What was found
HFEC INSPECTION FOUND 01EA CRACK APPROX 0.350" IN LENGTH ON STA 1809 RIGHT FORWARD OUTER CHORD BETWEEN STA 4R AND 5R , ABOUT 1" FROM STR 5R AS MARKED . PER W/C 5310-0138-0202 STEP 6. STA 1809 RIGHT FORWARD CHORD BETWEEN S-4R AND 7R CRACK AREA CUTED OUT AND ERMOVED AS PER B767-400 SRM 53-80-08 REPAIRE 9 REV 58.00 09/05/2019. THE REPAIR PART MADE FORM 7075-0-0.080" CLAD HEAT TREAT TO T62 , 7075-0-0.071" CLAD HEAT TREAT TO T62 , 7075 0-0.090" CLAD HEAT TREAT TO T62, 7075-T7451 EXTRUSION BAR 4"X4" AS PER B767-400 SRM 53-80-08 REPAIR 9 REV58.00 09/05/2019. THE REPAIR PARTS INSTALLED ON STA 1809 RH FORWARD OUTER CHORD BETWEEN STA 4R AND STR 7R AS PER B767-400 SRM 53-80-08 REPAIR 9 REV58.00 09/05/2019. THE REPAIR IS A CATEGORY B REPAIR AND REQUIRES THE SUPPLEMENTAL INSPECTION THRESHOLD :30000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR WITHIN 6000 FLIGHT CYCLES FROM THE REPAIR INSTALLATION WHICHEVER COMES LAST. (1400796)