What was found
DURING SCHEDULED D-CHECK, FOUND A 2 INCH CRACK IN RADIUS OF SUPPORT FITTING MEMBER AT HORZ STAB CENTER SECTION UPPER SUPPORT, O/B SIDE OF BEAM, 25 AFT OF FWD SPAR, 20 I/B OF RT SIDE INTERNAL FUSE SKIN. REPAIRED PER BOEING SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED D-CHECK, FOUND A 2 INCH CRACK IN RADIUS OF SUPPORT FITTING MEMBER AT HORZ STAB CENTER SECTION UPPER SUPPORT, O/B SIDE OF BEAM, 25 AFT OF FWD SPAR, 20 I/B OF RT SIDE INTERNAL FUSE SKIN. REPAIRED PER BOEING SRM.