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Airworthiness Directive 93-17-08

one-time
AD 93-17-08 · 1993-01-01 · airframe

Airworthiness Directives; BOEING Model 737-100, 737-200, 737-200C Airplanes

Which aircraft AD 93-17-08 applies to

MakesBoeing
Models737-100, 737-200, 737-200C, 737

Certificated in any category; inspection/modification thresholds per Boeing Document D6-38505, "Aging Airplane Service Bulletin Structural Modification and Inspection Program," Revision F, dated April 23 (year truncated).

Whether AD 93-17-08 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 93-17-08 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.