Airworthiness Directive 83-05-05

one-time
AD 83-05-05 · 1983-01-01 · airframe

Airworthiness Directives; ), accomplish the repair modification specified in BAC Modification PM2857, part (a), prior to further flight. E. Incorporation of

Which aircraft AD 83-05-05 applies to

MakesBac

Accomplish repair modification per BAC Modification PM2857, Part (a), prior to further flight; incorporation of BAC Modification PM2857 Part (a), PM3346, or PM5525 eliminates the repetitive inspection requirement; approved by the Manager, Seattle Aircraft Certification Office, FAA Northwest Mountain Region.

Whether AD 83-05-05 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 83-05-05 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.