What was found
WHILE ON GROUND, MAINTENANCE FOUND CRACK ABOUT 1.25 INCHES LONG ON WING L/E LOWER OUTBOUND OF NR 2 ENGINE, 8 INCHES AFT OF FIRE BOTTLE INSP PLATE INBOUND. REPAIRED PER UPS ENGINEERING FILE NR DC8-57-0615.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE ON GROUND, MAINTENANCE FOUND CRACK ABOUT 1.25 INCHES LONG ON WING L/E LOWER OUTBOUND OF NR 2 ENGINE, 8 INCHES AFT OF FIRE BOTTLE INSP PLATE INBOUND. REPAIRED PER UPS ENGINEERING FILE NR DC8-57-0615.