Airworthiness Directive 86-23-04
one-timeAD 86-23-04 · 1986-01-01 · airframe
Airworthiness Directives; 10, 1986. FOOTER: Fokker Services F27 Mark 050 F27 Mark 100 F27 Mark 200 F27 Mark 300 F27 Mark 400 F27 Mark 500 F27 Mark 600 F27 M
Which aircraft AD 86-23-04 applies to
Makes10 1986 Footer Fokker Services F27 Mark 050 F27 Mark 100 F27 Mark 200 F27 Mark 300 F27 Mark 400 F27 Mark 500 F27 Mark 600 F27 Mark 700 Fokker Services\F27 Mark 050 Fokker Services\F27 Mark 100 Fokker Services\F27 Mark 200 Fokker Services\F27 Mark 300 Fokker Services\F27 Mark 400 Fokker Services\F27 Mark 500 Fokker Services\F27 Mark 600 Fokker Services\F27 Mark 700 This Information Is Not Available Unknown 86-23-04 Ad Final Rules 86-23-04 Fokker B V Amendment 39-5459 Applies To
ModelsF27
Whether AD 86-23-04 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 86-23-04 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.