As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PIT - DURING Q-1 CHECK, FOUND 3 INCH CRACKS (2 EACH) AND .075 INCH CRACKS (2 EACH) AT FUSELAGE CENTER WING FRONT SPAR FRAME AND ANGLES AT STA 11 (LHS) AND STA 64 (RHS). ROUTED OUT CRACK AREAS IN FRAME AND INSTALLED NEW ANGLES PER EA NR 33430 AND EA NR 32077. (X)