What was found
DURING INSPECTION, FOUND FUSELAGE FRAME CRACKED AT STA 1605, STR 14. DAMAGE IS TYPICAL TO THAT DESCRIBED IN FAA AD 95-10-17 AND LAC S/B 093-53-A271. REPAIR IS BEING ACCOMPLISHED PER DAL SI 7-69903-12AD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND FUSELAGE FRAME CRACKED AT STA 1605, STR 14. DAMAGE IS TYPICAL TO THAT DESCRIBED IN FAA AD 95-10-17 AND LAC S/B 093-53-A271. REPAIR IS BEING ACCOMPLISHED PER DAL SI 7-69903-12AD.