What was found
(CAN) DURING INSPECTION FOUND FUSELAGE RT STR 23743-05 AND LT FUSELAGE STR 23743-04 CRACKED AT THE FORWARD ENDS BELOW THE FORWARD WING ATTACH FITTINGS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING INSPECTION FOUND FUSELAGE RT STR 23743-05 AND LT FUSELAGE STR 23743-04 CRACKED AT THE FORWARD ENDS BELOW THE FORWARD WING ATTACH FITTINGS.