What was found
AT C-CHECK, R/W WS 224 COVE PANEL ANGLE CRACKED BELOW NR 8 SPOILER ACTUATOR. REMOVED AND REPLACED ANGLE PER SRM 51-30-2, 9 X 4. N/R 2356
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, R/W WS 224 COVE PANEL ANGLE CRACKED BELOW NR 8 SPOILER ACTUATOR. REMOVED AND REPLACED ANGLE PER SRM 51-30-2, 9 X 4. N/R 2356