What was found
AFTER PHASE II INSPECTION, FOUND POSSIBLE LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 500A TO 500B, STR 19R. PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN BS 500A - 500B, STR 19R, IAW SRM 53-00-01-2R-41.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER PHASE II INSPECTION, FOUND POSSIBLE LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 500A TO 500B, STR 19R. PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN BS 500A - 500B, STR 19R, IAW SRM 53-00-01-2R-41.