Airworthiness Directive 48-44-02
one-timeAirworthiness Directives; center section lower skin beneath the fitting, just forward of the beam, and far enough inboard so that the resultant opening will
Which aircraft AD 48-44-02 applies to
Inspect wing center section lower skin beneath the fitting, just forward of the beam, for damage; resultant opening must be fully covered upon wing reinstallation.
Whether AD 48-44-02 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.