What was found
DURING INSPECTION, FOUND DAMAGE TO THE LT FUSELAGE SKIN BETWEEN FS 625.00 & 654.00, STRINGER 22L & 23L. THE DAMAGE MEASURES A MAXIMUM OF 30.0” X 4.5” X .375” DEEP. REPAIRED IAW CRJ253-03382.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND DAMAGE TO THE LT FUSELAGE SKIN BETWEEN FS 625.00 & 654.00, STRINGER 22L & 23L. THE DAMAGE MEASURES A MAXIMUM OF 30.0” X 4.5” X .375” DEEP. REPAIRED IAW CRJ253-03382.