What was found
DURING T-CHECK, FOUND A 4.3 CRACK IN THE RIGHT WING FRONT SPAR TO FUSELAGE ATTACH ANGLE FS 1159 AT LONGERON 28R. REPAIRED ANGLE (P/N ANB 7353-1), PER EA 11-99276.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING T-CHECK, FOUND A 4.3 CRACK IN THE RIGHT WING FRONT SPAR TO FUSELAGE ATTACH ANGLE FS 1159 AT LONGERON 28R. REPAIRED ANGLE (P/N ANB 7353-1), PER EA 11-99276.