Airworthiness Directive 78-18-02

one-time
AD 78-18-02 · 1978-01-01 · airframe

Airworthiness Directives; MCDONNELL DOUGLAS DC-3 Series, DC-3A Series, DC-3C Series, DC-3D, Super DC-3 and R4D Series

Which aircraft AD 78-18-02 applies to

MakesDouglasMcdonnell DouglasThe Boeing Company
ModelsDC-3, DC-3A, DC-3C, DC-3D, Super DC-3, R4D-8, R4D-8Z, R4D

Amendment 39-3289, effective September 6, 1978. Applies to Model DC-3 Series, DC-3A Series, DC-3C Series, DC-3D, Super DC-3 and R4D Series airplanes (source text truncated; specific requirement not captured). Type certificate lineage: Douglas Aircraft Co., Inc. / The Boeing Company.

Whether AD 78-18-02 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 78-18-02 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.