What was found
DURING CHECK-C MAINT, THE FUSELAGE SKIN WAS DEFORMED FROM STA 1193 TO 1211, LONGERON 27L TO 28L. REPAIRED PER SRM 53-04, FIG 12B, PAGE 39.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, THE FUSELAGE SKIN WAS DEFORMED FROM STA 1193 TO 1211, LONGERON 27L TO 28L. REPAIRED PER SRM 53-04, FIG 12B, PAGE 39.