What was found
FOUND ON CV2 CHECK, TWO CRACKS IN NR 7 SLAT COVE PANEL ATTACH ANGLE BELOW TAI DUCT. REPAIR: REPAIRED PER M/M 57-54-0, PAR 5A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND ON CV2 CHECK, TWO CRACKS IN NR 7 SLAT COVE PANEL ATTACH ANGLE BELOW TAI DUCT. REPAIR: REPAIRED PER M/M 57-54-0, PAR 5A.