Airworthiness Directive 90-22-02
one-timeAirworthiness Directives; flight, LPT shafts found cracked during inspections conducted in accordance with (a) or (b) above. (d) LPT shafts which have been
Which aircraft AD 90-22-02 applies to
Low pressure turbine (LPT) shaft crack inspection; cracked shafts removed from service prior to further flight.
Whether AD 90-22-02 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.