What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE AT 2D FASTENER HOLE FROM TOP OF ANGLE AT VSS 5.00, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-55-016. 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 RT FWD SPAR CAP ANGLE AT 2D FASTENER HOLE FROM TOP OF ANGLE AT VSS 5.00, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-55-016. MAJOR REPAIR.