What was found
C4 CHECK - 2.0" LONG CRACK IN FUSELAGE SKIN AT BS 801, S23L. REPAIRED FUSELAGE SKIN AT BS 801, S23L IAW B737 SRM 53-00-01-2R-31, FIG 201, PROCEDURE V, DETAIL VIII.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C4 CHECK - 2.0" LONG CRACK IN FUSELAGE SKIN AT BS 801, S23L. REPAIRED FUSELAGE SKIN AT BS 801, S23L IAW B737 SRM 53-00-01-2R-31, FIG 201, PROCEDURE V, DETAIL VIII.