What was found
C4 CHECK - 1.25 INCH LONG CRACK IN FUSELAGE SKIN AT BS 727E, S24R. REPAIRED FUSELAGE SKIN AT BS 727E, S24R IAW SRM 53-00-01-2R-31 PROCEDURE V, FIG 201, DETAIL XI.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C4 CHECK - 1.25 INCH LONG CRACK IN FUSELAGE SKIN AT BS 727E, S24R. REPAIRED FUSELAGE SKIN AT BS 727E, S24R IAW SRM 53-00-01-2R-31 PROCEDURE V, FIG 201, DETAIL XI.