Airworthiness Directive 86-10-09
one-timeAirworthiness Directives; MCDONNELL DOUGLAS DC-9, MD-80, and C-9 (Military) Series Airplanes
Which aircraft AD 86-10-09 applies to
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:
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.