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Airworthiness Directive 68-11-01

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AD 68-11-01 · 1968-01-01 · airframe

Airworthiness Directives; May 10, 1968. FOOTER: The Boeing Company 707-100 Long Body 707-100B Long Body 707-100B Short Body 707-200 707-300 Series 707-300B

Which aircraft AD 68-11-01 applies to

MakesThe Boeing Company
Models707-100 Long Body, 707-100B Long Body, 707-100B Short Body, 707-200, 707-300 Series, 707-300B Series, 707-300C Series, 707-400 Series, 707

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

Whether AD 68-11-01 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 68-11-01 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.