What was found
PREVIOUSLY REWORKED AREA ON EXTERNAL FUSELAGE SKIN BS 380-400 S-38R-39R BY 2.0 X 1.6 X 0.011 X 0.010" (NOTED AREA FOUND WITHIN ALLOWABLE DAMAGE; LIMITS IAW SRM 53-30-01, FIG 1.)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PREVIOUSLY REWORKED AREA ON EXTERNAL FUSELAGE SKIN BS 380-400 S-38R-39R BY 2.0 X 1.6 X 0.011 X 0.010" (NOTED AREA FOUND WITHIN ALLOWABLE DAMAGE; LIMITS IAW SRM 53-30-01, FIG 1.)