What was found
THE FUSELAGE SKIN WAS CRACKED AT LONGERON 22L FS 194 BELOW THE AIRSTAIR DOOR CUTOUT. MAINTENANCE INSPECTED AND REPAIRED THE FUSELAGE IAW DC-9 SRM 53-04 FIG 12B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN WAS CRACKED AT LONGERON 22L FS 194 BELOW THE AIRSTAIR DOOR CUTOUT. MAINTENANCE INSPECTED AND REPAIRED THE FUSELAGE IAW DC-9 SRM 53-04 FIG 12B.