Airworthiness Directive 75-07-04
one-timeAirworthiness Directives; The directive requires an inspection prior to further flight, unless already accomplished, and is effective immediately upon recei
Which aircraft AD 75-07-04 applies to
Possible missing welds in rudder control bar assemblies P/N 601031-501 located inside the forward portion of the fuselage; inspect before further flight, unless already accomplished. Effective immediately upon receipt. Special flight permit per FAR 21.197 may be issued after accomplishment of paragraph 1 to allow repairs.
Whether AD 75-07-04 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:
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.