What was found
MIA - INSPECTION FOUND A .5 INCH CRACK IN LEFT AND RIGHT VERTICAL STABILIZER TO FUSELAGE EXTERNAL ATTACH ANGLES LOCATED BETWEEN BS 1401 TO 1429. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MIA - INSPECTION FOUND A .5 INCH CRACK IN LEFT AND RIGHT VERTICAL STABILIZER TO FUSELAGE EXTERNAL ATTACH ANGLES LOCATED BETWEEN BS 1401 TO 1429. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)