What was found
DURING PERIODIC CHECK, THE TRIANGLE WEB PANEL AFT OF FRAME 68, NEAR THE FUSELAGE SKIN WAS FOUND CRACKED. STOP DRILLED CRACK AND SEALED PER EA 32-106827.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING PERIODIC CHECK, THE TRIANGLE WEB PANEL AFT OF FRAME 68, NEAR THE FUSELAGE SKIN WAS FOUND CRACKED. STOP DRILLED CRACK AND SEALED PER EA 32-106827.