Airworthiness Directive 50-19-02
one-timeAirworthiness Directives; Aircraft. Compliance required as indicated. Failures of the rudder flight tab balance weight brackets and of the rudder closing sp
Which aircraft AD 50-19-02 applies to
Inspect rudder flight tab balance weight brackets for cracks near the neck-down area and counterweight edges, and inspect the rudder closing spar for cracks adjacent to the tab hinge brackets; repair/replace cracks before further flight.
Whether AD 50-19-02 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.