What was found
INSPECTION FOUND A .25 INCH CRACK IN TAIL COMPARTMENT LEFT VENTRAL BOX SUPPORT ANGLE AT CANTED FRAME STA 1474. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN TAIL COMPARTMENT LEFT VENTRAL BOX SUPPORT ANGLE AT CANTED FRAME STA 1474. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-05.