What was found
AT C-CHECK, CRACK AT BS 1263 RT SIDE BELOW UPPER SKIN TORQUE BOX FWD SIDE OF FS 1263 UNDER FILLER. REMOVED AND INSTALLED ANGLE PER SRM 51-30-2. 30 BY 1.5 BY 1.5. INSTALLED WEB REPAIR ON TORQUE BOX PER SRM 51-40-2, 31. BY 15. N/R 4850.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, CRACK AT BS 1263 RT SIDE BELOW UPPER SKIN TORQUE BOX FWD SIDE OF FS 1263 UNDER FILLER. REMOVED AND INSTALLED ANGLE PER SRM 51-30-2. 30 BY 1.5 BY 1.5. INSTALLED WEB REPAIR ON TORQUE BOX PER SRM 51-40-2, 31. BY 15. N/R 4850.