What was found
C4 CHECK - 1.25 INCH LONG CRACK IN FUSELAGE SKIN AT BS 727F+3 INCHES, S22R. REPAIRED FUSELAGE SKIN AT BS 727F+3 INCHES, S22R IAW SRM 53-00-01-2R-31, PROCEDURE V, FIG 201.
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 727F+3 INCHES, S22R. REPAIRED FUSELAGE SKIN AT BS 727F+3 INCHES, S22R IAW SRM 53-00-01-2R-31, PROCEDURE V, FIG 201.