What was found
DAMAGED AREA BY 6.0 X 3.0" ON EXTERNAL FUSELAGE SKIN AT STRINGER AREA BS 160-180 S-42AL (DAMAGED AREA FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DAMAGED AREA BY 6.0 X 3.0" ON EXTERNAL FUSELAGE SKIN AT STRINGER AREA BS 160-180 S-42AL (DAMAGED AREA FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A).