Airworthiness Directive 77-15-06

one-time
AD 77-15-06 · 1977-01-01 · airframe

Airworthiness Directives; 98/2, dated April 1976, or an FAA-approved equivalent. This amendment becomes effective August 22, 1977. FOOTER: SOCATA - Groupe A

Which aircraft AD 77-15-06 applies to

MakesMorane SaulnierSocata - Groupe Aerospatiale
ModelsMS 892A-150, MS 892E-150, MS 893A, MS 893E, Rallye 150 ST, Rallye 150 T, MS 892, MS 893, Rallye 150

Compliance per SOCATA Service Bulletin 98/2, dated April 1976, or FAA-approved equivalent.

Whether AD 77-15-06 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

Supersession

Superseded by AD 2002-05-04 — comply with the superseding directive.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 77-15-06 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.