As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 94-03-01, FOUND THE UPPER FORWARD CORNER OF SERVICE DOOR JAMB HAD A CRACK IN THE EXTERIOR SKIN AT RIVET STA 160. TO GAIN ACCESS TO REPAIR SKIN THE WEB WAS CUT AT STA 184.375. REPAIRED CRACKED SKIN IAW DC-9 SRM 53-05 FIGURE 38 AND 51-30-5. INSTALLED WEB SPLICE IAW ABX REA D953-11251-MR.