What was found
LEFT AND RIGHT OUTBOARD WEB SUPPORT ANGLES AT THE BOTTOM OF THE VERTICAL STABILIZER HAS 2 INCH CRACK ON EACH ANGLE. VIEWED THRU PANELS 324LL. REMOVED AND REPLACED ANGLES IAW 51-40-02 SRM, ACFT WAS GROUNDED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT AND RIGHT OUTBOARD WEB SUPPORT ANGLES AT THE BOTTOM OF THE VERTICAL STABILIZER HAS 2 INCH CRACK ON EACH ANGLE. VIEWED THRU PANELS 324LL. REMOVED AND REPLACED ANGLES IAW 51-40-02 SRM, ACFT WAS GROUNDED.