What was found
DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR R3 FOUND CRACK 0.5 INCH LONG ON THE WEB. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR R3 FOUND CRACK 0.5 INCH LONG ON THE WEB. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.