Is AD 89-07-02 a recurring Airworthiness Directive?

No — AD 89-07-02 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 89-07-02 apply to?

AD 89-07-02 applies to Mcdonnell Douglas — models DC-8. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 89-07-02

one-time

AD 89-07-02 · 1989-01-01 · airframe

Airworthiness Directives; the rudder drive crank assembly with P/N 5647102-503 in accordance with McDonnell Douglas DC-8 Service Bulletin 27-268, dated Febr

Which aircraft AD 89-07-02 applies to

MakesMcdonnell Douglas

ModelsDC-8

Part-conditional — 5647102-503.

applicability read from the AD teaser — confirm exact model/serial from the records

Whether AD 89-07-02 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 89-07-02 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.