Airworthiness Directive 93-19-02 R1
one-timeAirworthiness Directives; inches, inspect in accordance with the new criteria, improved technique, intervals, and requirements defined in the Accomplishment
Which aircraft AD 93-19-02 R1 applies to
Eddy current inspection (ECI) of diffuser case rear rail for cracks per Pratt & Whitney Service Bulletin (SB) No. 5591, Revision 7, dated March 6, 1986.
Whether AD 93-19-02 R1 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.