What was found
DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1256 JAMB DOOR R3 FOUND CRACK 0.5" LONG ON THE WEB UPPER SIDE 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 1256 JAMB DOOR R3 FOUND CRACK 0.5" LONG ON THE WEB UPPER SIDE REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.