What was found
AT C CHECK, RT WING UPPER L/E INTERIOR WEB AT STA 0 O/B SUPPORT ANGLE CRACKED L/E STA 349. REMOVED AND FABRICATED SUPPORT ANGLE PER SRM 51-40-3 1, 65 BY 15, 65 N/R 2826.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, RT WING UPPER L/E INTERIOR WEB AT STA 0 O/B SUPPORT ANGLE CRACKED L/E STA 349. REMOVED AND FABRICATED SUPPORT ANGLE PER SRM 51-40-3 1, 65 BY 15, 65 N/R 2826.