What was found
ANGLE CRACKED THROUGH 7 FASTENERS INSIDE AT BOTOM OF RIGHT WING LEADING EDGE RIB AT WBL 92.0 INBOARD AND AFT OF NR 4 LEADING EDGE FLAP AREA. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-10-6 AND 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ANGLE CRACKED THROUGH 7 FASTENERS INSIDE AT BOTOM OF RIGHT WING LEADING EDGE RIB AT WBL 92.0 INBOARD AND AFT OF NR 4 LEADING EDGE FLAP AREA. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-10-6 AND 51-10-1.