Airworthiness Directive 86-05-08
one-timeAD 86-05-08 · 1986-01-01 · airframe
Airworthiness Directives; effective April 7, 1986. FOOTER: Fokker Services F.28 Mark 0070 F.28 Mark 0100 F.28 Mark 1000 F.28 Mark 2000 F.28 Mark 3000 F.28 M
Which aircraft AD 86-05-08 applies to
MakesFokker
ModelsF.28 Mark 0070, F.28 Mark 0100, F.28 Mark 1000, F.28 Mark 2000, F.28 Mark 3000, F.28 Mark 4000, F.28
Whether AD 86-05-08 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 86-05-08 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.
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.