What was found
CRACKS ON STRINGERS 6LH, 8LH AND 6RH STA Y=1022 AT INTERNAL FUSELAGE (PAX CABIN). SUMMARY OF NRC 00153: REPAIR ON STRINGERS 6LH, 8LH AND 6RH STA Y = 1022 AT INTERNAL FUSELAGE WAS PERFORMED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 PAR 5 FIG 201. (LP #2891854)