What was found
WING TO FUSELAGE PANEL 193D HAS 2 AREAS OF DAMAGE 1 AFT CENTER 32 BY 31.25, THE OTHER FORWARD LOWER 8 BY 2.5, FOUND ON BLOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WING TO FUSELAGE PANEL 193D HAS 2 AREAS OF DAMAGE 1 AFT CENTER 32 BY 31.25, THE OTHER FORWARD LOWER 8 BY 2.5, FOUND ON BLOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01.