Is AD 60-02-05 a recurring Airworthiness Directive?

No — AD 60-02-05 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 60-02-05 apply to?

AD 60-02-05 applies to Douglas — models DC-6. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 60-02-05

one-time

AD 60-02-05 · 1960-01-01 · airframe

Airworthiness Directives; DOUGLAS DC-6

Which aircraft AD 60-02-05 applies to

MakesDouglas

ModelsDC-6

Amendment 84, 14 CFR Part 507. At next regularly scheduled overhaul, holes located in the forward tang of the front spar lower cap should be enlarged and new attachments installed per Kit "A" of Douglas Service Bulletin A-845 or equivalent; if spar cap cracks are found, temporary rework per drawing referenced in source (cut off).

Whether AD 60-02-05 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 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 60-02-05 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.