What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE AT CSS 69.184 AND 20 PERCENT CHORD, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-55-004. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE AT CSS 69.184 AND 20 PERCENT CHORD, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-55-004. MAJOR REPAIR.