What was found
C-CHECK: FUSELAGE LT SIDE AT FRAME 68, STRINGER 23, LEFT LATERAL SHEAR PLATE CRACKED. R & R PLATE IAW SRM 51-42-11, PAR 6.B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C-CHECK: FUSELAGE LT SIDE AT FRAME 68, STRINGER 23, LEFT LATERAL SHEAR PLATE CRACKED. R & R PLATE IAW SRM 51-42-11, PAR 6.B.