What was found
DURING OP 16 MAINT CHECK, FOUND RT SIDE OF FUSELAGE WITH STATIC BURN AT STA 110, 24 IN BELOW RT SLIDING WINDOW. BLENDED OUT PER SRM 53-04. NDT SHOWED CRACK WHICH WAS REPAIRED PER SRM 53-04 FIG 38.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 16 MAINT CHECK, FOUND RT SIDE OF FUSELAGE WITH STATIC BURN AT STA 110, 24 IN BELOW RT SLIDING WINDOW. BLENDED OUT PER SRM 53-04. NDT SHOWED CRACK WHICH WAS REPAIRED PER SRM 53-04 FIG 38.