Airworthiness Directive 82-02-03
one-timeAirworthiness Directives; the following: 1. Remove the large inspection panel located in the center of the bottom skin just aft of the Station 68 frame. 2.
Which aircraft AD 82-02-03 applies to
Remove bottom-skin inspection panel just aft of the Station 68 frame and drill a 3/8-inch diameter inspection hole for further inspection.
Whether AD 82-02-03 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.