What was found
DURING C-CHECK, FOUND UPPER LEADING EDGE GOUGED AND CRACKED AT XRS 289. STOP DRILLED CRACK, FABRICATED DOUBLER FROM .063 7075T-6AL, IAW DER APPROVED ENGINEERING SKETCH A96-R01 AND INSTALLED IAW DC-8 SRM 51-1-20D, 21, 21D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND UPPER LEADING EDGE GOUGED AND CRACKED AT XRS 289. STOP DRILLED CRACK, FABRICATED DOUBLER FROM .063 7075T-6AL, IAW DER APPROVED ENGINEERING SKETCH A96-R01 AND INSTALLED IAW DC-8 SRM 51-1-20D, 21, 21D.