Airworthiness Directive 62-08-04

one-time
AD 62-08-04 · 1962-01-01 · airframe

Airworthiness Directives; incorporating magnesium skin; (3) Replace with a new standard cover incorporating aluminum alloy skin; (4) Replace with a cover in

Which aircraft AD 62-08-04 applies to

MakesBoeing
Part-conditional65-28201, 65-28202, 65-28203, 65-28204, 65-28205, 65-28206, 65-28207, 65-28208.

Compliance is gated to installation of one of the specific replacement cover part numbers noted in the teaser — confirm applicable model from the full AD text before use.

Whether AD 62-08-04 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 62-08-04 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.

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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.