Airworthiness Directive 85-01-04

one-time
AD 85-01-04 · 1985-01-01 · airframe

Airworthiness Directives; are not present, install P/N 2-5100-20 gussets in accordance with Pitts Service Letter No. 5, Revision B. (b) The aircraft may be

Which aircraft AD 85-01-04 applies to

MakesAviat Aircraft Inc.Pitts
ModelsS-2A
Part-conditional2-5100-20.

If gussets are not present, install P/N 2-5100-20 gussets in accordance with Pitts Service Letter No. 5, Revision B. Aircraft may be flown per FAR 21.197 to a location where the AD can be accomplished; equivalent means of compliance approved by the Denver Aircraft Certification Office. Effective January 21, 1985.

Whether AD 85-01-04 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 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 85-01-04 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.

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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.