What was found
DURING THE INTERMEDIATE EXTERNAL INSPECTION THE CREW DISCOVERED TWO HOLES PUNCTURED IN THE FUSELAGE SKIN BELOW AND AFT OF THE CARGO DOOR. THE HOLES WERE TEMP REPAIRED AND THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE REPAIRED DAMAGED STRINGERS 22L & 23L IAW CRJ 200 SRM 53-00-03 AND REPAIRED THE FUSELAGE SKIN AT FS 605-654.50 STR 20L-24L IAW BOMBARDIER REPAIR ENGINEERING ORDER 601R-53-61-1391. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.