As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FORWARD FUSELAGE SKIN HAS AREA OF THROUGH DAMAGE LOCATED NEAR THE INTERSECT OF FRAME 22 AND STRINGER 14L. THE DAMAGED AREA MEASURES APPROX 3.0 INCHES LONG AND 1.5 INCHES HIGH. THE ACTUAL THROUGH DAMAGE MEASURES APPROX 1.0 INCH LONG AND 3/4 INCHES HIGH.*THIS DAMAGE IS CONSIDERED A MAJOR REPAIR AND WILL REQUIRE A FROM 337 PER GMM 3-26*REFERENCE CP 2861303-1 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS