As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A MAINTENANCE VISIT FOUND CRACK IN FUSELAGE SKIN AT LONGERON 31 RT (2 INCH CRACK) STA 1690. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLER IAW SRM 51-1-8 AND 51-1-21 AND DER APPROVED EO 00-016. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.