What was found
ASSESS DAMAGE ON FUSELAGE SKIN BS 484, BETWEEN LONGERON 23-24 RT, SPEED TAPE ID DATA. REPAIR WAS EVALUATED AND FOUND ACCOMPLISHED IAW INSTRUCTIONS OF SRM 53-04-2, FIG 2, SHEET 5, AS PERMANENT REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ASSESS DAMAGE ON FUSELAGE SKIN BS 484, BETWEEN LONGERON 23-24 RT, SPEED TAPE ID DATA. REPAIR WAS EVALUATED AND FOUND ACCOMPLISHED IAW INSTRUCTIONS OF SRM 53-04-2, FIG 2, SHEET 5, AS PERMANENT REPAIR.