TailplateTailplate
Run a report

Airworthiness Directive 69-06-05

one-time
AD 69-06-05 · 1969-01-01 · airframe

Airworthiness Directives; by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region. This amendment is effective April 15, 1969. FOOTER: Maryla

Which aircraft AD 69-06-05 applies to

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

Source applicability text truncated; references the Chief, Engineering and Manufacturing Branch, FAA Eastern Region. Amendment effective April 15, 1969.

Whether AD 69-06-05 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 69-06-05 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.