring Airworthiness Directive?

No — AD 75-26-09 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 75-26-09 apply to?

AD 75-26-09 applies to Morane Saulnier (Socata) — models MS892.A-150, MS893-A, MS894-A, MS 892, MS 893, MS 894. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 75-26-09

one-time

AD 75-26-09 · 1975-01-01 · airframe

Airworthiness Directives; INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-26-09 MORANE SAULNIER (SOCATA): Amendment 39-2460. Applies to

Which aircraft AD 75-26-09 applies to

MakesMorane Saulnier (Socata)

ModelsMS892.A-150, MS893-A, MS894-A, MS 892, MS 893, MS 894

Part-conditional — 880-27.0.261.0, 880-27.0.371.0.

Visually inspect elevator bellcrank (pitch control crank lever) per Socata Service Bulletin No. 89 GR 27.07, dated June 1971; if worn, replace elevator bellcrank No. 880-27.0.261.0 with reinforced bellcrank No. 880-27.0.371.0.

Whether AD 75-26-09 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 75-26-09 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.