What was found
INSPECTION FOUND A .75 INCH CRACK IN EXTERIOR FUSELAGE SKIN AT CAPTAIN'S WINDSHIELD O/B CORNER, STA 219.8-227.8, S9L. THE SKIN WAS REPAIRED IAW SRM 53-10-01, FIGURE 201, REPAIR 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK IN EXTERIOR FUSELAGE SKIN AT CAPTAIN'S WINDSHIELD O/B CORNER, STA 219.8-227.8, S9L. THE SKIN WAS REPAIRED IAW SRM 53-10-01, FIGURE 201, REPAIR 10.