Airworthiness Directive 85-08-08
one-timeAD 85-08-08 · 1985-01-01 · propeller
Airworthiness Directives; - CLM, -JLM, -KLM, -LM, and -M. Compliance is required as indicated unless already accomplished. To detect propeller hub cracks an
Which aircraft AD 85-08-08 applies to
Makes- Clm -Jlm -Klm -Lm And -M Compliance Is Required As Indicated Unless Already Accomplished To Detect
ModelsD3A32C90-BLM, T207
Whether AD 85-08-08 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 85-08-08 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.