Airworthiness Directive 86-24-07

one-time
AD 86-24-07 · 1986-01-01 · other

Airworthiness Directives; T210G T210H T210J T210K T210L T210M TP206A TP206B TP206C TP206D TP206E TU206A TU206B TU206C TU206D TU206E TU206F TU206G U206 U206A

Which aircraft AD 86-24-07 applies to

MakesT210G T210H T210J T210K T210L T210M Tp206A Tp206B Tp206C Tp206D Tp206E Tu206A Tu206B Tu206C Tu206D Tu206E Tu206F Tu206G U206 U206A U206B U206C U206D U206E U206F U206G Textron \150C Textron \150D Textron \150E Textron \150F Textron \150G Textron \150H Textron \150J Textron \150K Textron \150L Textron \150M Textron \152 Textron \172D Textron \172E Textron \172F (Usaf T
ModelsT210G, T210H, T210J, T210K, T210L, T210M

Whether AD 86-24-07 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 86-24-07 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.