What was found
INSPECTION FOUND LT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1474 - 1485. THERE WERE FIVE CRACKS TOTALING 8 INCHES IN COMBINED LENGTH. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND LT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1474 - 1485. THERE WERE FIVE CRACKS TOTALING 8 INCHES IN COMBINED LENGTH. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-01.