Airworthiness Directive 48-02-04

one-time
AD 48-02-04 · 1948-01-01 · airframe

Airworthiness Directives; adjusting pin Goodyear P/N 9510744. (Douglas Service Bulletin DC-6 No. 90 covers this same subject.) FOOTER: The Boeing Company DC

Which aircraft AD 48-02-04 applies to

MakesThe Boeing CompanyDouglas
ModelsDC-6, DC-6A, DC-6B
Serial-conditional — narrows to serials 42854–42880, 42882–?.
Part-conditional9510744.

Concerns an adjusting pin, Goodyear P/N 9510744; see Douglas Service Bulletin DC-6 No. 90 covering the same subject.

Whether AD 48-02-04 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 48-02-04 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.