What was found
DURING OP 16 MAINT CHECK AT STA 936, RBL 6 IN, FWD SIDE FUSELAGE PANEL SUPPORT STRUCTURE HAD 1.5 IN HORIZONTAL CRACK. REPAIRED PER SRM 53-05, FIG 81 PAGE 267.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 16 MAINT CHECK AT STA 936, RBL 6 IN, FWD SIDE FUSELAGE PANEL SUPPORT STRUCTURE HAD 1.5 IN HORIZONTAL CRACK. REPAIRED PER SRM 53-05, FIG 81 PAGE 267.