Is AD 89-19-04 R1 a recurring Airworthiness Directive?

No — AD 89-19-04 R1 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 89-19-04 R1 apply to?

AD 89-19-04 R1 applies to Beech. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 89-19-04 R1

one-time

AD 89-19-04 R1 · 1989-01-01 · airframe

Airworthiness Directives; partial replacement panel per Paragraph (a)(3) of this AD. (B) and there is no debonding, prior to further flight reseal the blind

Which aircraft AD 89-19-04 R1 applies to

MakesBeech

Part-conditional — 101-4048-1S.

Panel repair: reseal blind rivets or install a temporary repair per Figure 1 of Beech Service Bulletin No. 2040, Revision III, dated April 1990 (usable no longer than 12 calendar months), then install an approved partial replacement panel per Beech Kit 101-4048-1S if debonding is not present.

Whether AD 89-19-04 R1 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 89-19-04 R1 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.