As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
F008527 THE EXTERNAL SKIN OF THE FUSELAGE IS CRACKED AT FRAME 75 BETWEEN STRINGERS 1L AND 2L. PERFORMED REPAIR ON EXTERNAL SKIN OF THE FUSELAGE AT FRAME 75 BETWEEN STRINGERS 1L AND 2L. IAW EMB 145 SRM53-31-01 ITEM 11 FIGURE 219 SHEET 1 AND TABLE 27 AND EO1-53-24-0729.