Airworthiness Directive 76-14-02
one-timeAirworthiness Directives; Visually inspect and, if necessary, replace the three attachment bolts on the tailwheel assembly in accordance with the 2d and 3rd
Which aircraft AD 76-14-02 applies to
Compliance is gated to replacement/repair with the specific DeHavilland part number noted in the teaser — confirm applicable aircraft/model from the full AD text before use.
Whether AD 76-14-02 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.