What was found
DURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN THE RIGHT HAND FUSELAGE TO WING ANGLE P/N 114-43002-180 AND THE DOUBLER INSTALLED IN AUGUST OF 2000. THE ANGLE HAD BEEN PREVIOUSLY REPAIRED, RECORDED AND SUBMITTED ON A 337 DATED 08/15/00. THE DAMAGE INCLUDED SEVERAL SEARED RIVETS AND AN 1 INCH CRACK IN THE DOUBLER NEAR FS 288. THE DAMAGE WAS REPAIRED BY REMOVING THE OLD DOUBLER AND ANGLE AND INSTALLING A NEW ANGLE IAW 1900 AIRLINES SERIES SRM. THE TIME BETWEEN THE TWO MAJOR REPAIRS WAS 14599.6.