What was found
DURING D-CHECK, LEADING EDGE SUPPORT ANGLE CRACKED AT UPPER AFT CORNER ALONG RADIUS FSS 337. REMOVED AND REPLACED ANGLE PER SRM 51-10-1 15 INCHES BY 2 INCHES 2024-T3 .040.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, LEADING EDGE SUPPORT ANGLE CRACKED AT UPPER AFT CORNER ALONG RADIUS FSS 337. REMOVED AND REPLACED ANGLE PER SRM 51-10-1 15 INCHES BY 2 INCHES 2024-T3 .040.