What was found
CRACK AT FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE. SUMMARY OF NRC 00644: FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0851423)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK AT FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE. SUMMARY OF NRC 00644: FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0851423)