Airworthiness Directive 64-19-03

one-time
AD 64-19-03 · 1964-01-01 · airframe

Airworthiness Directives; to this same subject.) This supersedes AD 62-20-01. This directive effective September 7, 1964. Revised October 13, 1964. FOOTER:

Which aircraft AD 64-19-03 applies to

MakesThe Boeing Company
ModelsDC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43, DC-8-51, DC-8-52, DC-8-53, DC-8-55, DC-8F-55, DC-8, DC-8F

Applicability read from the AD teaser — confirm exact model/serial from the records.

Whether AD 64-19-03 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 64-19-03 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.