Airworthiness Directive 65-19-03
one-timeAirworthiness Directives; in the vicinity of waterline 208.1 (top of floor beam). If cracks are found, rework the frames before further flight in accordance
Which aircraft AD 65-19-03 applies to
Inspect fuselage frames at Station 800 near waterline 208.1 (top of floor beam) for cracks; if cracks are found, rework the frames before further flight per paragraph 3 of the referenced Boeing Service Bulletin.
Whether AD 65-19-03 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:
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.