Is AD 66-06-02 a recurring Airworthiness Directive?

No — AD 66-06-02 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 66-06-02 apply to?

AD 66-06-02 applies to Boeing. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 66-06-02

one-time

AD 66-06-02 · 1966-01-01 · airframe

Airworthiness Directives; pressure ratio) system. To prevent erroneous readings of the EPR system, install an additional rotary latch on the aft edge of the

Which aircraft AD 66-06-02 applies to

MakesBoeing

To prevent erroneous readings of the EPR (engine pressure ratio) system, install an additional rotary latch on the aft edge of the access door in accordance with Boeing Service Bulletin (bulletin number and specific model not present in available text).

Whether AD 66-06-02 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 66-06-02 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.