Airworthiness Directive 61-04-04
one-timeAirworthiness Directives; inspections contained in this AD may be discontinued after the Howard Aero, Inc., replacement main landing gear drag strut attach
Which aircraft AD 61-04-04 applies to
Special inspections of main landing gear drag strut attach plates may be discontinued after installing Howard Aero, Inc. replacement attach plates P/N 5-302006 or FAA-approved equivalent; deformed or cracked bolts must be replaced prior to next flight.
Whether AD 61-04-04 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.