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Airworthiness Directive 67-30-03

one-time
AD 67-30-03 · 1967-01-01 · airframe

Airworthiness Directives; and Manufacturing Branch, FAA Eastern Region. This supersedes Amendment 39-390 (Part 39 F.R. April 8, 1967), AD 67-12-03. This ame

Which aircraft AD 67-30-03 applies to

MakesMaryland Air Industries, Inc.
ModelsF-27A, F-27F, F-27G, F-27J, FH-227, FH-227B, FH-227C, FH-227D, FH-227E, F-27

Issued by Engineering and Manufacturing Branch, FAA Eastern Region; supersedes Amendment 39-390 (AD 67-12-03, Part 39 F.R. April 8, 1967); effective November 1, 1967.

Whether AD 67-30-03 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 67-30-03 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.

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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.