What was found
CRACK - STRINGER OF FUSELAGE STA 880 TO STA 900 S10R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-6 REV 40 AND DWG 142U3725 SH 19 REV -. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK - STRINGER OF FUSELAGE STA 880 TO STA 900 S10R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-6 REV 40 AND DWG 142U3725 SH 19 REV -. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)