What was found
INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 727E + 3, S23L. REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 201, PROCEDURE 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 727E + 3, S23L. REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 201, PROCEDURE 5.