Airworthiness Directive 83-17-06
one-timeAD 83-17-06 · 1983-01-01 · airframe
Airworthiness Directives; CESSNA: Amendment 39-4716. Applies to Models 180 through 180H, 180J and 180K airplanes, modified per Robertson STC SA1435WE; 150D
Which aircraft AD 83-17-06 applies to
MakesCessna Amendment 39-4716 Applies To
Models180, 180K, 150L, A185F, TR182, 172P, T182
Serial-conditional — narrows to serials 180–180H, 150D–150L, 150D–150L, 185A–185E, 182–182R, 172A–172P.
Whether AD 83-17-06 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 83-17-06 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.