Airworthiness Directive 86-10-09

one-time
AD 86-10-09 · 1986-01-01 · airframe

Airworthiness Directives; MCDONNELL DOUGLAS DC-9, MD-80, and C-9 (Military) Series Airplanes

Which aircraft AD 86-10-09 applies to

ModelsDC-9, MD-80, C-9

Amendment 39-5319, effective June 9, 1986. Applies to McDonnell Douglas Model DC-9, MD-80, and C-9 (Military) series airplanes. Requires inspecting switch cams for proper installation position and repositioning if necessary, per McDonnell Douglas Alert Service Bulletin A76-43, dated April 14, 1986.

Whether AD 86-10-09 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 86-10-09 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.