What was found
FOUR FASTENER HOLES CRACKED IN THE FUSELAGE SKIN, STA 908 - STA 951, S10R. THREE FASTENER HOLES CRACKED IN THE FUSELAGE SKIN, STA 908 - STA 951, S10L. REPAIRED PER DALFORT AEROSPACE XEA X2-53-219, REV 2 DATED 8-25-98 AND BOEING SRM 53-30-3, FIG 42. APPROVAL DATA: FAA FORM 8110-3 DATED 8-24-98.