Airworthiness Directive 63-11-01

one-time
AD 63-11-01 · 1963-01-01 · airframe

Airworthiness Directives; of the Boeing Overhaul Manual. (2) Inspect and, as necessary, rework or replace the truck beam in accordance with paragraphs (b) a

Which aircraft AD 63-11-01 applies to

MakesBoeing

Inspect and, as necessary, rework or replace the landing gear truck beam per the Boeing Overhaul Manual; if a truck beam shield is fabricated, an alternative inspection procedure for the shielded truck beam area may be followed (clean shield with Navee 427 or FAA-approved equivalent; check for dents, gouges, cracks, pressure marks). Specific Boeing model not stated in excerpt.

Whether AD 63-11-01 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 63-11-01 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.