Airworthiness Directive 85-03-01

one-time
AD 85-03-01 · 1985-01-01 · airframe

Airworthiness Directives; with this AD may be used if approved by the Manager, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Room 100, Mid-

Which aircraft AD 85-03-01 applies to

MakesCessna Aircraft Company
Models206, 207, 210-5, 205, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, P206, P206A, P206B, P206C, P206D, 210

Amendment effective March 15, 1985; equivalent compliance methods approved by Manager, FAA Wichita ACO.

Whether AD 85-03-01 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 85-03-01 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.