As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NUMEROUS CRACKS IN TAILBOOM STRUCTURE REQUIING ENGINEERED REPAIR. PN 117-22122-15 FRAME 2L CRACKED AT OMEGA STRINGER CUTOUT. PN 105-30251-44 SUPPORT ANGLE CRACKED AT THE TOP OF THE 10L FRAME. PN 105-304061 AFT SPAR CRACKED AT A CAMLOC FASTENER. PN 117-22122-51 FRAME X6616 CRACKED IN NUMEROUS LOCATIONS.