Airworthiness Directive 79-03-04

one-time
AD 79-03-04 · 1979-01-01 · airframe

Airworthiness Directives; Headquarters in Washington, D.C. and at the Southern Regional Office. This amendment is effective February 5, 1979. FOOTER: Lockhe

Which aircraft AD 79-03-04 applies to

MakesLockheed Martin Corporation
Models382, 382B, 382E, 382F, 382G

Effective February 5, 1979. Full regulatory text not available in source data.

Whether AD 79-03-04 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:

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 79-03-04 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.