Airworthiness Directive 76-24-04
one-timeAirworthiness Directives; FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 76-24-04 MORANE SAULNIER (SOCATA): Amendment 39-2780.
Which aircraft AD 76-24-04 applies to
Inspect rocker oil return pipes for wear; rework cylinder cooling deflector spring; per Socata Service Bulletin No. 124, GR 79-09, dated January 1976.
Whether AD 76-24-04 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:
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.