What was found
CORROSION AT CUSP WEB BETWEN STA 832 AND STA 851 AND X=60 PAX CABIN. SUMMARY OF NRC 0395: CORROSION LEVEL 2. CORROSION AT CUSP WEB BETWEN STA 832 AND STA 851 AND X=60 PAX CABIN WAS REMOVED B717-200 SRM 51-10-04-0G PAR 26 C (1). (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON AT CUSP WEB BETWEN STA 832 AND STA 851 AND X=60 PAX CABIN. ORIGINAL THICKNESS IS 0.040IN REMAINING THICKNESS IS 0.017IN THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE PAR 4 C AND DC-MD/BOEING NDT SPM PART 4, 04-00-06 PAR 4 FIG 9. AREA OUT LIMITS WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 215. (LP #0222439)