What was found
CRACK ON FUS SKIN AT BS500B TO 500C BETWEEN 23L & 24L REPAIRED CRACK ON FUSELAGE SKIN AT STA 500B TO 500C BETWEEN STRINGER 23L AND 24L IAW SB 737-53-1168 REV 4 AND SRM REV 116 CHAPTER 53-00-01 REPAIR 31 FIG 201 DETAIL VII.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FUS SKIN AT BS500B TO 500C BETWEEN 23L & 24L REPAIRED CRACK ON FUSELAGE SKIN AT STA 500B TO 500C BETWEEN STRINGER 23L AND 24L IAW SB 737-53-1168 REV 4 AND SRM REV 116 CHAPTER 53-00-01 REPAIR 31 FIG 201 DETAIL VII.